AIRBUS 

Customer Services Directorate 

A340 Airworthiness Limitation Items

A340 

Airworthiness Limitation Items

© AIRBUS SAS 2009. All rights reserved. Confidential and proprietary document. 

This document and all information contained herein is the sole property of AIRBUS SAS. No 

intellectual property rights are granted by the delivery of this document or the disclosure of its 

content. This document shall not be reproduced or disclosed to a third party (except for the 

purposes of performing the tasks described hereunder and provided that any recipient of such 

document shall comply with the conditions herein) without the express written consent of AIRBUS 

SAS. This document and its content shall not be used for any purpose other than that for which it is 

supplied.

AI/SE-M4/95A.0051/97 

20 Feb 2009 

Issue 11
AIRWORTHINESS LIMITATION ITEMS 

TABLE OF CONTENTS

SUBJECT SECTION

ISSUE: FEB 20/09 PAGE: 1-TOC 

©AIRBUS SAS 2009. All rights reserved. 

A340

RECORD OF REVISIONS ROR 

INTRODUCTION 1 

 GENERAL 1-1 

 Airworthiness Limitations 1-1- A 

 RULES FOR COMPLIANCE DEMONSTRATION 1-2 

 General 1-2- A 

 Conditions for DT ALI inspection 1-2- B 

 Reporting 1-2- C 

 Production/Repair concessions and Alternative Means Of Compliance 1-2- D 

 Modifications/repairs not originating from Airbus 1-2- E 

 LIMIT OF VALIDITY (LOV) 1-3 

 APPLICABILITY 1-4 

 General 1-4-A 

 Weight Variant (WV) applicability 1-4-B 

 Applicability System 1-4-C 

 EXPLANATION OF SECTION 2 TABLE FORMAT 1-5 

AIRWORTHINESS LIMITATIONS 2 

 A340-200/300 Airworthiness Limitation Items 2-1 

 A340-500/600 Airworthiness Limitation Items 2-2 

SUMMARY OF CHANGES APPENDIX A 

 

 ABBREVIATIONS APPENDIX B 

TERMS AND DEFINITIONS APPENDIX C 
AIRWORTHINESS LIMITATION ITEMS 

RECORD OF REVISIONS

ISSUE: FEB 20/09 PAGE: 1-ROR 

EASA APPROVED 

©AIRBUS SAS 2009. All rights reserved. 

A340

Issue Date Reason for revision Approved 

by EASA 

1 22 Aug 97 Section 2 of CMR documents originally identified 

‘Structural Inspections’ These are not CMRs. New 

document created. 

Target date for inclusion of these requirements in 

MRB report extended from 1998 to 1999. 

2 17 Oct 00 Title of document changed from ‘Structural 

Inspection Requirements’ to ‘Airworthiness 

Limitation Items’. 

Document completely revised to introduce ALIs 

following completion of the full-scale fatigue test 

and teardown analysis. 

3 30 Apr 02 Document amended to include –600 

requirements. Section 2 renamed section 2.1, 

now contains all –200 and –300 data. New 

Section 2.2 contains all –600 data. Reference to 

Zonal Program deleted from paragraph 1.5. 

4 30 Sep 02 Section 1 amended to include new WV 

applicability. Section 2.1 amended to include 

requirements of WV 027. Task numbering, 

applicability and format of sections 2.1 amended 

to provide compatibility with MRBR and MPD. 

The requirements in Section 2.2 remain 

unchanged in this revision.

5 02 Dec 02 Document amended to include new -500 tasks 

and modified -600 tasks in Section 2.2. Task 

numbering, applicability and format of sections 

2.2 amended to provide compatibility with MRBR 

and MPD. New ALIs added in Section 2.1. 

6 30 May 03 Temporary ALI requirements added for 

modifications 48487 & 48538. 

7 29 Jan 04 ALI requirements added for modifications 48487 

& 48538 for A340-500/600.New requirements 

added for A340-300 WV 50 series included. 

New ALIs added for A340-200/300 in ATA 71 & 

78. Applicability of ALIs in ATA 71 & 78 extended 

to new alternative powerplant CFM 56-5C/P. 

Existing tasks are changed due to revised lift off 

loads, “enhanced” modifications 48437, 48779, 

49008 & 49202 and product improvement 

modifications. 
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RECORD OF REVISIONS

ISSUE: FEB 20/09 PAGE: 2-ROR 

EASA APPROVED 

©AIRBUS SAS 2009. All rights reserved. 

A340

Issue Date Reason for revision Approved 

by EASA 

8 10 Oct 05 Task applicabilities changed due to impact of 

product improvement mods for A340 WV000 up 

to WV030 series. 

Minor changes on A3456 tasks. 

WV and Groups added for A340-500 and A340-

600. 

New numbering rules (ALI task previously with 9 

digits replaced by 10 Digit number system) 

included in section 2.1 and 2.2. 

WV029, 030 added for Group 43B. 

Confidentiality statement added. 

Approved by 

EASA 

under reference 

EASA.A.C.01279 

on 17 January 2006

9 17 Jan 06 For A340-600, tasks updated following full-scale 

fatigue and teardown analysis. 

GROUP 46B created for new WV 101 and 102. 

Tasks updated and created for Group 46B. 

Approved by 

EASA 

under reference 

EASA.A.414 

on 24 April 2006

10 1 Feb 07 Tasks updated and created following full-scale 

fatigue and teardown analysis. 

WV 053 and 054 added for Group 43E. 

GROUP 45B created for new WV 101, 102 and 

103. 

Tasks updated and created for Group 45B. 

Approved by 

EASA 

under reference 

EASA.A.C.05841 

on 13 April 2007

11 20 Feb 09 New compliance time requirements introduced in 

the Record Of Revisions. 

Introduction reworded with: 

New Limit Of Validity (LOV) (A340-200/-300 

WV<50 only) 

New information concerning Rules for 

Compliance Demonstration (Alternative 

inspections, Multiple WV configuration...) 

Task requirements updated due to: 

Intermediate Service Goal exercise (A340-200/-

300 WV<50 only) 

Fleet survey results (A340-200/-300 only) 

Modifications/In-service experience 

WV 004 added for Group 45A. 

Approved by 

EASA 

under reference 

10026899 

on 20 August 2009 
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RECORD OF REVISIONS

ISSUE: FEB 20/09 PAGE: 3-ROR 

EASA APPROVED 

©AIRBUS SAS 2009. All rights reserved. 

A340

COMPLIANCE TIME:

1. From 20 August 2010 it is mandatory to comply with the airworthiness limitations as 

defined in the A340 ALI Document at Issue 11. 

2. From 20 August 2009 to 19 August 2010, except for those specific task/applicabilities 

limitations stated in paragraph 3, it is mandatory to comply with the airworthiness 

limitations defined in, either: 

− The ALI Document at issue 10 

or, 

− The ALI Document at issue 11. 

3. From 20 August 2009 to 19 August 2010, for the following task/applicabilities limitations, 

it is mandatory to comply with the airworthiness limitations defined in, either: 

− Table 1 or table 2 

or, 

− The ALI Document at Issue 11: 

TABLE 1 

Adapted Threshold 

(whichever occurs first, from aircraft first 

flight) 

Task 

reference 

FH FC 

Applicability 

533111-01-01 70170 9902 MSN 006 

 71374 10000 MSN 007 

 72197 8713 MSN 013 

 71786 8138 MSN 015 

 73820 9991 MSN 018 

 73794 10000 MSN 019 

 72249 10000 MSN 021 

 71468 9950 MSN 023 

 72731 9886 MSN 025 

 78329 9540 MSN 035 

 71237 9073 MSN 038 

 69134 8944 MSN 043 

 76176 9877 MSN 053 

 73721 9912 MSN 056 

 71035 9341 MSN 057 

 82467 10040 MSN 058 

 72152 10040 MSN 078 

 73246 10040 MSN 084 

533163-01-01 72197 8713 MSN 013 

 71786 8138 MSN 015 

 71237 9073 MSN 038 

 69134 8944 MSN 043 

 73872 9242 MSN 052 

 70283 9242 MSN 057 

 69705 8487 MSN 058 

 65755 9013 MSN 084 
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RECORD OF REVISIONS

ISSUE: FEB 20/09 PAGE: 4-ROR 

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A340

TABLE 1 

Adapted Threshold 

(whichever occurs first, from aircraft first 

flight) 

Task 

reference 

FH FC 

Applicability 

571102-01-02 38200 11718 MSN 242 

571103-01-02 

571103-02-02 37200 11411 MSN 242, 243,264 

571123-01-01 

571123-01-02 

571123-01-03 

571123-01-04 

571123-01-05 

Refer to AD 2008-0050 ALL 

571149-01-03 38000 11656 MSN 242 

572046-01-02 44267 10522 MSN 199 

572052-01-01 49631 11194 MSN 159 

575022-01-01 73847 13009 MSN 032 

 74226 12957 MSN 033 

 74652 12895 MSN 034 

 64693 14813 MSN 039 

575023-01-01 71549 12604 MSN 032 

 72203 12604 MSN 033 

 72967 12604 MSN 034 

 56033 12604 MSN 101 

TABLE 2 

Adapted interval 

for the next task accomplishment only 

(whichever occurs first, from last 

accomplishment of the task) 

Task 

reference 

FH FC 

Applicability 

534136-01-01 14700 2200 MSN 005 

 14700 2200 MSN 006 

 14700 2200 MSN 007 

 14700 2200 MSN 008 

572030-01-01 22300 3610 MSN 056 

 22300 3336 MSN 075 

575022-01-01 41363 9471 MSN 039 

575023-01-01 15176 2673 MSN 032 

 15254 2663 MSN 033 

 15342 2650 MSN 034 

 13463 3028 MSN 101 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: FEB 20/09 PAGE: 1 

EASA APPROVED 

©AIRBUS SAS 2009. All rights reserved. 

A340

1 INTRODUCTION

1-1 GENERAL

The data provided has been established with the following rules: 

Compliance with the requirements contained in this document is mandatory. ALL 

aircraft shall be operated in accordance with the requirements of ALI Document, 

unless otherwise agreed with the Authority of the State of aircraft registry. 

Note: The ALI Document is covered by the Certification Document 00F050A3401/C01. 

1-1-A Section 2 - Airworthiness Limitations

The section 2 contains airworthiness limitations arising from fatigue and damage 

tolerance evaluation on structural element that could contribute to catastrophic failure 

of the aircraft. 

The ALI requires also to control corrosion to Level 1 or better on all metallic structure 

details, elements or assemblies which contribute significantly to carrying flight, 

ground, or pressurization loads, and whose failure could result in catastrophic failure 

of the airplane. 

Corrosion Level 1 is defined as follows: 

- Corrosion damage that does not require structural reinforcement or replacement. 

or 

- Corrosion occurring between successive inspections that exceeds allowable limit 

but is local and can be attributed to an event not typical of Operator usage of other 

aircraft in the same fleet (e.g. mercury spill). 

The Corrosion Prevention and Control Program (CPCP) defined in the Structure 

Program (SECTION D) of the A340 MRB Report is an acceptable means of 

compliance. 

Credit may be taken for the Maintenance Review Board Report (MRBR) Structures 

Section maintenance tasks, providing that they are performed with the same 

inspection level, as frequently, or more frequently, than the inspection threshold and 

interval quoted in this document. Additional information concerning DT ALI 

requirements can be found in the following Airbus supporting publications: 

- Maintenance Planning Document (MPD), 

- Aircraft Maintenance Manual (AMM), 

- Non-Destructive Testing Manual (NTM) 

- Structural Repair Manual (SRM). 
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INTRODUCTION

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A340

1-2 RULES FOR COMPLIANCE DEMONSTRATION

1-2-A General

The ALI document is applicable and mandated up to the Limit Of Validity (LOV) in FC 

or FH whichever occurs first. (Refer to paragraph 3 for definition of the LOV). No 

aircraft shall be operated beyond the LOV of the ALI Document, unless the Type 

Certificate Holder (i.e. Airbus) has updated this document to reflect a LOV extension 

approved by the Type Certification Authority (EASA). 

The Threshold is the time at which the maintenance requirement is first due. 

- For FC of FH tasks without MOD applicability, the thresholds are counted from 

first flight. 

- For FC or FH tasks with MOD applicability the thresholds are counted from point 

of embodiment, unless otherwise stated. 

- For tasks in Calendar Time, the thresholds are counted from date of initial 

delivery from manufacturer, unless otherwise stated. 

For repeat maintenance tasks, the interval starts at the time of the last maintenance 

task accomplishment. 

When alternative inspection methods are provided, the next interval applicable is the 

one associated with the inspection method used at last inspection. 

In cases when the first maintenance task is accomplished very early, the next 

inspection can be performed at the threshold if the period (years, FC or FH) between 

initial task accomplishment and the threshold is greater than the interval. 

“Touch and Go" cycles can be neglected if they are less than 5% of the total number 

of Flight Cycles up to threshold inspection or between two consecutive inspections. 

Each "Touch and Go" cycle above 5% is to be counted as one Flight Cycle, up to 

threshold inspection or between two consecutive inspections. 

1-2-B Conditions for DT ALI inspection

It is assumed that the DT ALI to be inspected is in a state of cleanliness, which 

allows a satisfactory inspection to be carried out at the required inspection level. 

Where existing Temporary Protection System (TPS) permits unobscured 

assessment of the condition of the DT ALI, then that TPS may remain in place for 

the inspection. 

Limitations quoted in section 2 are applicable to the undamaged and unrepaired DT 

ALI. Damage has to be evaluated and repaired in accordance with the AIRBUS

Structural Repair Manual (SRM) or other documentation acceptable to the relevant 

Airworthiness Authority. 
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INTRODUCTION

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A340

If damage is found or suspected (such as bulging skin, paint discoloration) then the 

full extent of any damage must be clearly identified using appropriate inspection 

techniques and/or disassembly when necessary. This may require additional 

access to that stated for the DT ALI maintenance requirement. 

In cases of damage or repair, the DT ALI maintenance requirements may have to 

be adapted, or additional requirements may be necessary. In these cases the 

requirements that are given in the relevant documents (SRM or specific Repair 

design Approval Sheet) must be applied. 

If inspections indicate evidence of deterioration, appropriate further actions must be 

taken to prevent similar deteriorations from occurring in the Operator’s fleet. 

1-2-C Reporting

Any damage, e.g. fatigue cracks or corrosion greater than Level 1 (regardless where 

and when the corrosion is detected) shall be reported to Airbus. 

The finding report should include at least the information stated below: 

− DT ALI maintenance requirement reference, 

− Aircraft Manufacturer Serial Number (MSN) affected, 

− Life (in FH and/or FC and/or calendar time, as applicable) accumulated at the 

time of the finding, 

− Identification of the affected structure, 

− Location and description of the finding, with indication of the size and 

orientation, 

− Circumstance of detection and inspection method used. 

1-2-D Production/Repair concessions and Alternative Means Of Compliance

Limitations of the ALI may be superseded by instructions given in either a 

Production concession, a Repair design Approval Sheet (RAS) or an Alternative 

Means Of Compliance (AMOC). 

It is the operator’s responsibility to refer to the applicable limitations. 
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INTRODUCTION

ISSUE: FEB 20/09 PAGE: 4 

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A340

1-2-E Modifications/repairs not originating from Airbus

If an aircraft/a DT ALI has a modification or repair embodied that is not of Airbus 

origin (e.g. Supplemental Type Certificate) and which affects the content of the ALI, 

the Operator is responsible for obtaining approval by the relevant Airworthiness 

Authority for any necessary adaptations of the limitations. 

1-3 LIMIT OF VALIDITY (LOV)

LOV Aircraft series Flight Hours Flight Cycles 

A340-200/300 excl. WV027 100000 20000 

A340-300 WV 027 60000 30000 

A340-500/600 100000 16600 

1-4 APPLICABILITY

1-4-A General

ALI document covers the following aircraft models and the following weight variants: 

Aircraft series Aircraft models WV 

A340-211 000, 001, 002 

A340-200 A340-212 000, 001, 002 

A340-213 000, 001, 002, 021 

A340-311 000, 001, 002, 003, 004 

A340-312 000, 001, 002, 003, 004, 

029 

A340-300 

A340-313 

000, 001, 002, 003, 004, 

020, 021, 023, 024, 025, 026, 027, 

028, 

050, 051, 052, 053, 054 

A340-541 000, 001, 002, 003, 004, 

A340-500 101, 102, 103 

A340-542 101, 102, 103 

A340-642 000, 001, 

A340-600 101, 102, 103 

A340-643 101, 102, 103 
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INTRODUCTION

ISSUE: FEB 20/09 PAGE: 5 

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A340

1-4-B Weight Variant (WV) applicability

A/C series Weight variants WV Group 

000, 001, 002 Group 42A

A340-200 

021 Group 42B 

000, 001, 002, 003, 004 Group 43A

020, 021, 023, 024, 025, 026, 028, 029 Group 43B 

027 Group 43C 

A340-300 

050, 051, 052, 053, 054 Group 43E 

000, 001, 002, 003, 004, Group 45A 

A340-500 

101, 102, 103 Group 45B

000, 001 Group 46A

A340-600 

101, 102, 103 Group 46B

Interpretation: Group XYZ 

- X: Aircraft Type 4 for A340 

- Y: Series (2 for -200, 3 for -300, 5 for -500 and 6 for -600) 

- Z: Various WV corresponding to a specific certified Type/Serie 

DT ALIs may have different limitations depending on the aircraft WV. The applicability 

of limitations for different aircraft weight variants are indicated with the help of WV 

groups. These groups are given in addition to the general applicability system in 

order to improve the readability of the applicability column. 

The ALI section 2 tables provide limitations depending on the aircraft weight variants 

within the limits of the list of WV’s defined in the above table. 

Section 2 is defined through 2 sub-sections: 

- Section 2.1for A340-200/-300 requirements 

- Section 2.2 for A340-500/-600 requirements 

It is Operator’s responsibility to refer to the applicable WV. 

The applicable Weight Variant status for each individual aircraft at delivery can be 

found in Table 1 “Airplane Allocation List” of the Structural Repair Manual (SRM) 

introduction. This Table 1 does not necessarily reflect the actual current status of the 

aircraft that needs to be confirmed using the weight variant information given in Table 

3 of SRM introduction. 
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ISSUE: FEB 20/09 PAGE: 6 

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A340

Table 3 “Weight Variant/Service Bulletin list” shows the Service Bulletins with the 

associated modifications corresponding to the weight variant change after the aircraft 

delivery. 

It is operator’s responsibility to check the embodiment of the referenced Service 

Bulletins in order to determine the relevant weight variant for the affected 

Manufacturer Serial Number (MSN). 

For aircraft having multiple WV configurations possibility, the limits of the WV of the 

highest MTOW have to be applied. 

The Fatigue figures for WV 027 are based on an average flight time of 2.0 FH/FC. 

The operator must contact Airbus if this figure exceeds 2.5 FH/FC.
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INTRODUCTION

ISSUE: FEB 20/09 PAGE: 7 

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A340

1-4-C Applicability system

The applicability column of ALI sub-part 2-1 indicates the aircraft type/ series/ model/ 

weight variant group and modification status for which the task is applicable. 

Examples are given below: 

Applicability Task applicable to 

A340-xxx -xxx series aircraft. 

A340-xxx 

PRE nnnnn 

xxx series aircraft PRE MOD nnnnn. 

i.e. A340 xxx series that do not have MOD nnnnn embodied. 

A340-xxx 

POST nnnnn 

xxx series aircraft POST MOD nnnnn. 

i.e. A340 xxx series that do have MOD nnnnn embodied. 

A340-xxx 

POST nnnnn 

Sxxxxx 

xxx series aircraft POST MOD nnnnn (at least with Mod Proposal 

Sxxxxx embodied). 

A340-xxx 

POST nnnnn 

POST mmmmm 

xxx series aircraft POST MOD nnnnn and POST MOD mmmmm. 

i.e. A340 xxx series that do have MOD nnnnn and MOD mmmmm 

embodied. 

A340-200 

OR 

A340-300 

PRE nnnnn 

All A340-200, 

Or, 

All A340-300 that do not have MOD nnnnn embodied. 

A340-200 

POST nnnnn 

OR 

POST mmmm 

All A340-200 that do have MOD nnnnn embodied, 

Or, 

All A340-200 that do have MOD mmmm embodied. 

A340-200 

POST nnnnn 

OR 

A340-300 

POST nnnnn 

PRE mmmmm 

All A340-200 that do have MOD nnnnn embodied, 

Or, 

All A340-300 that do have MOD nnnnn embodied and do not have 

MOD mmmmm embodied. 

Door Type 1 Door Type 1 = 1.60 m High, 0.61 m Wide - Emergency exit type 

door. 

Door Type A Door Type A = 1.93 M High, 1.07 m Wide - Pax type door. 

GROUP XYZ All aircraft with weight variant group XYZ 

GROUP XYZ 

PRE nnnn 

All aircraft with weight variant group XYZ that do not have MOD 

nnnn embodied 

GROUP XYZ 

POST nnnn 

All aircraft with weight variant group XYZ that do have MOD nnnn 

embodied 
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INTRODUCTION

ISSUE: FEB 20/09 PAGE: 8 

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A340

1-5 EXPLANATION OF SECTION 2 TABLE FORMAT

Detailed information is given below concerning the format of the section 2 tables: 

REV CODE

This column indicates the revision code “status ” of the DT ALI maintenance 

requirement compared to previous issue of the document. 

<Blank> = No amendment. 

<R> = The DT ALI maintenance requirement has been revised. 

<N> = The DT ALI maintenance requirement is new. 

<D> = The DT ALI maintenance requirement is deleted. 

TASK REFERENCE

This column indicates the task number, e.g. 521101-01-01. It is composed of 10 

digits as follows: 

XXXXXX-XX-XX 

 Applicability index 

 Sequential number 

 SSI number 

The SSI number is represented by the six first digits, e.g. 521101. 

The sequential number is composed of two digits. It identifies different inspections 

e.g. Detailed or Special Detailed. 

The applicability index is composed of two digits. It identifies different applicability 

e.g. aircraft series, mod status, WV group etc ...It is also used to differentiate 

between access differences e.g. different access panel numbers. 
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A340

ACCESS

This column indicates the access requirements to adequately perform the 

inspection, i.e. all items listed must be removed or opened unless otherwise stated 

(e.g. NOTE 1). 

“NOTE 1” means “Insulation to be displaced as required to complete the 

inspection”. 

TASK DESCRIPTION

This column describes the inspection to be performed. It includes the inspection 

level, the description and the boundaries of the DT ALI to be inspected. All structural 

items within this boundary are to be inspected, unless otherwise stated. Additional 

information may be added to clarify the inspection area. 

Where applicable, notes providing details of alternative inspections, and inspections 

to be performed at the same time, are included. 

THRESHOLD

This column indicates the threshold when the inspection is due for the first time. 

INTERVAL

This column indicates the repeat interval when the inspection is due the second and 

subsequent times. 

APPLICABILITY

This column indicates the applicability of the task. 
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

521101-01-01 831 841 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 1 (FORWARD PASSENGER/CREW DOOR).

1100

521103-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 1

(FWD PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

521201-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 2

(MID PASSENGER/CREW DOOR) SKIN,EXTERNAL SURFACE.

8500 

521203-01-01 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 2 (MID PASSENGER/CREW DOOR).

1100

521203-01-02 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 2 (MID PASSENGER/CREW DOOR).

6000 

521301-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

521303-01-01 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 4(AFT PASSENGER/CREW DOOR).

1100

AIRWORTHINESS LIMITATIONS SECTION

2 AIRWORTHINESS LIMITATIONS

 SECTION 2.1 - A340-200/300 AIRWORTHINESS LIMITATIONS

A340

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

521303-01-02 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 4 (AFT PASSENGER/CREW DOOR).

6000 

522201-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 3 

(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

522203-01-01 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).

1100

522203-01-02 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 3 (EMERGENCY/PASSENGER/ CREW DOOR).

6000 

R 523106-01-01 821CR

DOOR LOCKING HANDLE UNLOCKED

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR FR 20B BETWEEN BEAM 3 AND 4.

1060

524101-01-01 N/A DETAILED INSPECTION OF AVIONICS COMPARTMENT 

LOWER ACCESS DOOR SKIN, EXTERNAL SURFACE.

1040

R 528104-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR MAIN 

DOOR, CENTER FITTING AND SURROUNDING AREA (300 MM AROUND), LH/RH.

2650 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 528104-01-02 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR MAIN 

DOOR CENTER FITTING AND SURROUNDING AREA (300 MM AROUND), LH/RH.

8300 

528203-01-01 713 714 DETAILED INSPECTION OF NOSE LANDING GEAR 

FORWARD DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS ON FUSELAGE, LH/RH.

9600 

528303-01-02 753 754 DETAILED INSPECTION OF CENTER LANDING GEAR, MAIN 

DOOR FITTINGS, LH/RH.

2160

531110-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN 

FR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD, EXTERNAL SURFACE, LH/RH.

1850

531112-02-01 N/A DETAILED INSPECTION OF FUSELAGE STRUCTURE 

AROUND DOOR 1 (FORWARD PASSENGER/CREW DOOR), , EXTERNAL SURFACE, BETWEEN FR 13 AND FR 18 FROM LATERAL LONGITUDINAL LAP JOINT TO STR 9 AFT, LH/RH.

9000 

531118-01-01 713 714 121AL

121EL

GENERAL VISUAL INSPECTION OF GROUND SERVICES CONNECTING ACCESS DOORS CUTOUTS AND NOSE LANDING GEAR CUTOUT, BETWEEN FR 4 AND FR 19 ON LOWER FUSELAGE.

3100 

531120-01-02 713 714 GENERAL VISUAL INSPECTION OF NLG BAY INTERNAL 

STRUCTURE, NOSE LANDING GEAR WELL PANELS.

1400 

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A340

531131-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR16A JOINT AREA BETWEEN STRS 28 AND 30, LH/RH.NOTE : TASK TO BE PERFORMED IN CONJUCTION WITH TASK 531131-02-01

1850

531131-02-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 16A JOINT AREA BETWEEN STRS 28 AND 30, LH/RH. NOTE : TASK TO BE PERFORMED IN CONJUNCTION WITH TASK 531131-01-01.

1850

531133-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION AIR DUCTS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON FR12A AT STR 26 LEVEL LH/RH.

2260

531135-01-01 N/A SPECIAL DETAILED INSPECTION OF REAR LOWER CORNER 

OF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OF FR 10, EXTERNAL SURFACE, LH/RH

4850 

531136-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION CEILING PANELS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRS 12 AND 13 DOUBLER AREA AT CROWN CENTERLINE. 

1750

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A340

531140-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS, 831GALLEYS & TOILETS IF INSTALLED

SPECIAL DETAILED INSPECTION OF LATERAL FRAME 10 AT FLOOR LEVEL ATTACHMENT, ABOVE COCKPIT FLOOR, INTERNAL STRUCTURE, LH/RH.

1570

531141-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS

DETAILED INSPECTION OF LATERAL FR11, SPLICE ABOVE COCKPIT FLOOR LEVEL ATTACHMENT, INTERNAL STRUCTURE, LH/RH.

1760

531143-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION AIR DUCTSVACUUM PIPES

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING AT FR 14, LH/RH.

1660

531144-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGTOILET

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FR 14 AND CRUCIFORM FITTING, LH/RH. 

1660

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AIRWORTHINESS LIMITATIONS SECTION

A340

531154-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGSSLIDING WINDOWS OPENED

DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELD SIDE POST, INTERNAL STRUCTURE, LH/RH. 

1300

531161-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS

DETAILED INSPECTION OF PAX / CREW DOOR UPPER KEEL FITTING AT FR 18 FORWARD AND AFT FACE AT STGR 12 LEVEL, INTERNAL STRUCTURE, LH/RH.

1410

531175-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT JUNCTION BETWEEN FR 17 AND MACHINED STIFFENERS AT STRS 14/18/22/24, LH/RH. 

2270

531192-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FR 13 FORWARD FACE AND STR 9 FORWARD, AND FR 13 AFT FACE AND STR 12, LH/RH. 

2190

531194-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LININGS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, MACHINED STIFFENERS 14 AND 22 BETWEEN FR 17 AND FR 18, LH/RH.

2190

R 532101-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-

02

2200 

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A340

N 532101-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-

01

6900 

R 532114-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AROUND FORWARD CARGO COMPARTMENT DOOR CUTOUT AT UPPER AND LOWER CORNERS.

1080

O

6000

532114-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AROUND FORWARD CARGO COMPARTMENT DOOR CUTOUT AT UPPER AND LOWER CORNERS.

1080

O

2160

532114-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AROUND FORWARD CARGO COMPARTMENT DOOR CUTOUT AT UPPER AND LOWER CORNERS.

1300

532115-01-02 821 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL FRAMES (FR 20A AND FR 25A).

3500 

R 532117-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROM STR6 TO STR 26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-

02

1300

N 532117-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR18 AND FR 38 FROM STR6 TO STR 26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-

01

1300

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A340

R 532124-02-01 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

R 532124-02-02 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1380

R 532124-02-03 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1600

532124-02-04 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1600

N 532124-02-05 832 842 

SCUFF PLATE 

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. 

1600

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A340

R 532125-01-01 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNER, LH/RH.

1080

R 532125-01-02 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNER, LH/RH.

1380

R 532125-01-03 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNER, LH/RH.

1600

532125-01-04 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNER, LH/RH.

1600

N 532125-01-05 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNER, LH/RH. 

1600

532128-01-01 832 842 GENERAL VISUAL INSPECTION OF DOOR 2 (MID 

PASSENGER/CREW DOOR) STOP FITTINGS ON FR 33 AND FR 35A, LH/RH.

1400

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A340

532129-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING 

AREAS AT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTER 

LINE, EXTERNAL SURFACE.

2100

O

4200

532130-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AND VISIBLE PORTION OF WINDOW FORGINGS,- BETWEEN FR 18 AND FR 31,- BETWEEN FR 36 AND FR 38,FROM STR 18 TO STR 22, LH/RH.

2500

532138-01-01 821 131AG

DRAINMAST

DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL SURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37 AND FR 37.1, FROM STR 53 TO STR 54, LH ONLY.

2000

532142-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNA 

CUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTER LINE, EXTERNAL SURFACE.

2400

R 532143-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND GPS ANTENNA

CUT-OUTS BETWEEN- FR 35 AND FR 36 AND- FR 37 AND FR 37.1,ON CROWN CENTER LINE, EXTERNAL SURFACE.

2400

R 532144-01-01 832 842 

CEILING PANELS NOTE 1

DETAILED INSPECTION OF FRAMES AND STRINGER COUPLING AREA, BETWEEN FR 32 AND FR 34, FROM STR 9 TO STR 13 LH/RH, INTERNAL STRUCTURE.

2000

532145-01-01 N/A GENERAL VISUAL INSPECTION OF SKIN AT SHEAR TIE 

ATTACHMENTS BETWEEN- FR 19 AND FR 25,- FR 26.1 AND FR 37,- FR 37.2 AND FR 37.4,FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2280

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A340

532146-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 26 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2400

R 532147-01-01 821

CARGO COMPARTMENTFLOOR PANELSLININGSNOTE1

DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OF CARGO FLOOR ATTACHMENT FITTINGS,- FROM FR 20 TO FR 38 LH,- FROM FR 26 TO FR 38 RH,BETWEEN STR 34 AND STR 43.

2000

532148-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREA AT FR 31 FROM STR 9 TO STR 15 LH/RH, EXTERNAL SURFACE.

2400

532149-01-01 832 842

CEILING AND SIDE WALL PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE CIRCUMFERENTIAL SPLICE AT FR 26, FROM- STR 4 TO STR 6,- STR 12 TO STR 14 AND- STR 21 TO STR 22,LH/RH.

2400

532150-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 37.1.

2000

O

4000

532152-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AT SHEAR TIE 

ATTACHMENT BETWEEN FR 26 AND FR 37.1, FROM STR 13 TO STR 31 LH/RH, EXTERNAL SURFACE.

2000

O

4000

532153-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW 

VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32 AND FR 33, FROM STR 45 TO STR 49, LH ONLY.

1500

532154-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AT SPLOT LIGHT CUT-OUT,- BETWEEN FR 27 AND FR 28,- BETWEEN FR 30 AND FR 31,FROM STR 24 TO STR 26, LH/RH.

2000

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AIRWORTHINESS LIMITATIONS SECTION

A340

532155-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN DOUBLER AT 

PRESSURE RELIEF VALVE CUT-OUT, BETWEEN FR 24 AND FR 25, FROM STR 26 TO STR 30, LH ONLY.

2000

532156-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE LH/RH.

2000

O

4000

532157-01-01 832 842

SIDE WALL LININGINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR 15, LH/RH.

1500

532158-01-01 833 843

CEILING PANELSINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 38, FROM STR 13 TO CROWN CENTERLINE, LH/RH.

1500

O

9000

532158-02-01 833 843

CEILING PANELSINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTERLINE, LH/RH.

1500

O

9000

532159-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 1 ANTENNA 

CUT-OUT BETWEEN FR 22 AND FR 23, ON CROWN CENTER LINE, EXTERNAL SURFACE.

2400

532160-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND ATC 1+2 

ANTENNA CUT-OUT BETWEEN FR 24 AND FR 25, AND BETWEEN STR 2 AND STR 3, LH/RH, EXTERNAL SURFACE.

2400

532161-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND SATCOM(LG) 

ANTENNA CUT-OUT BETWEEN FR 26 AND FR 26.1 ON CROWN CENTER LINE, EXTERNAL SURFACE.

2400

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AIRWORTHINESS LIMITATIONS SECTION

A340

532162-01-01 831 841

OVERHEAD STOWAGECOMPARTMENT DOORMAINTENANCE DOORANTENNA

DETAILED INSPECTION OF SKIN AROUND SATCOM (45 DEGREE) ANTENNA CUT-OUT BETWEEN FR 26.1 AND FR 26.3 AND BETWEEN STR 12 AND STR 13, LH/RH, EXTERNAL SURFACE.

2400

532163-01-01 ANTENNA REAR FAIRING

COVER AND BRACKET

DETAILED INSPECTION OF SKIN AROUND SATCOM (HG) ANTENNA CUT-OUT BETWEEN FR 26.4 AND FR 27, ON CROWN CENTER LINE, EXTERNAL SURFACE.

2400

532165-01-01 831 841

CEILING PANELSLININGINSULATION .

SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 38.

1500

O

9000

532165-02-01 831 841

CEILING PANELSLININGINSULATION .

SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 AND FR 37.1.

1500

O

9000

N 532166-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-

02

4500 

N 532166-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-

01

6900 

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A340

R 533005-01-01 191AB 191AT 191BB

191CB 192AT 192BB192CB 197AT 197FB197GB 197HB 198AT198GB 198HB

DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING SEALING LIP ATTACHMENT FROM FR 37.1 TO FR 38 AND FROM FR 53.6 TO FR 56.

1520

O

10310

N 533005-01-02 191AB 191AT 191BB

191CB 192AT 192BB192CB 197AT 197FB197GB 197HB 198AT198GB 198HB

DETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRING SEALING LIP ATTACHMENT FROM FR 37.1 TO FR 38 AND FROM FR 53.6 TO FR 56.

1520

O

3050

R 533103-02-01 N/A DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, SKIN PANEL RIVETING ON FR 40 FROM STR 17 TO STR 19, LH/RH.

1510

O

10210

R 533104-01-02 ANTICOLLISION LIGHT: 

LENS 7LVADF: LENSES 2RP1 & SEAL AND 2RP2 & SEALPOST 49842: OBTURATOR OF AIRLINE IN-FLIGHT INFORMATION SERVICES ANTENNA CUTOUT.

DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN STRINGER 1 LH AND 1 RH 50MM AROUND:- UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 AND FR.49 AND BETWEEN FR.52 AND FR.53- AFIS ANTENNA CUTOUT BETWEEN FR.40 AND FR.40.1 (IF INSTALLED)

2530

O

5070

R 533105-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING AND AIR CONDITIONINGDUCTS.

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FASTENER HOLE AREA ABOVE STRINGER 28 AT FR 39.1 WEB JUNCTION ON HOIST FITTING, LH/RH.

1360

O

9210

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533106-01-01 N/A DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS AREA AT WINDOW FRAMES JUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR 22, FROM FRAME 38 TO 53.3, LH/RH.

2490

O

4990

R 533107-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING AND AIR CONDITIONINGDUCTS.

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE , FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STRINGER 29 LEVEL, LH/RH.

1830

O

12370

R 533107-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING AND AIR CONDITIONINGDUCTS.

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE , FRAMES 39 TO 39.2 WEB HOLE AREA JUST BELOW STRINGER 28 AND FASTENERS AREA AT FRAMES JUNCTION BELOW STRINGER 29 LEVEL, LH/RH.

2400

O

4810

R 533111-01-01 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FIRST FASTENERS ROW AREA ABOVE STR 39 BETWEEN FR 53.2 AND FR 53.3, LH/RH.

1000

O

6770

R 533113-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 TO ABOVE STR 24 LEVEL, LH/RH.

1720

O

11630

R 533113-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 TO ABOVE STR 24 LEVEL, LH/RH.

1230

O

8300

R 533113-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 TO ABOVE STR 24 LEVEL, LH/RH.

1500

O

3000

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AIRWORTHINESS LIMITATIONS SECTION

A340

533113-01-04 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENER ROWS AT FR 47 FROM BELOW STR 22 TO ABOVE STR 24 LEVEL, LH/RH.

1230

O

8320

R 533114-01-01 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZER STRS 20 TO 23, LH/RH.

1300

 O

8770

R 533114-01-02 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZER STRS 20 TO 23, LH/RH.

1500

O

3000

R 533115-01-01 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 , LH/RH.

1700

O

11500

R 533115-01-02 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 , LH/RH.

1200

O

8120

R 533115-01-03 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 , LH/RH.

1570

O

3150

533115-01-04 251XW 252XW

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 , LH/RH.

1200

O

8100

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533116-01-01 753 754

FASTENERS

SPECIAL DETAILED INSPECTION OF CENTER LANDING GEAR TRUNNION FITTING, BEAM Y = 450, FIRST 2 FASTENER HOLES AT ATTACHMENT TO OUTER SKIN, LH/RH.

7400 

O

2850

R 533125-01-02 734 744 753

754

GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENT AREA OF THE CENTER LANDING GEAR TRUNNION FITTINGS.

1500 

O

1010

N 533125-01-03 734 744 753

754

GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENT AREA OF THE CENTER LANDING GEAR TRUNNION FITTINGS.

1500 

O

3000 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 533126-01-02 734 744 753

754

GENERAL VISUAL INSPECTION OF SKIN PANEL AREA AROUND CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

3800 

O

2620

R 533126-01-03 734 744 753

754

GENERAL VISUAL INSPECTION OF SKIN PANEL AREA AROUND CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

3300 

O

2280

R 533126-01-04 734 744 753

754

GENERAL VISUAL INSPECTION OF SKIN PANEL AREA AROUND CENTER LANDING GEAR AND MAIN LANDING GEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

4600 

O

9250 

R 533127-01-01 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47

DETAILED INSPECTION OF AREA AROUND AIR CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

3800 

O

2620

D 533127-01-02 TASK DELETED IN ALI ISSUE 11

R 533127-03-01 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47

DETAILED INSPECTION OF AREA AROUND AIR CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

3300 

O

2280

R 533127-03-02 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47

DETAILED INSPECTION OF AREA AROUND AIR CONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.

4600 

O

9250 

D 533127-03-03 TASK DELETED IN ALI ISSUE 11

R 533132-02-02 753 754 SPECIAL DETAILED INSPECTION OF CLG TRUNNION 

FITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARD FLANGES RADIUS, LH/RH.

2070

O

4150

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533134-02-01 753 754

SPHERICAL BEARINGACTUATOR DISCONNECTED

SPECIAL DETAILED INSPECTION OF ATTACH FITTING FOR CLG ACTUATOR AND ITS ATTACHMENT TO THE CENTER LINE STIFFENER AT FR 53.2.

1430

O

9670

N 533134-02-02 753 754

SPHERICAL BEARINGACTUATOR DISCONNECTED

SPECIAL DETAILED INSPECTION OF ATTACH FITTING FOR CLG ACTUATOR AND ITS ATTACHMENT TO THE CENTER LINE STIFFENER AT FR 53.2.

1430

O

2860

R 533139-01-01 753 754 755

756

SPECIAL DETAILED INSPECTION OF VERTICAL BEAM AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG ACTUATOR FITTING UPPER END.

1525

O

 1029

R 533139-01-03 753 755 754

756

SPECIAL DETAILED INSPECTION OF VERTICAL BEAM AT Y = 0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLG ACTUATOR FITTING UPPER END.

2060

O

4120

R 533145-01-02 197AT 197HB 198AT

198HB

SPECIAL DETAILED INSPECTION OF FUSELAGE LONGITUDINAL BUTT JOINT AT STR 31 LEVEL FROM FR 53.3 TO FR 54, LH/RH.

1300

O

2600

R 533154-01-01 CABIN FLOOR PANELS

GALLEYS AND TOILETS (IF INSTALLED)

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1, LH/RH.

1300

O

8800

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533154-01-03 CABIN FLOOR PANELS

GALLEYS AND TOILETS (IF INSTALLED)

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RIVET ROWS AT SHEAR PANELS AND LONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1, LH/RH.

2000

O

4000

R 533162-01-01 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR 

BAY, LOWER FLANGE OF GANTRY Y = 1456, 40 FASTENERS FORWARD AND AFT OF FR 48 DATUM, LH/RH.

1620

O

10960

R 533163-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY , 

CANTED DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 0 TO Y = 450, LH/RH.

9200 

O

6230

R 533164-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY , 

CANTED DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO Y = 1959, LH/RH.

1690

O

11410

R 533164-01-02 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY , 

CANTED DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO Y = 1959, LH/RH.

2130

O

4260

R 533164-01-03 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY , 

CANTED DIAPHRAGMS AND CANTED DIAPHRAGMS JUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48 FROM Y = 450 TO Y = 1959, LH/RH.

1780

O

12000

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533165-01-01 251MG 251SG 252MG

252SGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION GALLEYS AND TOILETS (IF INSTALLED).

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FR 48 TO FR 53.1, HORIZONTAL LEG AT STRINGER PASSAGE, LH/RH.

1190

O

8030

R 533180-01-01 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS BETWEEN FR 53.6 AND FR 53.7,EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

1500

O

10000

R 533180-01-02 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL 

SPLICE AND STRINGER COUPLING AREAS BETWEEN FR 53.6 AND FR 53.7,EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

1500

O

10000

R 533181-01-01 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

1600

O

8000

533181-01-02 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

1600

O

3200

533181-01-03 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

1300

O

9570

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AIRWORTHINESS LIMITATIONS SECTION

A340

533184-01-01 N/A DETAILED INSPECTION OF SKIN AT SHEAR TIE 

ATTACHMENTS BETWEEN FR 53,4 AND FR 53,9 FROM STRINGER 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2280

O

4800

533192-01-01 834 844 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS 

OF DOOR 3 EMERGENCY/PASSENGER/CREW DOOR) AT FR 53.5 AND 53.7 A, LH/RH.

1400

533193-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

(INCLUDING DOOR 3 CUTOUT) BETWEEN FR 53.3 AND FR 54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTER LINE, EXTERNAL SURFACE, LH/RH.

3600 

R 533194-01-01 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1080

O

7800

R 533194-01-02 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1800

O

13000

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533194-01-03 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1800

O

13000

R 533194-01-04 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1080

O

7800

R 533194-01-05 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1300

O

10100

R 533194-01-06 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS LH/RH.

1080

O

2150

R 533194-01-09 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

1080

O

2160

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533195-02-01 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

O

7800

R 533195-02-02 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1800

O

13000

R 533195-02-03 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1800

O

13000

R 533195-02-04 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

O

7800

R 533195-02-05 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1300

O

10100

R 533195-02-06 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH

1080

O

2150

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 533195-02-09 834 844 

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

O

2150

R 534102-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 58 FROM STR 13 TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

8290 

O

5800

534102-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 58 FROM STR 13 TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

2200

O

4400

534104-01-01 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 22

1275

O

9000

R 534104-01-02 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 22

6970 

O

4880

R 534104-01-03 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM:- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 22

9920 

O

6940

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

534104-01-05 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 22

1275

O

2550

534104-01-06 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 22

1300

O

10100

R 534105-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 72 FROM STR 13 TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

1300

O

9200

534105-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 72 FROM STR 13 TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

2400

O

4800

534107-01-01 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

1275

O

9750

534107-01-03 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

1275

O

2550

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

534107-01-04 833 843

CEILING PANELSOVERHEAD STOWAGE BINSINSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

1300

O

11630

534108-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 76 FROM STRINGER 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2280

O

4560

534110-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN 

CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM STRINGERS 6 TO 13 LH/RH, EXTERNAL SURFACE

2280

O

4560

534120-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

PART OF WINDOW FORGING BETWEEN FR 53.8 AND FR 73 AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNAL SURFACE.

2280

O

4560

534122-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AT 

SHEAR TIE ATTACHMENTS- BETWEEN FR 55 AND FR 57.4,- BETWEEN FR 59 AND FR 71 AND- BETWEEN FR 73 AND FR 79,FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE EXCLUDING AREA COVERED BY FIN TO FUSELAGE FAIRING.

2280

O

4560

R 534124-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR 54 AND 80 FROM STR6 TO STR 26 LH/RH, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-02-01.

1300

R 534124-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 

54 AND 80 FROM STR6 TO STR 26 LH/RH, EXTERNAL SURFACE.

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-01-

1300

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 534126-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH TO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR 54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-02-01

2200 

R 534126-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RH TO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR 54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-01-01

6900 

R 534131-01-01 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

1080

534131-01-02 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

1300

O

10260

N 534131-01-03 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

1080

R 534132-02-01 833 843

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

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AIRWORTHINESS LIMITATIONS SECTION

A340

534132-02-02 833 843

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1300

O

10260

N 534132-02-03 833 843 

SCUFF PLATE 

SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.

1080

534135-01-01 833 843 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS 

OF DOOR 4 (AFT PASSENGER /CREW DOOR) AT FR 73A AND FR 75A, LH/RH.

1400

R 534136-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN OF 

AFT CARGO COMPARTMENT DOOR CUT-OUT AT UPPER REAR AND LOWER FORWARD CORNERS, EXTERNAL SURFACE.

1010

O

6780

534137-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER AND LOWER CORNERS, EXTERNAL SURFACE.

1080

O

6600

534137-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER AND LOWER CORNERS, EXTERNAL SURFACE.

1080

O

2160

534137-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER AND LOWER CORNERS, EXTERNAL SURFACE.

1300

O

8660

534139-01-02 822 GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A AND FR 65) AS FAR AS VISIBLE.

3500 

534140-02-02 822 GENERAL VISUAL INSPECTION OF LOCK FITTINGS BUSHES 

FOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEEN FR 59A AND FR 65.

7500 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 534143-01-01 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS EXTERNAL SURFACE.

9700 

O

7170

534143-01-03 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS EXTERNAL SURFACE.

1020

O

2400

534143-01-04 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS EXTERNAL SURFACE.

1300

O

9570

R 534144-02-01 823

SCUFF PLATE

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.

9700 

O

7170

R 534144-02-02 823

SCUFF PLATE

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.

1020

O

2400

R 534144-02-03 823

SCUFF PLATE

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.

1300

O

9570

534146-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGO 

COMPARTMENT DOOR STOP FITTINGS AT 10 POSITIONS AT FR 67 AND FR 69.

1000

534148-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA 

CUT-OUT BETWEEN FR 56 AND FR 57 FROM STRINGERS 2 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2280

O

4560

534149-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 67 AND FR 69) AS FAR AS VISIBLE.

3500 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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A340

R 534150-01-01 823 

LINING NOTE 1

DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OF CARGO FLOOR ATTACHMENT FITTINGS,- FROM FR 54 TO FR 64 LH AND FROM FR 54 TO FR 58 RH, BETWEEN STR 39 AND STR 45- FROM FR 65 TO FR 69 LH, BETWEEN STR 41 AND STR 50.

2000

534154-01-01 833 843

LINING INSULATION

DETAILED INSPECTION OF INTERNAL STRUCTURE OF TORSION BOX, INCLUDING SKIN AND SPLICE PLATE, BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 AND FR 76, LH/RH.

2000

534155-01-01 833 843

LINING INSULATION

SPECIAL DETAILED INSPECTION OF TORSION BOX LONGITUDINAL BEAM ADJACENT TO RUN OUT OF CORNER DOUBLER BETWEEN FR 73A AND FR 74, LH/RH.

2000

534156-01-02 822

LININGCARGO FLOOR PANELSINSULATION

DETAILED INSPECTION OF INTERNAL STRUCTURE BELOW AFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59 AND FR 67, FROM CARGO FLOOR LEVEL TO STR 47 RH.

1500

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

534166-01-01 ANTENNA SPECIAL DETAILED INSPECTION OF SKIN AROUND VHF 2 

ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 56 TO STR 57, RH.

1300

N 534177-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR 54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINE EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-

01

4500 

N 534177-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 

54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINE EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-01-

01

6900 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

535103-01-02 312AR DETAILED INSPECTION OF REAR PRESSURE BULKHEAD 

AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STRINGERS 26 LH/RH AND CROWN CENTERLINE.

1650

535104-02-01 312AR GENERAL VISUAL INSPECTION OF REAR PRESSURE 

BULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STRINGERS 26 LH/RH AND BOTTOM CENTER LINE.

3600 

535109-01-01 313AL

HINGE ARMS

SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER HINGE SUPPORT MEMBERS AND UPPER AND LOWER ATTACHMENT LUGS OF FR 91, LH/RH.

2000

D 545104-01-01 TASK DELETED IN ALI ISSUE 11D 545104-01-02 TASK DELETED IN ALI ISSUE 11D 545104-01-06 TASK DELETED IN ALI ISSUE 11R 545142-01-01 453CL 453CR 463CL

463CR 473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

1300

O

8770

545142-01-02 453CL 453CR 463CL

463CR 473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

1300

O

2600

545142-01-03 453CL 453CR 463CL

463CR 473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

1300

O

8800

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 545146-01-01 415AL 416AR 417AL 

418AR 425AL 426AR 427AL 428AR 435AL 436AR 437AL 438AR 445AL 446AR 447AL 448AR 453AL 453AR 463AL 463AR 473AL473AR 483AL 483AR

DETAILED INSPECTION OF PYLON LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4.

2000

O

8000

N 545146-01-02 415AL 416AR 417AL 

418AR 425AL 426AR 427AL 428AR 435AL 436AR 437AL 438AR 445AL 446AR 447AL 448AR 453AL 453AR 463AL 463AR 473AL473AR 483AL 483AR

DETAILED INSPECTION OF PYLON LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4.

3000

O

6000

R 545166-01-01 452DR 452EL 452FR 

462DL 462FR 462GR 472ER 472FL 472GL 482DL 482ER 482FL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1190

O

8030

545166-01-02 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1300

O

2600

R 545166-01-03 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1280

O

8630

545166-01-04 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1300

O

8800

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 545166-01-05 452DR 452FR 452GL 

462DL 462FR 462GR 472ER 472FL 472GL 482FL 482GL 482HR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1190

O

8030

R 545166-01-06 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUGS AT RIB 8.

1190

O

8030

R 545168-01-01 452DR 452EL 452FR 

462DL 462FR 462GR 472ER 472FL 472GL 482DL 482ER 482FL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1190

O

8030

545168-01-02 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1300

O

2600

R 545168-01-03 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1280

O

8630

545168-01-04 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1300

O

8800

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Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 545168-01-05 452DR 452FR 452GL 

462DL 462FR 462GR 472ER 472FL 472GL 482FL 482GL 482HR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1190

O

8030

R 545168-01-06 452KL 452KR 452MR 

462DL 462FR 462GR 472ER 472FL 472GL 482ML 482MR 482NL

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 8.

1190

O

8030

N 545174-01-01 454BL 454BR 464BL 

464BR 474BL 474BR 484BL 484BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUG AND LINKS AT RIB 14.

2000

O

8000

N 545174-01-02 454BL 454MR 464KL 

464KR 474KL 474KR 484NL 484NR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUG AND LINKS AT RIB 14.

3000

O

6000

N 545174-01-04 454BL 454BR 464KL 

464KR 474KL 474KR 484BL 484BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUG AND LINKS AT RIB 14.

2000

O

8000

N 545174-01-05 454BL 454MR 464KL 

464KR 474KL 474KR 484NL 484NR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LUG AND LINKS AT RIB 14.

2000

O

8000

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 545180-02-02 ENGINE, LINKS, BOLTS, 

SLEEVES454NR 454QL 464JL 464JR 474JL 474JR 484PL 484PR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

2130

O

4260

R 545180-02-03 ENGINE, LINKS, BOLTS, 

SLEEVES454NR 454QL 464JL 464JR 474JL 474JR 484PL 484PR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

1200

O

8120

R 545180-02-04 ENGINE, LINKS, BOLTS, 

SLEEVES454FL 454FR 464FL 464FR 474FL 474FR 484FL 484FR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

1330

O

8960

R 545180-02-05 ENGINE, LINKS, BOLTS, 

SLEEVES454FL 454FR 464JL 464JR 474JL 474JR 484FL 484FR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

1330

O

8960

R 545180-02-06 ENGINE, LINKS, BOLTS, 

SLEEVES454NR 454QL 464JL 464JR 474JL 474JR 484PL 484PR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

1330

O

8960

N 545180-02-07 ENGINE, LINKS, BOLTS, 

SLEEVES454NR 454QL 464JL 464JR 474JL 474JR 484PL 484PR

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3 PLACES PER PYLON).

1240

O

8370

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 551016-01-01 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH.

2830

O

11330

R 571102-01-01 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING AND AIR CONDITIONINGDUCTS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 LEVEL, LH/RH.

1330

O

8980

R 571102-01-02 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING AND AIR CONDITIONINGDUCTS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FASTENER ON FRAME 40 FRONT FITTING AT STRINGER 38 LEVEL, LH/RH.

1690

O

3390

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571103-01-01 191HB 192HB 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING ANDAIR CONDITIONINGDUCTSFASTENER REMOVAL

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- ROTOTEST INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-01.

1310

O

8840

R 571103-01-02 191HB 192HB 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING ANDAIR CONDITIONINGDUCTSFASTENER REMOVAL

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- ROTOTEST INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-02.

1300

O

2600

R 571103-02-01 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING ANDAIR CONDITIONINGDUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- HIGH FREQUENCY EDDY CURRENT INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-01.

1310

O

8840

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571103-02-02 821

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION LINING ANDAIR CONDITIONINGDUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- HIGH FREQUENCY EDDY CURRENT INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-02.

1300

O

2600

R 571104-01-01 191FB 192GB 192JB

821131CX 131DX 132CX 132DX FASTENER TO BE REMOVEDINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENER BETWEEN STR 38 AND STR 39, LH/RH.

1300

O

8810

R 571104-01-02 191FB 192GB 192JB

821131CX 131DX 132CX 132DX FASTENER TO BE REMOVEDINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENER BETWEEN STR 38 AND STR 39, LH/RH.

1110

O

7530

R 571104-01-03 191FB 192GB 192JB

821131CX 131DX 132CX 132DX FASTENER TO BE REMOVEDINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENER BETWEEN STR 38 AND STR 39, LH/RH.

8000 

O

5460

R 571104-01-04 191FB 192GB 192JB

821131CX 131DX 132CX 132DX FASTENER TO BE REMOVEDINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENER BETWEEN STR 38 AND STR 39, LH/RH.

1180

O

7980

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571104-01-05 191FB 192 GB 192JB

821131CX 131DX 132CX 132DX FASTENER TO BE REMOVEDINSULATION

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF FASTENER BETWEEN STR 38 AND STR 39, LH/RH.

1700

O

3410

R 571107-01-01 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN STRINGERS 20 AND 21, LH/RH.

1400

O

9450

R 571107-01-02 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN STRINGERS 20 AND 21, LH/RH.

1290

O

8730

R 571107-01-03 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN STRINGERS 20 AND 21, LH/RH.

1890

O

3780

571107-01-04 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEEN STRINGERS 20 AND 21, LH/RH.

1360

O

9200

R 571108-01-01 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS.

1280

O

8700

R 571108-01-03 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS.

1730

O

11740

R 571108-01-04 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS.

2060

O

4120

571108-01-05 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS.

1920

O

13000

R 571114-01-01 147AZ 734 148AZ

744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28.

1350

O

9150

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571114-01-03 147AZ 734 148AZ

744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28.

1080

O

7290

R 571114-01-04 147AZ 734 148AZ

744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28.

1280

O

2560

R 571116-01-01 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN STRINGERS 21 AND 22, AT Y =-567.5.

1400

O

9450

R 571116-01-02 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN STRINGERS 21 AND 22, AT Y =-567.5.

1290

O

8730

R 571116-01-03 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN STRINGERS 21 AND 22, AT Y =-567.5.

1890

O

3780

571116-01-04 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREA BETWEEN STRINGERS 21 AND 22, AT Y =-567.5.

1360

O

9200

R 571118-01-01 FAIRING PANELS 

BETWEEN FR.44 AND FR.47

SPECIAL DETAILED INSPECTION OF THE CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 27 AND STR 28.

1400

O

9450

D 571118-01-02 TASK DELETED IN ALI ISSUE 11

R 571118-01-03 FAIRING PANELS 

BETWEEN FR.44 AND FR.47

SPECIAL DETAILED INSPECTION OF THE CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 27 AND STR 28.

1290

O

8730

D 571118-01-04 TASK DELETED IN ALI ISSUE 11

R 571118-01-05 FAIRING PANELS 

BETWEEN FR.44 AND FR.47

SPECIAL DETAILED INSPECTION OF THE CENTER WING BOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 27 AND STR 28.

1890

O

3780

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

D 571118-01-06 TASK DELETED IN ALI ISSUE 11

571118-01-07 192QB 195CB SPECIAL DETAILED INSPECTION OF THE CENTER WING 

BOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180 BETWEEN STR 27 AND STR 28.

1360

O

9200

R 571122-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y = 953 TO Y = 1959, LH/RH.

1380

O

9340

R 571122-01-03 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y = 953 TO Y = 1959, LH/RH.

2010

O

4030

571122-01-04 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

EXTERNAL STRUCTURE, FASTENER AREA AT REAR SPAR LOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION, FROM Y = 953 TO Y = 1959, LH/RH.

1460

O

9900

R 571123-01-01 251AG 251FG 252AG

252FGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.

8800 

O

6000

R 571123-01-02 251AG 251FG 252AG

252FGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.

8600 

O

5820

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571123-01-03 251AG 251FG 252AG

252FGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.

1700

O

3410

N 571123-01-04 251AG 251FG 252AG

252FGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.

1960

O

13270

N 571123-01-05 251AG 251FG 252AG

252FGINSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE INSPECTION 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.

1820

O

12340

R 571125-01-01 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND FR 47 LOWER CORNER FITTING, LH/RH.

1420

O

9600

R 571125-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR AFT FACE, FASTENERS AREA BETWEEN Y=2219 AND FR 47 LOWER CORNER FITTING, LH/RH.

2070

O

4150

R 571126-01-01 734 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER.

1180

O

8000

R 571126-01-02 734 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER.

1480

O

2970

R 571133-01-02 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES).

1440

O

9770

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 571133-01-03 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES).

2110

O

4230

571133-01-04 147AZ 734 148AZ

744

DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES).

1530

O

10300

571145-01-01 734 744 147AZ 148AZ

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF CWB, INTERNAL STRUCTURE, RIB1 LOWER TEE FITTING INBOARD FLANGE; FASTENERS IN RADIUS AREA AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH.

1870

O

12600

R 571146-02-01 191QB 192QB

191HB 192HB

SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH.

1740

O

11790

R 571146-02-02 191QB 192QB

191HB 192HB

SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH.

1150

O

7780

R 571146-02-03 191QB 192QB

191HB 192HB

SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH.

1360

O

2730

571146-02-04 191QB 192QB

191HB 192HB

SPECIAL DETAILED INSPECTION OF CENTER WING BOX LOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20, STR21 AND STR25 TO STR29, LH/RH.

1180

O

8000

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 571149-01-02 191HB 192HB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH.

1290

O

8740

R 571149-01-03 191HB 192HB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

LOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGE FROM FR 40 DATUM TO STR 1 LEVEL, LH/RH.

1690

O

3380

R 571152-01-01 147AZ 148AZ

734 744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE, RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE AT FASTENERS 3 TO 12, LH/RH.

1520

O

10320

N 571153-01-01 147AZ 148AZ 

734 744SEALANT REMOVAL

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.

8900 

O

6050

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 571153-01-02 147AZ 148AZ 

734 744 SEALANT REMOVAL

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.

1360

O

9280

N 571153-01-03 147AZ 148AZ 

734 744 SEALANT REMOVAL

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.

1190

O

8080

N 571153-01-04 147AZ 148AZ 

734 744 SEALANT REMOVAL

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.

1600

O

3200

R 571153-01-05 147AZ 148AZ 

734 744SEALANT REMOVAL

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OF GUSSET INSTALLED ON LOWER L FITTING AT CROSSING AREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER L FITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.

1710

O

11600

N 571162-01-01 191HB 192HB SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING, 

TWO FASTENERS HOLES AT STIFFENER 1 LEVEL, LH/RH.

1360

O

9220

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

N 571163-01-01 191HB 192HB SPECIAL DETAILED INSPECTION OF FRAME 40 NODE, 

FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAM FITTING AND LOWER PANEL, LH/RH.

1100

O

7470

R 571165-01-01 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR, FILLET RADIUS FROM Y=1959 TO Y=2219 AND FROM Z=-1859.6 TO Z=-2073, LH/RH.

1120

O

7560

R 571165-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

REAR SPAR, FILLET RADIUS FROM Y=1959 TO Y=2219 AND FROM Z=-1859.6 TO Z=-2073, LH/RH.

1010

O

6820

N 572004-01-02 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING. 

1350

O

7730

R 572004-01-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY MAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING. 

2170

O

4350

D 572004-01-05 TASK DELETED IN ALI ISSUE 11

N 572006-02-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWER 

SURFACE MAIN LANDING GEAR REINFORCING PLATE.

2450

O

4900

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

N 572006-02-07 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWER 

SURFACE MAIN LANDING GEAR REINFORCING PLATE.

1520

O

8690

N 572006-02-08 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWER 

SURFACE MAIN LANDING GEAR REINFORCING PLATE.

1440

O

8260

N 572007-01-02 464GL 464GR 531AB

474GL 474GR 631AB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD PYLON FAIRING.

1350

O

7730

R 572007-01-03 464GL 464GR 531AB

474GL 474GR 631AB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARD PYLON FAIRING.

2170

O

4350

N 572010-02-01 541AB 541BB 541CB 541DB 

541EB 541FB 641AB 641BB 641CB 641DB 641EB 641FB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND ACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10 AND 11-12.

1500

O

8590

N 572012-01-01 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING PLATE.

1810

O

10330

N 572012-01-04 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLON REINFORCING PLATE.

1870

O

10710

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

N 572013-01-01 464AL 464AR 464BL 464BR 

464FL 464FR 464GL 464GR 464HL 474AL 474AR 474BL 474BR 474FL 474FR 474GL 474GR 474HL

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.

1530

O

8710

N 572013-01-03 464AL 464GL 464GR 464HL 

464JL 464JR 464KL 464KR 464M 474AL 474GL 474GR 474HL 474JL 474JR 474KL 474KR 474MR

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.

1530

O

8710

N 572013-01-05 464AL 464GL 464GR 464HL 

464JL 464JR 464KL 464KR 464M 474AL 474GL 474GR 474HL 474JL 474JR 474KL 474KR 474MR

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREA COVERED BY INBOARD PYLON FAIRING, EXCLUDING AREA COVERED BY PYLON REINFORCING PLATE AND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.

1860

O

10620

N 572014-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE SPANWISE SKIN JOINTS AT STR 13 AND STR 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BY FAIRINGS.

1550

O

8840

N 572015-02-05 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND RIB 12.

1680

O

9570

R 572016-02-01 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4.

1390

O

7950

N 572016-02-02 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4.

1800

O

10290

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

572016-02-03 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4.

2930

O

5860

N 572016-02-05 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4.

1860

O

10510

R 572017-01-05 541AB 641AB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

ROOT JOINT FITTINGS ON STR 13 AND STR 20.

1030

O

5920

R 572018-01-01 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 AND STR 20 BETWEEN RIB 5 AND RIB 7.

1160

O

6650

N 572018-01-02 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 AND STR 20 BETWEEN RIB 5 AND RIB 7.

1810

O

10350

N 572018-01-03 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 AND STR 20 BETWEEN RIB 5 AND RIB 7.

1880

O

10750

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
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AIRWORTHINESS LIMITATIONS SECTION

A340

R 572019-01-01 541EB 541FB 541GB

641EB 641FB 641GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.

1160

O

6650

N 572019-01-02 541EB 541FB 541GB

641EB 641FB 641GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.

1810

O

10350

N 572019-01-03 541EB 541FB 541GB

641EB 641FB 641GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.

1880

O

10750

N 572019-01-06 541EB 541FB 541GB

641EB 641FB 641GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15 AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.

1850

O

10470

N 572021-01-01 474FL 474FR 474GL 474GR 

464FL 464FR 464GL 464GR 531AB 631AB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 AND STR 20 IN AREAS COVERED BY INBOARD PYLON FAIRING AND FLAP TRACK 2 FAIRING.

1550

O

8840

N 572021-01-04 464GL 464GR 464JL 464JR 

474GL 474GR 474JL 474JR 531AB 631AB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STR 13 AND STR 20 IN AREAS COVERED BY INBOARD PYLON FAIRING AND FLAP TRACK 2 FAIRING.

1550

O

8840

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

N 572022-01-01 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE HOT FUEL RECIRCULATION HOLE IN RIB BAY 10-11, FROM STR 6 TO STR 7.

1680

O

9570

N 572023-02-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 

STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.

1810

O

10330

N 572023-02-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 

STRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDING GEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.

1870

O

10710

R 572027-01-01 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB 1 AND RIB 9.

1160

O

6640

R 572029-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 12.

1660

O

8620

572029-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 12.

2350

O

4700

N 572029-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 AND RIB 12.

1620

O

8430

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 572030-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 9 AND RIB 11.

5600 

O

2930

R 572030-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 9 AND RIB 11.

8400 

O

4350

R 572030-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 9 AND RIB 11.

1180

O

2370

R 572032-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

9700 

O

5020

R 572032-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

9200 

O

4790

R 572032-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

1300

O

2600

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

572032-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

1570

O

7230

N 572032-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7.

1600

O

7660

R 572033-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR.

1790

O

9310

N 572033-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR.

1990

O

10300

572033-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR.

2820

O

5640

R 572034-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEEN RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13.

9800 

O

5110

R 572034-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEEN RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13.

1330

O

6930

572034-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEEN RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13.

1780

O

3560

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

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AIRWORTHINESS LIMITATIONS SECTION

A340

572034-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEEN RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13.

1540

O

7110

N 572034-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEEN RIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19 BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS 11 AND 13.

1570

O

7530

R 572035-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TO RIB 8.

9000 

O

4680

R 572035-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TO RIB 8.

1000

O

5210

572035-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TO RIB 8.

1300

O

2600

R 572036-01-01 541AB 541AZ 541BZ

641AB 641AZ 641BZ

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS.

1610

O

8350

R 572036-01-02 541AB 541AZ 541BZ

641AB 641AZ 641BZ

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS.

1540

O

7980

572036-01-03 541AB 541AZ 541BZ

641AB 641AZ 641BZ

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR SPARS.

2140

O

4280

R 572039-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO RIB 9 AND FROM RIB 11 TO RIB 12.

1610

O

8350

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572039-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO RIB 9 AND FROM RIB 11 TO RIB 12.

1680

O

8730

572039-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO RIB 9 AND FROM RIB 11 TO RIB 12.

2310

O

4620

R 572040-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 AND RIB 13.

1300

O

6760

R 572040-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 AND RIB 13.

1450

O

7510

572040-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 AND RIB 13.

1940

O

3880

R 572046-01-01 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

5800 

O

3320

R 572046-01-02 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

8500 

O

4890

572046-01-03 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

1250

O

2500

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572046-01-04 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

1380

O

6220

N 572046-01-05 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

1300

O

7030

N 572047-01-01 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.

1910

O

10870

572047-01-02 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.

2720

O

5440

572047-01-03 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.

1910

O

8610

N 572047-01-04 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.

1750

O

9980

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572047-01-05 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1 AND RIB 7.

1800

O

9710

R 572050-01-01 573DB 673DB

FLAPS EXTENDED

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

1050

O

6010

R 572050-01-02 573DB 673DB

FLAPS EXTENDED

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

1210

O

6930

R 572050-01-03 573DB 673DB

FLAPS EXTENDED

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

1540

O

3090

R 572051-01-02 FLAPS EXTENDED

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.

1210

O

6890

R 572051-01-03 FLAPS EXTENDED

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.

1250

O

7150

572051-01-04 FLAPS EXTENDED

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.

1880

O

3760

R 572052-01-01 541AB 541BB 541BZ

541CZ 641AB 641BB641BZ 641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 

INCLUDING TOP AND BOTTOM FLANGES.

9100 

O

5220

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572052-01-02 541AB 541BB 541BZ

541CZ 641AB 641BB641BZ 641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.

8700 

O

4970

572052-01-03 541AB 541BB 541BZ

541CZ 641AB 641BB641BZ 641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.

1300

O

2600

572052-01-04 541AB 541BB 541BZ

541CZ 641AB 641BB641BZ 641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.

1650

O

7470

N 572052-01-05 541AB 541BB 541BZ

541CZ 641AB 641BB641BZ 641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGES.

1560

O

8430

R 572054-01-05 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.

1710

O

7710

R 572054-01-06 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.

1130

O

6470

R 572054-01-07 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.

1350

O

7700

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572054-01-08 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.

1610

O

8700

R 572063-01-01 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

1040

O

5970

N 572063-01-02 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

1770

O

10110

572063-01-05 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

1450

O

6550

N 572063-01-06 541AB 541BB 541CB

541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

1370

O

7410

R 572064-01-01 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10.

1040

O

5970

N 572064-01-02 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10.

1790

O

10220

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572065-01-01 522DB 522EB 622DB

622EB

DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12.

1350

O

7680

R 572065-01-02 522DB 522EB 622DB

622EB

DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12.

1210

O

6890

572065-01-03 522DB 522EB 622DB

622EB

DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE SPAR JOINT PLATE AT RIB 12.

2240

O

4480

D 572068-01-01 TASK DELETED IN ALI ISSUE 11

572068-01-04 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

1960

O

8860

N 572068-01-05 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

1850

O

10020

R 572073-01-01 541FB 541GB 641FB

641GB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

1220

O

6910

N 572073-01-02 541FB 541GB 641FB

641GB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

1410

O

7940

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572073-01-03 541FB 541GB 641FB

641GB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

2490

O

4980

R 572081-01-01 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

1060

O

6030

R 572081-01-02 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.NOTE: TASK APPLICABLE IF MOD 43021 CARRIED OUT BY RETROFIT SOLUTION

1390

O

7930

R 572081-01-03 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

1310

O

7500

572081-01-04 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

2070

O

4140

R 572082-01-01 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

1180

O

6770

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572082-01-02 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

1440

O

8240

R 572082-01-03 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

1250

O

7170

572082-01-04 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

2210

O

4420

572082-01-05 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

1800

O

8130

N 572082-01-06 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

1700

O

9190

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572084-01-05 541AB 641AB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR11, STR14, STR18 TO STR20 AND AT STR23 TO STR28, LH/RH.

1600

O

10800

R 572093-01-01 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-01

9600 

O

5490

R 572093-02-01 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-01

9600 

O

5490

R 572094-01-01 541EB 541FB 541GB

641EB 641FB 641GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 20 BETWEEN RIB 9 AND RIB 12.

1160

O

6640

R 572095-01-01 541BB 541CB 641BB

641CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

1160

O

6650

N 572095-01-02 541BB 541CB 641BB

641CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

1810

O

10350

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572095-01-03 541BB 541CB 641BB

641CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

1880

O

10750

N 572102-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE IN REGION OF RIB 27 SKIN JOINT AREA.

1750

O

9990

N 572109-02-01 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

1750

O

9970

N 572109-02-02 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

1680

O

9600

572109-02-03 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

2850

O

5700

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572110-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

1530

O

8740

N 572110-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

1550

O

8840

572110-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

2470

O

4940

N 572111-01-01 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

1530

O

8740

N 572111-01-02 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

1550

O

8840

572111-01-03 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

2470

O

4940

N 572116-01-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND STRINGER 20 BETWEEN RIB 12 AND RIB 27, AS FAR AS VISIBLE.

1550

O

8840

N 572117-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 

AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 

AND 5.

1550

O

8840

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572121-01-01 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

1380

O

7880

N 572121-01-02 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

1530

O

8730

R 572121-01-03 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

2450

O

4900

R 572122-01-01 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642FB642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAYS 26 TO 28 AND STRINGERS 15 AND 18.

1380

O

7880

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572122-01-02 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642FB642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAYS 26 TO 28 AND STRINGERS 15 AND 18.

1530

O

8730

572122-01-03 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAYS 26 TO 28 AND STRINGERS 15 AND 18.

2450

O

4900

N 572125-01-02 542DB 542EB 642DB 642EB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-01

1800

O

10280

N 572125-01-03 542DB 542EB 642DB 642EB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-02

1900

O

10840

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572125-02-01 542DB 542EB 642DB 642EB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-02

1800

O

10280

N 572125-02-02 542DB 542EB 642DB 642EB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-03

1900

O

10840

N 572126-02-01 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27.

1750

O

9990

N 572129-01-01 541SB 641SB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-02-01

1530

O

8740

N 572129-01-02 541SB 641SB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-02-02

1530

O

8730

N 572129-02-01 541SB 641SB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-01-01

1530

O

8740

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572129-02-02 541SB 641SB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-01-02

1530

O

8730

N 572130-01-01 542AB 560CB 642AB 660CB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-02-01

1530

O

8740

N 572130-01-02 542AB 560CB 642AB 660CB

SEALANT REMOVAL AS PER NTM

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-02-02

1530

O

8730

N 572130-02-01 542AB 560CB 642AB 660CB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-01-01

1530

O

8740

N 572130-02-02 542AB 560CB 642AB 660CB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-01-02

1530

O

8730

R 572131-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

1300

O

6000

R 572131-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR 

SPAR BETWEEN RIB 12 AND RIB 27.

1590

O

8240

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572131-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

2130

O

4260

R 572133-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

1670

O

8670

R 572133-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

1800

O

9350

572133-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

2460

O

4920

R 572135-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12 BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINT AT STRINGER 19 BETWEEN RIB 18 AND RIB 24.

1810

O

9390

R 572138-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA.

1520

O

7900

572138-01-03 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA.

2990

O

5980

R 572139-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

1520

O

7900

572139-01-03 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

2990

O

5980

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572140-01-01 541EB 541FB 541GB

541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGER JOINTS.

1840

O

9540

572140-01-03 541EB 541FB 541GB

541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGER JOINTS.

2910

O

5820

R 572141-01-01 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642DB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB660CB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24.

1300

O

6000

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572141-01-02 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24.

1980

O

10290

572141-01-03 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUT IN RIB BAY 23-24.

2970

O

5940

R 572144-01-01 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

1520

O

7900

572144-01-03 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

2990

O

5980

N 572148-01-01 542DB 542EB 642DB 642EB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

1800

O

10280

N 572148-01-02 542DB 542EB 642DB 642EB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

1900

O

10840

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EASA APPROVED
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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572154-01-04 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BERWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES, AND SPAR JOINT BOLTING AT RIB 27.

1770

O

7990

N 572154-01-05 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BERWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES, AND SPAR JOINT BOLTING AT RIB 27.

1670

O

9030

R 572158-01-01 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23.

1160

O

6640

R 572159-01-01 542AB 542BB 542CB

560CB 642AB 642BB642CB 660CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26.

1160

O

6640

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 572162-01-01 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE SPAR JOINT PLATE AT RIB 27.

1350

O

7680

R 572162-01-02 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE SPAR JOINT PLATE AT RIB 27.

1210

O

6890

572162-01-03 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE SPAR JOINT PLATE AT RIB 27.

2010

O

4020

R 572164-01-01 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

1040

O

5970

N 572164-01-02 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

1840

O

10470

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572164-01-07 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

1920

O

10400

R 572165-01-01 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM FLANGES.

1040

O

5970

N 572165-01-02 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP AND BOTTOM FLANGES.

1840

O

10470

N 572174-01-01 541GB 541HB 541MB 541NB 

541SB 542AB 641GB 641HB 641MB 641NB 641SB 642AB

DETAILED INSPECTION OF OUTER WING RIBS 13, 18 AND 23, AT SKIN ATTACHMENTS, REGION OF STRINGER CUTOUTS AND FORWARD FLAP TRACK BRACKETS.

1340

O

7580

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572180-01-01 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

1550

O

8860

N 572180-01-02 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

1550

O

8860

572180-01-03 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

2480

O

4960

572180-01-04 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

1730

O

7500

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572180-01-05 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

1590

O

8990

N 572181-01-01 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

1550

O

8860

N 572181-01-02 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

1550

O

8860

572181-01-03 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

2480

O

4960

N 572184-01-01 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-01

1530

O

8740

N 572184-01-02 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-02

1530

O

8730

572184-01-03 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-03

2450

O

4900

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EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 572184-02-01 541QB 641QB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-01

1530

O

8740

N 572184-02-02 541QB 641QB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-02

1530

O

8730

572184-02-03 541QB 641QB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-03

2450

O

4900

572605-01-03 573BB 573FB 673BB

673FB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS).

1660

R 572605-01-04 573BB 573FB 673BB

673FB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS).

1660

572606-01-02 532CB 533CB 534CB

632CB 633CB 634CB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK_UP ASSEMBLY.

1040

572606-01-03 532CB 533CB 534CB

632CB 633CB 634CB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK_UP ASSEMBLY.

1040

R 573003-02-02 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

1740

O

9030

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

573003-02-03 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

2320

O

4640

R 574106-01-01 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522LB522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB560AB 621BB 621CB621DB 621EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622HB 622JB622LB 622MB 622NB622PB 622QB 622RB622SB 623AB 623BB623CB 623DB 623EB623FB 660AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

1180

O

6730

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AIRWORTHINESS LIMITATIONS SECTION

A340

N 574106-01-02 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522LB522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB 623FB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

1560

O

8880

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

574106-01-03 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522LB522MB 522NB 522PB522QB 522RB 522SB523AB 523BB 523CB523DB 523EB 523FB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB 623FB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

2160

O

4320

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AIRWORTHINESS LIMITATIONS SECTION

A340

574107-01-04 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522LB 522MB522NB 522PB 522QB522RB 522SB 523AB523BB 523CB 523DB523EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

1290

O

5830

N 574107-02-02 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522LB 522MB522NB 522PB 522QB522RB 522SB 523AB523BB 523CB 523DB523EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

1770

O

10100

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

574107-02-03 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522LB 522MB522NB 522PB 522QB522RB 522SB 523AB523BB 523CB 523DB523EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

2460

O

4920

N 574107-02-04 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522LB 522MB522NB 522PB 522QB522RB 522SB 523AB523BB 523CB 523DB523EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

1210

O

6580

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 574109-01-01 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522LB 522MB 522NB522PB 522QB 522RB522SB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523LB 523MB523NB 523QB 560AB621AB 621BB 621CB621DB 621EB 621FB621GB 621HB 621JB622AB 622BB 622CB622DB 622EB 622FB622GB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623LB 623MB 623NB623QB 660AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

7800 

O

4460

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 574109-01-02 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522LB 522MB 522NB522PB 522QB 522RB522SB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523LB 523MB523NB 523QB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622JB 622LB 622MB622NB 622PB 622QB622RB 622SB 623AB623BB 623CB 623DB623EB 623FB 623GB623HB 623JB 623LB623MB 623NB 623QB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

7800 

O

4480

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AIRWORTHINESS LIMITATIONS SECTION

A340

574109-01-03 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522LB 522MB 522NB522PB 522QB 522RB522SB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523LB 523MB523NB 523QB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623LB 623MB 623NB623QB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

1190

O

2380

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AIRWORTHINESS LIMITATIONS SECTION

A340

574109-02-04 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522LB 522MB 522NB522PB 522QB 522RB522SB 523AB 523BB523CB 523DB 523EB523FB 523GB 523HB523JB 523LB 523MB523NB 523QB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622LB622MB 622NB 622PB622QB 622RB 622SB623AB 623BB 623CB623DB 623EB 623FB623GB 623HB 623JB623LB 623MB 623NB623QB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

1980

O

8920

N 574110-01-01 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9

1550

O

8870

N 574110-01-02 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9

1910

O

10920

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A340

574110-01-03 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9

2770

O

5540

N 574114-01-01 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26 TO RIB 39.

1550

O

8870

N 574114-01-02 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26 TO RIB 39.

1910

O

10920

574114-01-03 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 AND RIB 26 TO RIB 39.

2770

O

5540

N 574115-01-01 522AB 522BB 522CB 523AB 

523BB 523CB 560AB 622AB 622BB 622CB 623AB 623BB 623CB 660AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 AND RIB 24 TO RIB 26.

1920

O

10950

N 574115-01-02 522AB 522BB 522CB 523AB 

523BB 523CB 560AB 622AB 622BB 622CB 623AB 623BB 623CB 660AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR FROM RIB 9 TO RIB 11 AND RIB 24 TO RIB 26.

1920

O

10950

R 575011-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

9800 

O

5110

R 575011-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

1100

O

5700

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A340

R 575011-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

1570

O

3140

575011-01-04 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

1570

O

7240

R 575011-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

1600

O

7660

N 575012-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

1340

O

7650

R 575012-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

1270

O

7240

575012-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

2290

O

4580

N 575012-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

1940

O

10960

N 575014-01-01 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG REINFORCING.

1600

O

9140

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A340

N 575017-01-02 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OR REAR SPAR JUST OUTBOARD OF GEAR SUPPORT RIB 6.

1710

O

9740

575018-01-02 147 AT 148 AT 191CT

192 CTFLAPS DEPLOYED

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

2980

O

5960

575018-01-03 147 AT 148 AT 191CT

192 CTFLAPS DEPLOYED

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

1550

R 575018-01-04 147 AT 148 AT 191CT

192 CTFLAPS DEPLOYED

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

1340

O

7590

N 575018-01-05 147 AT 148 AT 191CT

192 CTFLAPS DEPLOYED

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

1880

O

10720

R 575022-01-01 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1010

O

5780

R 575022-01-03 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

2020

O

4050

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AIRWORTHINESS LIMITATIONS SECTION

A340

575022-01-04 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1230

O

5560

R 575022-01-05 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES 1 TO 3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1160

O

6270

R 575023-01-01 575CB 575DB 675CB

675DB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

9100 

O

5210

R 575023-01-02 575CB 575DB 675CB

675DB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1370

O

2740

575023-01-03 575CB 575DB 675CB

675DB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1180

O

5320

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 575023-01-04 575CB 575DB 675CB

675DB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1110

O

6030

N 575023-01-05 575CB 575DB 675CB

675DB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE OUTBOARD AILERON, HINGES 1-3 AT LUG AND AT ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1020

O

5810

N 575025-01-01 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

1750

O

9980

N 575025-01-02 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

1470

O

8380

575025-01-03 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

2650

O

5300

R 575051-01-01 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK BEAM NO.1, UPPER FLANGES RADII OF ROLLER TRACKS.

1200

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A340

575051-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK BEAM NO.1, UPPER FLANGES RADII OF ROLLER TRACKS.

1300

D 575051-01-03 TASK DELETED IN ALI ISSUE 11

575053-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO.1, DRIVE LINK, DRIVE LEVER, DRIVE STRUT AND CARRIAGE.

1200

575054-01-01 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOX SUPPORT, FORK ASSEMBLY DRIVE STRUT AND CARRIAGE.

1300

R 575054-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOX SUPPORT, FORK ASSEMBLY DRIVE STRUT AND CARRIAGE.

1200

575055-01-02 734 744 DETAILED INSPECTION OF FLAP TRACK NO.1, 

ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.

1200

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A340

575055-01-03 734 744 DETAILED INSPECTION OF FLAP TRACK NO.1, 

ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.

1300

R 575057-01-01 FLAPS EXTENDED

AFT FLAP TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAM NO.2, 3, 4 AND 5, UPPER FLANGES RADII.

1600

D 575057-01-02 TASK DELETED IN ALI ISSUE 11

575059-01-02 FLAPS EXTENDED

AFT FLAP TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELLING BEAM AT TRACK NO.4.

1600

575061-01-02 FLAPS EXTENDED DETAILED INSPECTION OF FLAP TRACKS NO. 2, 3, 4 AND 5, 

CARRIAGE ASSEMBLIES.

1600

575061-01-03 FLAPS EXTENDED

AFT FLAP TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5, CARRIAGE ASSEMBLIES.

1600

575063-01-01 FLAP TRACK FAIRINGS DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 

AND 5 LOWER FLANGES, STRAP AND ANGLES.

1600

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R 575067-01-02 FWD FLAP TRACK 

FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS. NOTE: TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-02-02.

1320

D 575067-01-03 TASK DELETED IN ALI ISSUE 11R 575067-02-02 FWD FLAP TRACK 

FAIRINGS

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS. NOTE: TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-01-02

1320

D 575067-02-03 TASK DELETED IN ALI ISSUE 11

575069-01-02 FLAPS EXTENDED DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4 

AND 5, AFT ATTACHMENT SPIGOTS.

1590

R 575401-01-01 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD FLAP, 

EXTERNAL SURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575401-02-

01

3000 

R 575401-02-01 FLAPS EXTENDED DETAILED INSPECTION OF INBOARD FLAP, EXTERNAL 

SURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575401-01-

01

5700 

575402-01-01 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN 

AND DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT TRACK 2, LH/RH.

1300

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AIRWORTHINESS LIMITATIONS SECTION

A340

575402-01-02 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN 

AND DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT TRACK 2, LH/RH.

1300

575402-01-03 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN 

AND DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT TRACK 2, LH/RH.

1300

R 575403-01-02 581AB 734 681AB

744

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-02-02

1600

D 575403-01-04 TASK DELETED IN ALI ISSUE 11R 575403-02-02 581AB 734 681AB

744

SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.1 AND TRUNNION, INTERNAL AND EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-01-02

1600

D 575403-02-04 TASK DELETED IN ALI ISSUE 11

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 575405-01-02 531AT 531CB 631AT

631CBFLAPS EXTENDED

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVE STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM ATTACHMENT BRACKET.

1600

575503-01-02 532AT 532CB 632AT

632CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.3, AND EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING.

1600

575503-02-02 532AT 532CB 632AT

632CBSPEED TAPE FLAPS EXTENDED

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.3.

1600

575505-01-02 533AT 533CB 633AT

633CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.4, AND EXTERNAL FWD. SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.

1600

575505-02-02 533AT 533CB 633AT

633CBSPEED TAPE FLAPS EXTENDED

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.4.

1600

575507-01-02 534AT 534CB 634AT

634CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO.5, AND EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING.

1600

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AIRWORTHINESS LIMITATIONS SECTION

A340

575507-02-02 534AT 534CB 634AT

634CBSPEED TAPE FLAPS EXTENDED

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO.5.

1600

575509-01-02 RUBBER SEAL 

FLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET, EXTERNAL.

1600

575509-02-02 RUBBER SEAL 

SPEED TAPE FLAPS EXTENDED

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET, INTERNAL.

1600

577003-01-02 SPOILERS DEPLOYED

FLAPS EXTENDED

DETAILED INSPECTION OF SPOILER NO.1, HINGE AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES).

1200

577003-01-03 SPOILERS DEPLOYED

FLAPS EXTENDED

DETAILED INSPECTION OF SPOILER NO.1, HINGE AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES).

1300

711311-01-01 415AL 416AR 425AL 

426AR 435AL 436AR 445AL 446ARDISASSEMBLY ONE BY ONE OF THE HINGE BOLT IS REQUIRED

DETAILED INSPECTION OF FAN COWL HINGE FITTINGS , SLEEVES, PINS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

4500 

711312-01-01 415AL 416AR 425AL 

426AR 435AL 436AR 445AL 446AR

DETAILED INSPECTION OF FAN COWL LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND FITTINGS).

1500 

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

712101-01-01 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION.

2800 

O

1400

712101-01-02 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

DETAILED INSPECTION OF FORWARD ENGINE MOUNT INSTALLATION.

2800 

O

5600 

712201-01-01 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION.

4500 

O

2250

712201-01-02 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

DETAILED INSPECTION OF AFT ENGINE MOUNT INSTALLATION.

4500 

O

9000 

722301-01-01 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

SPECIAL DETAILED INSPECTION OF THE FAN CASE VGROOVE INNER RADIUS. 1080

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AIRWORTHINESS LIMITATIONS SECTION

A340

R 783205-01-01 415AL 416AR 417AL

418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR

SPECIAL DETAILED INSPECTION OF THE THRUST REVERSER J-RING RADIUS.NOTE: "THIS TASK COVERS INSPECTION OF THE WHOLE JRING. REFER TO MANDATORY ROHR SERVICE BULLETIN RA34078-72 REV 02 FOR MORE RESTRICTIVE REQUIREMENT (INSPECTION OF THE 6 AND 12 O'CLOCK FITTINGS ONLY)"

1300

R 783211-01-01 417AL, 418AR, 427AL, 

428AR, 437AL, 438AR, 447AL, 448AR,415AL, 425AL, 435AL, 445AL,416AR, 426AR, 436AR, 446ARDISASSEMBLY ONE BY ONE OF HINGE BOLTS IS 

REQUIRED

DETAILED INSPECTION OF THRUST REVERSER HINGE FITTINGS , SLEEVES, PINS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

4500 

R 783212-01-01 417AL, 418AR, 427AL, 

428AR, 437AL, 438AR, 447AL, 448AR415AL, 425AL, 435AL, 445AL,416AR, 426AR, 436AR, 

DETAILED INSPECTION OF THRUST REVERSER LATCH ASSEMBLY, AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS).

1500 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

521121-01-01 831 841 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

FWD PASSENGER/CRES DOORS, LH/RH.

1100

521123-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

521221-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 2 (MID 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

521223-01-01 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 2 (MID PASSENGER/CREW DOOR).

1100

521321-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

521323-01-01 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 4 (AFT PASSENGER/CREW DOOR).

1100

522121-01-02 N/A GENERAL VISUAL INSPECTION OF OVERWING EMERGENCY 

EXIT DOOR SKIN, EXTERNAL SURFACE.

8500 

522123-01-01 836 846 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

OVERWING EMERGENCY EXIT DOOR.

1100

522221-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 3 

(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8500 

522223-01-01 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON 

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).

1100

AIRWORTHINESS LIMITATIONS SECTION

 SECTION 2.2 - A340-500/600 AIRWORTHINESS LIMITATIONS

A340

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AIRWORTHINESS LIMITATIONS SECTION

A340

523126-01-01 DOOR LINING DETAILED INSPECTION OF FWD CARGO COMPARTMENT 

DOOR, FRAME 20B BETWEEN BEAM 3 AND BEAM 4.

1060

524121-02-01 N/A DETAILED INSPECTION OF AVIONICS COMPARTMENT 

ACCESS DOOR SKIN, EXTERNAL SURFACE.

1040

528123-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, 

FWD AND AFT HINGES, INCLUDING FITTINGS ON KEELBEAM, LH/RH.

5700 

528125-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS, 

CENTER HINGE, INCLUDING FITTINGS ON KEELBEAM, LH/RH.

4000 

528223-01-01 713 714 DETAILED INSPECTION OF NOSE LANDING GEAR, 

FORWARD DOORS, HINGES (NO.1, NO.2, NO.3) INCLUDING FITTINGS ON FUSELAGE, LH/RH. 

7300 

528323-01-01 753 754 DETAILED INSPECTION OF CENTER LANDING GEAR, MAIN 

DOORS, HINGES (NO.1, NO.2, NO.3), INCLUDING FITTINGS ON KEELBEAM, LH/RH. 

2500 

531810-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN 

FR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD, EXTERNAL SURFACE, LH/RH.

1220

O

9760

531810-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN 

FR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD, EXTERNAL SURFACE, LH/RH.

1240

O

8520

531812-01-02 N/A DETAILED INSPECTION OF FUSELAGE STRUCTURE 

AROUND DOOR 1 (FWD PAX/CREW DOOR), EXTERNAL SURFACE BETWEEN FR.13 AND FR.18 FROM LATERAL LONGITUDINAL LAP JOINT TO STR.9 AFT, LH/RH.

8800 

O

5280

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

531816-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND 

JOINT SURFACES BETWEEN FR.0 AND FR.18/19 BELOW CABIN FLOOR LEVEL, EXTERNAL SURFACE.

5800 

O

3510

531816-01-04 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND 

JOINT SURFACES BETWEEN FR.0 AND FR.18/19 BELOW CABIN FLOOR LEVEL, EXTERNAL SURFACE.

4450 

O

3060

531818-01-02 121EL

713 714715 716811

DETAILED INSPECTION OF FUSELAGE LOWER SKIN AT AVIONICS COMPARTMENT ACCESS DOOR CUTOUT, GROUND SERVICES CONNECTION ACCESS DOOR CUTOUT AND NOSE LANDING GEAR CUTOUT, BETWEEN FR.7 AND FR.19.

8000 

O

5000

531820-01-02 713 714

715 716

GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY INTERNAL STRUCTURE, NOSE LANDING GEAR WELL PANELS.

4100 

O

2880

531824-01-01 713 714

715 716

DETAILED INSPECTION OF NOSE LANDING GEAR BAY INTERNAL STRUCTURE, BEAM BETWEEN LANDING GEAR BEARINGS, LH/RH.

5950 

O

3590

531827-01-02 713 714

715 716

GENERAL VISUAL INSPECTION OF NOSE LANDING GEAR BAY, ANGLE FITTINGS LINKING FORWARD CANTED PANEL TO ROOF PANEL.

6800 

O

4080

531830-01-02 711/712/713/714/715/716, 

NLG, BEARING811

SPECIAL DETAILED INSPECTION OF NLG MAIN ATTACHMENT BEARING BORE.

8000 

O

5000

531831-01-02 711/712/713/714/715/716, 

BEARING, DRAG STRUT811

SPECIAL DETAILED INSPECTION OF NLG DRAG STRUT BEARING HOLE IN LATERAL PANEL.

8000 

O

5000

531832-01-01 711/712/713/714/715/716, 

NLG, BEARING

SPECIAL DETAILED INSPECTION OF NLG MAIN ATTACHMENT BEARING LUBRICATION HOLE.

8000 

O

5000

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AIRWORTHINESS LIMITATIONS SECTION

A340

531833-01-03 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, AIR CONDITIONING DUCTS 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON FRAME 12A AT STRINGER 26 LEVEL, LH/RH.

1320

531835-01-01 N/A SPECIAL DETAILED INSPECTION OF REAR LOWER CORNER 

OF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OF FR.10, EXTERNAL SURFACE, LH/RH.

4600 

O

2760

531843-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, AIR CONDITIONING DUCTS, VACUUM PIPES

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING AT FR.14, LH/RH.

1270

531844-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, AIR CONDITIONING DUCTS, VACUUM PIPES

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN FR.14 AND CRUCIFORM FITTING, LH/RH.

1270

531854-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS, SLIDING WINDOWS OPENED

DETAILED INSPECTION OF LOWER SURFACE OF UPPER CLOSING PANEL BETWEEN FR.7 AND FRONT WINDSHIELD SIDE POST, INTERNAL STRUCTURE, LH/RH.

1180

531877-01-01 811 SPECIAL DETAILED INSPECTION OF FREE FLANGE AND 

WEB OF FRAME 17 AT JUNCTION WITH THE ROD FITTING.

8000 

O

5000

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

531877-01-02 811 SPECIAL DETAILED INSPECTION OF FREE FLANGE AND 

WEB OF FRAME 17 AT JUNCTION WITH THE ROD FITTING.

8000 

O

5000

531878-01-01 713 714

715 716

GENERAL VISUAL INSPECTION OF STRUCTURE AROUND CENTRAL HOLE OF NLG BAY AFT PANEL.

8000 

O

5000

531879-02-01 811 DETAILED INSPECTION OF NLG BAY LOWER ARCH FRAMES 

12 TO 16 SPLICINGS, LH/RH.

8000 

O

5000

531879-02-02 811 DETAILED INSPECTION OF NLG BAY LOWER ARCH FRAMES 

12 TO 16 SPLICINGS, LH/RH.

8000 

O

5000

531881-01-01 811 SPECIAL DETAILED INSPECTION OF NLG BAY LOWER ARCH 

FRAMES 16A SPLICING.

8000 

O

5000

531894-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, GUSSET AND MACHINED STIFFENERS BETWEEN STRINGERS 14 AND 24, AND BETWEEN FR.17 AND FR.18, LH/RH.

1240

R

532201-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR.18 AND FR.38 FROM STR.26 LH/RH TO BOTTOM CENTER LINE, EXCLUDING AREA UNDERNEATH BELLY FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532201-02-02.

2200 

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N

532201-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR.18 AND FR.38 FROM STR.26 LH/RH TO BOTTOM CENTER LINE, EXCLUDING AREA UNDERNEATH BELLY FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532201-01-02.

6900 

532214-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AROUND FORWARD CARGO COMPARTMENT DOOR CUT-OUT AT UPPER AND LOWER CORNERS.

1000

O

7770

532215-01-02 821 GENERAL VISUAL INSPECTION OF FORWARD CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR.20A AND FR.25A).

3500 

R

532217-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR.18 AND FR.38 FROM STR.6 TO STR.26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532217-02-02.

1100

N

532217-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR.18 AND FR.38 FROM STR.6 TO STR.26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532217-01-02.

1100

532224-02-01 832/842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.

9000 

532225-01-01 832/842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 CUT-OUT UPPER CORNERS, LH/RH.

9000 

532253-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW 

VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR.32 AND FR.33, FROM STR.45 TO STR.49, LH ONLY.

9300 

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

532253-02-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW 

VALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR.37.2 AND FR.37.3, FROM STR.45 TO STR.49, LH ONLY.

1250

N

532266-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532266-02-02

4500 

N

532266-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532266-0-02

6900 

533720-01-02 191AB 192AB 192GB

192KB 193CB 193FBLEFT RAM AIR INLET

DETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TO FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6900 

O

4500

533720-01-03 191AB 192AB 192GB

192KB 193CB 193FBLEFT RAM AIR INLET

DETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TO FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

4720

533720-01-04 191AB 192AB 192GB

192KB 193CB 193FBLEFT RAM AIR INLET

DETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TO FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

5250

533720-01-05 191AB 192AB 192GB

192KB 193CB 193FBLEFT RAM AIR INLET

DETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TO FR40.3, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

5480

533722-01-02 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR 

53.8, ANGLE FITTINGS BETWEEN LATERAL PANEL AND SKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6900 

O

4490

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533722-01-03 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR 

53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

4720

533722-01-04 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR 

53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

5250

533722-01-05 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR 

53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKIN OF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.

6800 

O

5480

533730-01-02 143AB 753

754

DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.

7800 

O

5110

533730-01-03 143AB 753

754

DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.

7700 

O

5330

533730-01-04 143AB 753

754

DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.

6200 

O

4770

533730-01-05 143AB 753

754

DETAILED INSPECTION OF KEEL BEAM, TORQUE BOX EXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.

6100 

O

4910

533733-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF FWD AND AFT CORNER FITTINGS OF MLG DOOR ACTUATOR, INNER RADIUS OF INTERMEDIATE WEB, LH/RH.

5900 

533801-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

1230

O

8050

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533801-01-03 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

1400

O

9660

533801-01-04 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

1430

O

10920

533801-01-05 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE, LH/RH.

1500

O

12020

533805-01-01 N/A SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT 

DOOR CORNERS, LH/RH.

1020

O

7780

533805-01-02 N/A SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT 

DOOR CORNERS, LH/RH.

1330

O

10640

533806-01-01 N/A DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, 

PANELS AND DOUBLER ENTRIES BETWEEN FR.53.4 AND FR.53.8 AND FROM STR.12 TO STR.18 AND FROM STR.23 TO STR.29, EXTERNAL SURFACE, LH/RH.

1630

O

12430

533806-01-02 N/A DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, 

PANELS AND DOUBLER ENTRIES BETWEEN FR.53.4 AND FR.53.8 AND FROM STR.12 TO STR.18 AND FROM STR.23 TO STR.29, EXTERNAL SURFACE, LH/RH.

1590

O

12730

533808-01-01 834, 822

FLOOR PANELS AND INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS 

DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, INTERNAL STRUCTURE, FRAMES 53.5 AND 53.6A FROM STGR 9 TO 31, AND FRAMES 53.4 TO FR. 53.7, FROM STGR 9 TO STGR 11 AND FROM STGR 28 TO STGR 30, LH/RH.

1510

O

11580

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533808-01-02 834, 822

FLOOR PANELS AND INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS 

DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, INTERNAL STRUCTURE, FRAMES 53.5 AND 53.6A FROM STGR 9 TO 31, AND FRAMES 53.4 TO FR. 53.7, FROM STGR 9 TO STGR 11 AND FROM STGR 28 TO STGR 30, LH/RH.

1490

O

11960

533811-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, INTERNAL STRUCTURE, SPLICES BETWEEN BEAMS AND STRINGERS 14, 15, 26 AND 27, AT FR.53.3, FR.53.4 AND 53.8, LH/RH.

1080

O

8230

533811-01-02 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR, INTERNAL STRUCTURE, SPLICES BETWEEN BEAMS AND STRINGERS 14, 15, 26 AND 27 AT FR.53.3, FR.53.4 AND 53.8, LH/RH.

8100 

O

6520

533816-01-01 834,

FLOOR PANELS,INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF THE UPPER FRAMES TO FOOT FRAME SPLICINGS FROM FRAMES 48 TO 53.2, INTERNAL STRUCTURE, LH/RH.

1160

O

8870

533819-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED, LINING, GALLEY OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGS AT CIRCUMFERENTIAL JUNCTION AT FR.45 AND FR.54, FROM STR.15 LH TO STR.15 RH.

6600 

O

4290

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533819-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED, LINING, GALLEY OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGS AT CIRCUMFERENTIAL JUNCTION AT FR.45 AND FR.54, FROM STR.15 LH TO STR.15 RH.

4700 

O

3210

533819-01-03 INSULATION TO BE 

DISPLACED AS REQUIRED, LINING, GALLEY OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGS 

AT CIRCUMFERENTIAL JUNCTION AT FR45 AND FR54, FROM 

STR15 LH TO STR15 RH.

7800 

O

6000

533819-01-04 INSULATION TO BE 

DISPLACED AS REQUIRED, LINING, GALLEY OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGS 

AT CIRCUMFERENTIAL JUNCTION AT FR45 AND FR54, FROM 

STR15 LH TO STR15 RH.

5300 

O

4290

R

533820-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FOOT FRAME RADII FROM FR.48 TO FR.53.1, INCLUDING AREA AROUND FASTENER HOLES OF BRACKETS WHERE INSTALLED, LH/RH.

770

O

5020

D 533820-01-02 TASK DELETED IN ISSUE 11R

533820-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FOOT FRAME RADII FROM FR.48 TO FR.53.1, INCLUDING AREA AROUND FASTENER HOLES OF BRACKETS WHERE INSTALLED, LH/RH.

820

O

6300

D 533820-01-04 TASK DELETED IN ISSUE 11R

533821-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF PRESSURIZED MEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959 AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.

 882

O

5730

R

533821-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF PRESSURIZED MEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959 AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.

1090

O

8340

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N

533821-01-04 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF PRESSURIZED MEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959 AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.

734

O

5870

N

533821-01-05 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF PRESSURIZED MEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959 AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.

9320 

O

 6400

533822-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAM WEB AROUND FIXED SUPPORT HOLES AT FR.53.3.

1110

O

7240

533822-01-02 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAM WEB AROUND FIXED SUPPORT HOLES AT FR.53.3.

1060

O

7330

533822-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAM WEB AROUND FIXED SUPPORT HOLES AT FR.53.3.

1330

O

8690

533822-01-04 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAM WEB AROUND FIXED SUPPORT HOLES AT FR.53.3.

1380

O

9490

533824-01-01 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEEL 

BEAM LOWER FITTING IN SPLICING AREA BETWEEN KEEL BEAM AND FR.53.2, LH/RH.

4000 

O

2640

533824-01-02 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEEL 

BEAM LOWER FITTING IN SPLICING AREA BETWEEN KEEL BEAM AND FR.53.2, LH/RH.

6400 

O

4430

533824-01-03 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEEL 

BEAM LOWER FITTING IN SPLICING AREA BETWEEN KEEL BEAM AND FR.53.2, LH/RH.

4100 

O

3120

533824-01-04 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEEL 

BEAM LOWER FITTING IN SPLICING AREA BETWEEN KEEL BEAM AND FR.53.2, LH/RH.

6400 

O

4890

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533825-01-02 734 744

753 754

GENERAL VISUAL INSPECTION OF FWD FACE OF FR.53.2 PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET AND CONNECTION PLATES LATERAL PANEL, BETWEEN STIFFENER 1 TO 9.

4200 

O

2770

533825-01-03 734 744

753 754

GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2 PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET AND CONNECTION PLATES LATERAL PANEL, BETWEEN STIFFENER 1 TO 9.

4100 

O

2880

533825-01-04 734 744

753 754

GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2 PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET AND CONNECTION PLATES LATERAL PANEL.

6700 

O

5180

533825-01-05 734 744

753 754

GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2 PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET AND CONNECTION PLATES LATERAL PANEL.

6700 

O

5430

533828-01-02 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT FITTINGS ON FR.53.2, INCLUDING RIVET ROWS AT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.

1050

O

6910

533828-01-03 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT FITTINGS ON FR.53.2, INCLUDING RIVET ROWS AT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.

8200 

O

5640

533828-01-04 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS AT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.

8600 

O

6560

533828-01-05 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS AT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.

7000 

O

5370

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533828-01-06 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR SUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS AT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.

6100 

O

4910

533829-01-01 FLOOR PANEL

LINING

DETAILED INSPECTION OF FLOOR IN LOWER DECK FACILITIES CONFIGURATION FROM FR.53.8 TO FR.54, FROM Y+1456 TO Y-1456.

1620

O

10530

533829-01-02 FLOOR PANEL

LINING

DETAILED INSPECTION OF FLOOR IN LOWER DECK FACILITIES CONFIGURATION FROM FR.53.8 TO FR.54, FROM Y+1456 TO Y-1456.

1560

O

10770

533831-01-02 734 744

753 754

DETAILED INSPECTION OF FORWARD FACE OF FR.53.2 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.

7300 

O

4790

533831-01-03 734 744

753 754

DETAILED INSPECTION OF FORWARD FACE OF FR.53.2 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.

7300 

O

5050

533831-01-04 734 744

753 754

DETAILED INSPECTION OF FORWARD FACE OF FR.53.2 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.

6700 

O

5180

533831-01-05 734 744

753 754

DETAILED INSPECTION OF FORWARD FACE OF FR.53.2 PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.

6700 

O

5430

533835-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGER 22 AT LONGITUDINAL JUNCTION FROM FR.38 TO FR.54, LH/RH.

1530

O

9970

533835-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGER 22 AT LONGITUDINAL JUNCTION FROM FR.38 TO FR.54, LH/RH.

1530

O

10520

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533835-01-03 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGER 22 AT LONGITUDINAL JUNCTION FROM FR.38 TO FR.54, LH/RH.

1580

O

12080

533835-01-04 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGER 22 AT LONGITUDINAL JUNCTION FROM FR.38 TO FR.54, LH/RH.

1580

O

12650

533837-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TO FR.54, LH/RH.

1530

O

9970

533837-01-02 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TO FR.54, LH/RH.

1530

O

10520

533837-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TO FR.54, LH/RH.

1580

O

12080

533837-01-04 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TO FR.54, LH/RH.

1580

O

12650

533839-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

8400 

O

5480

533839-01-02 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

1650

O

11400

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533839-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

8400 

O

5480

533839-01-04 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

8400 

O

5480

533839-01-05 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

1050

O

7210

533839-01-06 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

DETAILED INSPECTION OF FRAMES AND CROSSBEAMS SPLICINGS AND SURROUNDING AREA AT STR.26, FROM FR.53.3 TO FR.54, LH/RH.

1410

O

10780

533845-01-01 822

LDF FURNISHING AND EQUIPMENT

SPECIAL DETAILED INSPECTION OF FRAME SPLICES AND CROSSBEAMS AT SPLICING LEVEL FROM FR.53.3 TO FR.54 OF AFT CARGO STRUCTURE LOWER DECK FACILITIES (LDF), LH/RH.

1490

O

9730

533845-01-02 822

LDF FURNISHING AND EQUIPMENT

SPECIAL DETAILED INSPECTION OF FRAME SPLICES AND CROSSBEAMS AT SPLICING LEVEL FROM FR.53.3 TO FR.54 OF AFT CARGO STRUCTURE LOWER DECK FACILITIES (LDF), LH/RH.

1480

O

10190

533846-01-01 822

LDF FURNISHING AND EQUIPMENT

SPECIAL DETAILED INSPECTION OF FRAME SPLICES FROM FR.53.7 TO FR.53.9, BETWEEN STR.43 AND STR.44, ON LOWER DECK AFT CARGO STRUCTURE OF LDF, LH/RH.

1570

O

10230

533846-01-02 822

LDF FURNISHING AND EQUIPMENT

SPECIAL DETAILED INSPECTION OF FRAME SPLICES FROM FR.53.7 TO FR.53.9, BETWEEN STR.43 AND STR.44, ON LOWER DECK AFT CARGO STRUCTURE OF LDF, LH/RH.

1560

O

10740

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533852-01-01 197 AB DETAILED INSPECTION OF THE MAIN HOLE RCT FITTING 

AREA BETWEEN PUMP HOLE AND MAN HOLE BETWEEN FR.53.4 AND FR.53.5.

4500 

O

3450

533852-01-02 197 AB DETAILED INSPECTION OF THE MAIN HOLE RCT FITTING 

AREA BETWEEN PUMP HOLE AND MAN HOLE BETWEEN FR.53.4 AND FR.53.5.

3500 

O

2850

533860-01-01 734 744

753 754

DETAILED INSPECTION OF MAIN LONGERON FLANGE BETWEEN FR.51 AND FR.53.1.

1280

O

9780

533860-01-02 734 744

753 754

DETAILED INSPECTION OF MAIN LONGERON FLANGE BETWEEN FR.51 AND FR.53.1.

1260

O

10080

533860-01-03 734 744

753 754

DETAILED INSPECTION OF MAIN LONGERON FLANGE BETWEEN FR.51 AND FR.53.1.

1450

O

9460

533860-01-04 734 744

753 754

DETAILED INSPECTION OF MAIN LONGERON FLANGE BETWEEN FR.51 AND FR.53.1.

1440

O

9930

533861-01-01 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OF 

MAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1, LH/RH.

1460

O

9500

533861-01-02 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OF 

MAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1, LH/RH.

1450

O

9970

533861-01-03 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OF 

MAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1, LH/RH.

1280

O

9820

533861-01-04 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OF 

MAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1, LH/RH.

1260

O

10120

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533862-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF AFT CANTED LONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.

1450

O

9480

533862-01-02 734 744

753 754

SPECIAL DETAILED INSPECTION OF AFT CANTED LONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.

1440

O

9920

533862-01-03 734 744

753 754

SPECIAL DETAILED INSPECTION OF AFT CANTED LONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.

1370

O

10520

533862-01-04 735 744

753 754

SPECIAL DETAILED INSPECTION OF AFT CANTED LONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.

1350

O

10860

533864-01-01 734 744

753 754

DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAIN LONGERON BETWEEN UPPER AND LOWER SHELL FROM FR.53 TO FR.53.2, LH/RH.

1440

O

9390

533864-01-02 734 744

753 754

DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAIN LONGERON BETWEEN UPPER AND LOWER SHELL FROM FR.53 TO FR.53.2, LH/RH.

1400

O

9670

533864-01-03 734 744

753 754

DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAIN LONGERON BETWEEN UPPER AND LOWER SHELL FROM FR.53 TO FR.53.2, LH/RH.

1400

O

10730

533864-01-04 735 744

753 754

DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAIN LONGERON BETWEEN UPPER AND LOWER SHELL FROM FR.53 TO FR.53.2, LH/RH.

1390

O

11130

533865-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF INTERNAL STRAP ON MAIN LONGERON BETWEEN UPPER AND LOWER SHELL AT FR.53.1, LH/RH.

1430

O

9890

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533867-01-01 734 744 DETAILED INSPECTION OF PANEL, CANTED BEAM AND 

DOUBLER AT JUNCTION BETWEEN CANTED BEAM, TPROFILE AND X-DOUBLER AT FR.53.2, LH/RH.

1180

O

7670

533867-01-02 734 744 DETAILED INSPECTION OF PANEL, CANTED BEAM AND 

DOUBLER AT JUNCTION BETWEEN CANTED BEAM, TPROFILE AND X-DOUBLER AT FR.53.2, LH/RH.

1120

O

8600

533868-01-01 INSULATION TO BE 

DISPLACED, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE, SPLICING OF STRINGERS 12/13/14/15 AT FR.40.6, LH/RH.

1410

O

9200

533868-01-02 INSULATION TO BE 

DISPLACED, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE, SPLICING OF STRINGERS 12/13/14/15 AT FR.40.6, LH/RH.

1400

O

9680

533869-01-01 N/A SPECIAL DETAILED INSPECTION OF OVER WING EXIT 

EXTERNAL SURROUNDING STRUCTURE, SKIN PANELS AT TWO FIRST ROWS OF DOUBLER FASTENERS, LH/RH.

1550

O

10110

533869-01-02 N/A SPECIAL DETAILED INSPECTION OF OVER WING EXIT 

EXTERNAL SURROUNDING STRUCTURE, SKIN PANELS AT TWO FIRST ROWS OF DOUBLER FASTENERS, LH/RH.

1540

O

10630

533872-01-01 INSULATION TO BE 

DISPLACED, LININGS, LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF OVER WING EXIT SURROUNDING STRUCTURE, LOWER STRAPS AT FR.41A AND FR.42A JUNCTION AT STRINGER 26.

1640

O

10680

533873-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF SPLICE BRACKETS AT FR.53.2, AT LEVEL OF UPPER TEE/CENTRAL TEE JUNCTION, LH/RH.

7800 

O

5120

533873-01-02 734 744

753 754

SPECIAL DETAILED INSPECTION OF SPLICE BRACKETS AT FR.53.2 AT LEVEL OF UPPER TEE/CENTRAL TEE JUNCTION, LH/RH.

1030

O

6720

533874-01-01 N/A SPECIAL DETAILED INSPECTION OF TWO MIDDLE 

FASTENER ROWS OF BUTTSTRAP, AT CIRCUMFERENTIAL JUNCTION AT FR.40.5 FROM STR.11 TO STR.18, LH/RH.

1150

O

7510

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533876-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

JUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHT BETWEEN FR.42 AND FR.43 AT STR.1 LH AND STR.1 RH, AND AROUND COLLISION LIGHT CUTOUT.

1600

O

10450

533876-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

JUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHT BETWEEN FR.42 AND FR.43 AT STR.1 LH AND STR.1 RH, AND AROUND COLLISION LIGHT CUTOUT.

1530

O

10540

533876-02-04 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

JUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHT BETWEEN FR.40.4 AND FR.40.5 AND BETWEEN STR.2 AND STR.5, LH/RH.

1520

O

10440

R

533877-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF T-PROFILE AT JUNCTION WITH CANTED BEAM & PANEL AT FR.53.2, STR.38, LH/RH.

1060

O

6940

R

533877-01-02 734 744

753 754

SPECIAL DETAILED INSPECTION OF T-PROFILE AT JUNCTION WITH CANTED BEAM & PANEL AT FR.53.2, STR.38, LH/RH.

7400 

O

5650

R

533877-01-03 734 744

753 754

SPECIAL DETAILED INSPECTION OF T-PROFILE AT JUNCTION WITH CANTED BEAM & PANEL AT FR.53.2, STR.38, LH/RH.

9800 

O

6370

533878-01-01 734 744

753 754

DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH Y FITTING, EXTERNAL SIDE, AT STR.40/ FR.53.2, LH/RH.

1110

O

7260

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533878-01-02 734 744

753 754

DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH Y FITTING, EXTERNAL SIDE, AT STR.40/ FR 53.2, LH/RH.

1020

O

6670

533878-01-04 734 744

753 754

DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH Y FITTING, EXTERNAL SIDE, AT STR.40/ FR 53.2, LH/RH.

1100

O

8430

533879-01-01 734 744

753 754

SPECIAL DETAILED INSPECTION OF TEE PROFILE, AT JUNCTION BETWEEN UPPER TEE/CENTRAL TEE AND SPLICE BRACKETS, AT FR.53.2, LH/RH.

1130

O

7390

533879-01-02 734 744

753 754

SPECIAL DETAILED INSPECTION OF TEE PROFILE, AT JUNCTION BETWEEN UPPER TEE/CENTRAL TEE AND SPLICE BRACKETS, AT FR.53.2, LH/RH.

1250

O

8130

533880-01-01 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWER 

FITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.

7700 

O

5000

533880-01-02 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWER 

FITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.

7600 

O

5270

533880-01-03 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWER 

FITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.

7300 

O

5620

533880-01-04 735 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWER 

FITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.

7300 

O

5860

533884-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE - FR.41A AT STR.16 AND STR27 AND FR.42A STR27 INNER FLANGES AT JUNCTION WITH STRAPS, LH/RH.

1550

O

10100

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533884-02-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE - FR.41A AT STR.16 INNER FLANGES AT JUNCTION WITH STRAPS, LH/RH.

1550

O

10100

533885-01-01 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE, INNER FLANGE OF BEAMS STR.14 AND STR.15A, AT JUNCTION WITH STRAPS, AT FR.41A, LH/RH.

1070

O

6980

533885-01-02 INSULATION TO BE 

DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT INTERNAL SURROUNDING STRUCTURE, INNER FLANGE OF BEAMS STR.14 AND STR.15A, AT JUNCTION WITH STRAPS, AT FR.41A, LH/RH.

1460

O

10060

533886-01-01 N/A DETAILED INSPECTION OF OVER WING EXIT EXTERNAL 

SURROUNDING STRUCTURE, SKIN PANELS AT CUTOUT CORNERS, LH/RH.

1620

O

10590

533886-01-02 N/A DETAILED INSPECTION OF OVER WING EXIT EXTERNAL 

SURROUNDING STRUCTURE, SKIN PANELS AT CUTOUT CORNERS, LH/RH.

1510

O

10410

533889-01-01 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.40.3 TO FR.40.6 AND FROM STR.18 TO STR.22, LH/RH.

1450

O

9450

533889-01-03 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.40.3 TO FR.40.6 AND FROM STR.18 TO STR.22, LH/RH.

1430

O

9870

533889-02-02 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.41 TO FR.44 AND FROM STR.18 TO STR.22, LH/RH.

1600

O

12240

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533889-02-04 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.41 TO FR.44 AND FROM STR.18 TO STR.22, LH/RH.

1600

O

12830

533892-01-01 822,

FLOOR PANELS, AND INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK 

SPECIAL DETAILED INSPECTION OF THE FOOT FRAMES / UPPER LATERAL FRAMES SPLICINGS FROM FRAME 53.3 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) ABOVE RCT.

1160

O

8900

533892-01-02 822,

FLOOR PANELS, AND INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK 

SPECIAL DETAILED INSPECTION OF THE FOOT FRAMES / UPPER LATERAL FRAMES SPLICINGS FROM FRAME 53.3 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) ABOVE RCT.

1140

O

9190

533893-01-01 FLOOR PANELS, 

INSULATION TO BE DISPLACED AS REQUIRED

DETAILED INSPECTION OF RCT AT LATERAL PANEL FROM FRAME 53.2 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) UP TO STRINGER 33, LH/RH.

1530

O

11670

533893-01-02 FLOOR PANELS, 

INSULATION TO BE DISPLACED AS REQUIRED

DETAILED INSPECTION OF RCT AT LATERAL PANEL FROM FRAME 53.2 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) UP TO STRINGER 33, LH/RH.

1520

O

12180

533894-01-01 197CB 153AZ DETAILED INSPECTION OF RCT AT INTERNAL FOOT FRAME 

/ LATERAL FRAME SPLICING FROM FRAMES 53.3 TO 53.6 (5 FRAME RCT) OR FRAMES 53.3 TO 53.8 (7 FRAME RCT).

1250

O

9530

533894-01-02 197CB 153AZ DETAILED INSPECTION OF RCT AT INTERNAL FOOT FRAME 

/ LATERAL FRAME SPLICING FROM FRAMES 53.3 TO 53.6 (5 FRAME RCT) OR FRAMES 53.3 TO 53.8 (7 FRAME RCT).

1200

O

9630

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533897-01-01 197CB 153AZ SPECIAL DETAILED INSPECTION OF THE FRAME SPLICES 

AND LATERAL FRAMES FROM FR.53.3 TO FR.53.6 (ON RCT5), OR TO FR.53.8 (ON RCT7).

1460

O

11200

533897-01-02 197CB 153AZ SPECIAL DETAILED INSPECTION OF THE FRAME SPLICES 

AND LATERAL FRAMES FROM FR.53.3 TO FR.53.6 (ON RCT5), OR TO FR.53.8 (ON RCT7).

1530

O

12250

533898-01-01 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TO STR22, LH/RH.

8700 

O

5710

533898-01-02 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.47 TO FR.53.1 AND FROM STR.18 TO STR.22, LH/RH.

8700 

O

5710

533898-01-03 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TO STR22, LH/RH.

9400 

O

6460

533898-01-04 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TO STR22, LH/RH.

1240

O

9510

533898-01-05 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL AND 

WINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TO STR22, LH/RH.

1480

O

11850

533899-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF WINDOW FRAME AT JUNCTION WITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEEN STR.18 AND STR.22, INTERNAL SIDE, LH/RH.

9300 

O

6050

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533899-01-02 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF WINDOW FRAME AT JUNCTION WITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEEN STR.18 AND STR.22, INTERNAL SIDE, LH/RH.

9000 

O

6220

533899-01-03 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF WINDOW FRAME AT JUNCTION WITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEEN STR.18 AND STR.22, INTERNAL SIDE, LH/RH.

1010

O

7760

533899-01-04 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF WINDOW FRAME AT JUNCTION WITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEEN STR.18 AND STR.22, INTERNAL SIDE, LH/RH.

9900 

O

7940

533901-01-01 734 744 SPECIAL DETAILED INSPECTION OF EXTERNAL SKIN PANEL 

AROUND ALL FASTENERS AT JUNCTION WITH CANTED BEAM, AT FR.53.2, LH/RH.

1180

O

8140

533901-01-02 734 744 SPECIAL DETAILED INSPECTION OF EXTERNAL SKIN PANEL 

AROUND ALL FASTENERS AT JUNCTION WITH CANTED BEAM, AT FR.53.2, LH/RH.

1040

O

8330

533902-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT SURROUNDING STRUCTURE, AT FR.41A AND FR.42A, BETWEEN STR.23 AND STR.26, LH/RH.

1450

O

9480

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533902-01-02 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF OVER WING EXIT SURROUNDING STRUCTURE, AT FR.41A AND FR.42A, BETWEEN STR.23 AND STR.26, LH/RH.

1630

O

11260

533903-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JUNCTION AT FR.40.5, STRINGERS AND SPLICES AROUND FASTENER HOLES BETWEEN STR.11 AND STR.18, LH/RH.

1170

O

7650

533904-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

GENERAL VISUAL INSPECTION OF FRAMES AT JUNCTION WITH FLOOR CROSSBEAMS AT FR.38.1 AND FR.39, LH/RH.

1470

O

9610

533905-01-01 734 744 DETAILED INSPECTION OF CANTED BEAM AT JUNCTION 

WITH SKIN PANEL AT FR.53.2, LH/RH.

1440

O

9910

533905-01-02 734 744 DETAILED INSPECTION OF CANTED BEAM AT JUNCTION 

WITH SKIN PANEL AT FR.53.2, LH/RH.

1280

O

10310

533906-01-01 734 744

753 754

DETAILED INSPECTION OF LANDING GEAR BAY UPPER PRESSURE PANELS, LOWER FACE, BETWEEN FR.47 AND FR.53.

3600 

O

2360

533906-01-02 734 744

753 754

DETAILED INSPECTION OF LANDING GEAR BAY UPPER PRESSURE PANELS, LOWER FACE, BETWEEN FR.47 AND FR.53.

3500 

O

2420

533906-01-03 734 744

753 754

DETAILED INSPECTION OF LANDING GEAR BAY UPPER PRESSURE PANELS, LOWER FACE, BETWEEN FR.47 AND FR.53.

4100 

O

3190

533906-01-04 734 744

753 754

DETAILED INSPECTION OF LANDING GEAR BAY UPPER PRESSURE PANELS, LOWER FACE, BETWEEN FR.47 AND FR.53.

5600 

O

4550

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R

533907-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND FIVE FASTENER HOLES BETWEEN FR.48 AND FR.49, AT Y-1456 AND Y+1456.

7830 

O

 5090

D 533907-01-02 TASK DELETED IN ISSUE 11R

533907-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND FIVE FASTENER HOLES BETWEEN FR.48 AND FR.49, AT Y-1456 AND Y+1456.

9090 

 O

 6930

D 533907-01-04 TASK DELETED IN ISSUE 11

533908-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGERS 22 AND 23 AND STRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.

8900 

O

5800

533908-01-02 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGERS 22 AND 23 AND STRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.

8700 

O

6010

533908-01-03 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGERS 22 AND 23 AND STRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.

9700 

O

7430

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533908-01-04 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF STRINGERS 22 AND 23 AND STRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.

9500 

O

7610

533909-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1390

O

9030

533909-01-02 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1370

O

9450

533909-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL AT 

LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1540

O

12380

533910-01-01 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS 

DETAILED INSPECTION OF INTERNAL SKIN PANEL AT LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1380

O

9030

533910-01-02 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF INTERNAL SKIN PANEL AT LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1370

O

9450

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

533910-01-03 834

INSULATION TO BE DISPLACED AS REQUIRED TO COMPLETE THE REQUIRED MAINTENANCE TASK, LININGS

DETAILED INSPECTION OF INTERNAL SKIN PANEL AT LONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54, LH/RH.

1540

O

12380

533911-01-01 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR BAY UPPER PRESSURE PANEL, LOWER SURFACE, BETWEEN FR.53 AND FR.53.2.

4900 

O

3220

533911-01-02 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR BAY UPPER PRESSURE PANEL, LOWER SURFACE, BETWEEN FR.53 AND FR.53.2.

4600 

O

3190

533911-01-03 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR BAY UPPER PRESSURE PANEL, LOWER SURFACE, BETWEEN FR.53 AND FR.53.2.

3300 

O

2580

533911-01-04 734 744

753 754

DETAILED INSPECTION OF CENTER LANDING GEAR BAY UPPER PRESSURE PANEL, LOWER SURFACE, BETWEEN FR.53 AND FR.53.2.

4200 

O

3360

533912-01-01 831

CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATION

DETAILED INSPECTION OF STRINGERS AND SPLICES AROUND FASTENERS ON FLANGES AND WEBS, BETWEEN FR.40.3 AND FR.40.6 AND BETWEEN STR.3 AND STR.4, AROUND ANTICOLLISION LIGHTS, LH/RH.

1600

O

11000

533914-01-01 834

INSULATION, LININGS

SPECIAL DETAILED INSPECTION OF STRINGER 12 AT JUNCTION WITH FRAME 43, LH/RH.

6900 

O

4500

533914-01-02 834

INSULATION, LININGS

SPECIAL DETAILED INSPECTION OF STRINGER 12 AT JUNCTION WITH FRAME 43, LH/RH.

7000 

O

4840

533915-01-01 N/A GENERAL VISUAL INSPECTION OF EXTERNAL SKIN PANEL 

BETWEEN FR.53 AND FR.54, FROM STR.1 TO STR.11, LH/RH.

5600 

O

3890

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R

533916-01-01 834

INSULATION, LININGSCEILING PANELS,OVERHEADSTOWAGE BINS,INSULATION

DETAILED INSPECTION OF INTERNAL SKIN PANEL AROUND CBB ANTENNAS, SUPPORT FITTINGS AND JUNCTION WITH DOUBLERS BETWEEN FR.53 AND FR.54, FROM STR.1 TO STR.11, LH/RH.

1210

O

8380

534205-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR.72 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

8900 

O

7410

534205-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR.72 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

1000

O

8800

534207-01-01 833/843

CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR.72, FROM STR.3 TO STR.7 AND STR.11 TO STR.13, WHERE LAP JOINTS INTERSECT WITH CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

8900 

O

7410

534207-01-02 833/843

CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR.72, FROM STR.3 TO STR.7 AND STR.11 TO STR.13, WHERE LAP JOINTS INTERSECT WITH CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

1000

O

8800

534208-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR.78 FROM STRINGERS 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

1020

O

6950

534220-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

PART OF WINDOW FORGING BETWEEN FR.54 AND FR.73 AND BETWEEN STR.18 AND STR.22 LH/RH, EXTERNAL SURFACE.

1270

O

9170

534220-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

PART OF WINDOW FORGING BETWEEN FR.54 AND FR.73 AND BETWEEN STR.18 AND STR.22 LH/RH, EXTERNAL SURFACE.

8000 

O

5600

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

R

534224-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR.54 AND FR.80 FROM STR.6 TO STR.26 , LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534224-02-02.

1100

N

534224-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR.54 AND FR.80 FROM STR.6 TO STR.26.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534224-01-02.

1100

R

534226-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

EXTERNAL SURFACE BETWEEN FR.54 AND FR.80 FROM STR.26 LH/RH TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR.54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534226-02-02.

2200 

N

534226-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR.54 AND FR.80 FROM STR.26 LH/RH TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS AND INCLUDING THE LOWER, UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARD OF FR.54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534226-01-02.

6900 

534231-01-01 833 843 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS, LH/RH.

 1150

534232-02-01 833 843

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE LH/RH.

 1150

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

534239-01-02 822 GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR.59A AND FR.65).

3500 

534246-01-02 823 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS 

OF BULK CARGO COMPARTMENT DOOR, AT 10 POSITIONS AT FR 67 AND FR 69.

1000

534249-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR.67 AND FR.69).

3500 

534271-01-01 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 3 (EMERGENCY/ PASSENGER/CREW DOOR) CUTOUT UPPER CORNERS, LH/RH.

1070

O

10130

534272-02-01 834 844

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.

1070

O

10130

534273-01-01 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS INSULATION 

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR.78, FROM STR.5 TO STR.7, WHERE LAP JOINTS INTERSECT WITH CIRCUMFERENTIAL SKIN SPLICE, LH/RH.

1020

O

6950

534274-01-01 834 844

LINING, INSULATION

DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, FLANGE OF LATERAL FRAMES, FR 56.1 AND 56.3A AT BEAM T1, T2, T7 AMD T8, LH/RH.

7400 

534275-01-01 833 843

LINING, INSULATION

DETAILED INSPECTION OF DOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT, FLANGE OF LATERAL FRAMES, FR 73A AND 75A AT BEAM T1, T2, T7 AND T8, LH/RH.

7400 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

N 534277-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR 54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINE EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534277-02-01.

4500 

N 534277-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 

54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINE EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534277-01-01.

6900 

535213-01-01 312AR DETAILED INSPECTION OF SKIN, INNER DOUBLER AND 

EDGE BEAM AT LOWER HORIZONTAL TAILPLANE CUT-OUT AT FR.87 BETWEEN STR.26 AND STR.27, LH/RH.

1200

O

7800

535213-01-02 312AR DETAILED INSPECTION OF SKIN, INNER DOUBLER AND 

EDGE BEAM AT LOWER HORIZONTAL TAILPLANE CUT-OUT AT FR.87 BETWEEN STR.26 AND STR.27, LH/RH.

1200

O

6600

545721-01-02 415AL 416AR

425AL 426AR435AL 436AR445AL 446AR

DETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 - F4, LH/RH. 

5000 

O

3250

545721-01-03 415AL 416AR

425AL 426AR435AL 436AR445AL 446AR

DETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 - F4, LH/RH. 

5000 

O

3430

545721-01-04 415AL 416AR

425AL 426AR435AL 436AR445AL 446AR

DETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 - F4, LH/RH. 

5000 

O

3810

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545721-01-05 415AL 416AR

425AL 426AR435AL 436AR445AL 446AR

DETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 - F4, LH/RH. 

5000 

O

4000

545725-01-02 425AL 426AR

427AL 428AR435AL 436AR437AL 438AR

DETAILED INSPECTION OF PYLON THRUST REVERSER FITTINGS, R3- R4, LH/RH.

3500 

O

2300

545725-01-03 425AL 426AR

427AL 428AR435AL 436AR437AL 438AR

DETAILED INSPECTION OF PYLON THRUST REVERSER FITTINGS, R3- R4, LH/RH.

3600 

O

2490

545725-01-04 425AL 426AR

427AL 428AR435AL 436AR437AL 438AR

DETAILED INSPECTION OF PYLON THRUST REVERSER FITTINGS, R3- R4, LH/RH.

3000 

O

2340

545725-01-05 425AL 426AR

427AL 428AR435AL 436AR437AL 438AR

DETAILED INSPECTION OF PYLON THRUST REVERSER FITTINGS, R3- R4, LH/RH.

3200 

O

2600

545801-02-01 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OF 

LOWER ARMS AT ENGINE FORWARD MOUNT FITTING, SPIGOT HOLE LOCATION.

7100 

O

4620

545801-02-02 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OF 

LOWER ARMS AT ENGINE FORWARD MOUNT FITTING, SPIGOT HOLE LOCATION.

8000 

O

5500

545801-02-03 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OF 

LOWER ARMS AT ENGINE FORWARD MOUNT FITTING, SPIGOT HOLE LOCATION.

6700 

O

5100

545801-02-04 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OF 

LOWER ARMS AT ENGINE FORWARD MOUNT FITTING, SPIGOT HOLE LOCATION.

8000 

O

6400

545802-01-02 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINE 

ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING.

5000 

O

3250

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545802-01-03 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINE 

ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING.

5000 

O

3430

545802-01-04 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINE 

ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING.

5000 

O

3810

545802-01-05 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINE 

ATTACHMENT BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING.

5000 

O

4000

545804-01-01 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

SPECIAL DETAILED INSPECTION OF PYLON, ON THE PYRAMID END OF LOWER ARMS AFT RIB 1.

8000 

O

5200

545804-01-02 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

SPECIAL DETAILED INSPECTION OF PYLON, ON THE PYRAMID END OF LOWER ARMS AFT RIB 1.

8000 

O

5500

545804-01-03 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

SPECIAL DETAILED INSPECTION OF PYLON, ON THE PYRAMID END OF LOWER ARMS AFT RIB 1.

8000 

O

6100

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545804-01-04 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

SPECIAL DETAILED INSPECTION OF PYLON, ON THE PYRAMID END OF LOWER ARMS AFT RIB 1.

8000 

O

6400

545810-01-02 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT BEAM AT RIB 6.

5000 

O

3250

545810-01-03 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT BEAM AT RIB 6.

5000 

O

3430

545810-01-04 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT BEAM AT RIB 6.

5000 

O

3810

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545810-01-05 415AL 416AR

417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448AR

DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT BEAM AT RIB 6.

5000 

O

4000

545813-01-01 452CR 452GR 452EL

462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLY

DETAILED INSPECTION OF THE FORWARD PYLON TO WING ATTACHMENT AT RIB 8.

8000 

O

5200

545813-01-02 452CR 452GR 452EL

462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLY

DETAILED INSPECTION OF THE FORWARD PYLON TO WING ATTACHMENT AT RIB 8.

8000 

O

5500

545813-01-03 452CR 452GR 452EL

462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLY

DETAILED INSPECTION OF THE FORWARD PYLON TO WING ATTACHMENT AT RIB 8.

8000 

O

6100

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545813-01-04 452CR 452GR 452EL

462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLY

DETAILED INSPECTION OF THE FORWARD PYLON TO WING ATTACHMENT AT RIB 8.

8000 

O

6400

545814-01-01 454AL 454AR 454BL 454BR

464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BR

DETAILED INSPECTION OF THE AFT PYLON TO WING ATTACHMENT AT RIB 14.

8000 

O

5200

545814-01-02 454AL 454AR 454BL 454BR

464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BR

DETAILED INSPECTION OF THE AFT PYLON TO WING ATTACHMENT AT RIB 14.

8000 

O

5500

545814-01-03 454AL 454AR 454BL 454BR

464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BR

DETAILED INSPECTION OF THE AFT PYLON TO WING ATTACHMENT AT RIB 14.

8000 

O

6100

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

545814-01-04 454AL 454AR 454BL 454BR

464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BR

DETAILED INSPECTION OF THE AFT PYLON TO WING ATTACHMENT AT RIB 14.

8000 

O

6400

545842-01-01 453CL 453CR

463CL 463CR473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUT AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

6100 

O

4650

545842-01-02 453CL 453CR

463CL 463CR473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUT AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

6000 

O

3950

545842-01-03 453CL 453CR

463CL 463CR473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUT AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

6400 

O

4410

545842-01-04 453CL 453CR

463CL 463CR473CL 473CR483CL 483CR

DETAILED INSPECTION OF PYLON LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUT AND MATING SURFACE BETWEEN RIB 9 AND RIB 10.

6300 

O

5040

R

571801-01-01 147AZ 148AZ

734 744

DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN PANEL UPPER FACE AROUND HYDRAULIC HOLES BETWEEN STIFFENER 34 AND STIFFENER 35 AND BETWEEN Y-953 AND Y-1959.

1340

O

9210

571802-01-01 191FB 192FB 192JB

192NB 195JB 195NB

SPECIAL DETAILED INSPECTION OF TEE BACKING PLATES AROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEEN FR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.

1260

O

8250

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

571802-01-02 191FB 192FB 192JB

192NB 195JB 195NB

SPECIAL DETAILED INSPECTION OF TEE BACKING PLATES AROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEEN FR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.

1150

O

7960

571802-01-03 191FB 192FB 192JB

192NB 195JB 195NB

SPECIAL DETAILED INSPECTION OF TEE BACKING PLATES AROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEEN FR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.

1350

O

8830

571802-01-04 191FB 192FB 192JB

192NB 195JB 195NB

SPECIAL DETAILED INSPECTION OF TEE BACKING PLATES AROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEEN FR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.

1290

O

9840

571802-01-05 191FB 192FB 192JB

192NB 195JB 195NB

SPECIAL DETAILED INSPECTION OF TEE BACKING PLATES AROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEEN FR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.

1380

O

10530

571803-01-01 CABIN FLOOR PANELS, 

INSULATION, LININGS, GALLEYS AND TOILETS IF FITTED

DETAILED INSPECTION OF CENTER WING BOX BEAM RADII ON BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LH SIDE BETWEEN FR.46 AND FR.47.

6600 

O

4300

571803-01-02 CABIN FLOOR PANELS, 

INSULATION, LININGS, GALLEYS AND TOILETS IF FITTED

DETAILED INSPECTION OF CENTER WING BOX BEAM RADII ON BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LH SIDE BETWEEN FR.46 AND FR.47.

6400 

O

4410

571803-01-03 CABIN FLOOR PANELS, 

INSULATION, LININGS, GALLEYS AND TOILETS IF FITTED

DETAILED INSPECTION OF CENTER WING BOX BEAM RADII ON BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LH SIDE BETWEEN FR.46 AND FR.47.

6000 

O

4590

571803-01-04 CABIN FLOOR PANELS, 

INSULATION, LININGS, GALLEYS AND TOILETS IF FITTED

DETAILED INSPECTION OF CENTER WING BOX BEAM RADII ON BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LH SIDE BETWEEN FR.46 AND FR.47.

6000 

O

4680

571804-01-01 191 BT

192 BT,CT195 CT

SPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING, FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEEN STIFFENERS 19 AND 21, LH/RH.

1170

O

7640

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

571804-01-02 191 BT

192 BT,CT195 CT

SPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING, FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEEN STIFFENERS 19 AND 21, LH/RH.

1170

O

7640

571804-01-03 191 BT

192 BT,CT195 CT

SPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING, FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEEN STIFFENERS 19 AND 21, LH/RH.

1010

O

6940

571804-01-04 191 BT

192 BT,CT195 CT

SPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING, FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEEN STIFFENERS 19 AND 21, LH/RH.

1210

O

9730

571808-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 

FRAME 40 "NODE", LOWER SKIN PANEL AT JUNCTION WITH L- FLANGE AROUND FASTENER HOLES BETWEEN Y1959 AND RIB 1, LH/RH.

9200 

O

6020

571808-01-02 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 

FRAME 40 "NODE", LOWER SKIN PANEL AT JUNCTION WITH L- FLANGE AROUND FASTENER HOLES BETWEEN Y1959 AND RIB 1, LH/RH.

1380

O

9490

571808-01-03 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 

FRAME 40 "NODE" , LOWER SKIN PANEL AT JUNCTION WITH L- FLANGE AROUND FASTENERS HOLES, BETWEEN Y1959 AND RIB 1, LH/RH.

1030

O

7860

571808-01-04 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 

FRAME 40 "NODE" , LOWER SKIN PANEL AT JUNCTION WITH L- FLANGE AROUND FASTENERS HOLES, BETWEEN Y1959 AND RIB 1, LH/RH.

1550

O

12410

571809-01-01 147AZ 148AZ

734 744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWER SKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959 AND LOWER CORNER FITTING LH/RH. 

1560

O

9360

571809-01-02 147AZ 148AZ

734 744

SPECIAL DETAILED INSPECTION OFCENTER WING BOX, FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWER SKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959 AND LOWER CORNER FITTING, LH/RH. 

1560

O

10720

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

571809-01-03 147AZ 148AZ

734 744

SPECIAL DETAILED INSPECTION OFCENTER WING BOX, FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWER SKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959 AND LOWER CORNER FITTING, LH/RH. 

8000 

O

4800

R

571811-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40 

AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTION WITH CENTER WING BOX LOWER PANEL, LH/RH.

7400 

O

4850

R

571811-01-02 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40 

AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTION WITH CENTER WING BOX LOWER PANEL, LH/RH.

7300 

O

5620

R

571811-01-03 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40 

AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTION WITH CENTER WING BOX LOWER PANEL, LH/RH.

7400 

O

5110

R

571811-01-05 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40 

AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTION WITH CENTER WING BOX LOWER PANEL, LH/RH.

1480

O

11850

571812-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX, 

FRAME 40 "NODE", CIRCUMFERENTIAL JUNCTION, STR.35/36 AREA, OUTSIDE LOWER SHELL.

8000 

O

4800

571813-01-01 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40 

"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40 BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH. 

1110

O

7250

571813-01-02 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40 

"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40 BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH. 

1130

O

7360

571813-01-04 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40 

"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40 BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH. 

1040

O

7940

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TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

571813-01-05 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40 

"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40 BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH. 

1050

O

8060

R

571815-01-01 FLOOR PANELS

GALLEY OR LAVATORY IF INSTALLED734 744147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL, AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

8730 

O

5670

R

571815-01-02 FLOOR PANELS

GALLEY OR LAVATORY IF INSTALLED734 744147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

7350 

O

4770

R

571815-01-03 FLOOR PANELS

GALLEY OR LAVATORY IF INSTALLED734 744147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL AT SYSTEM HOLES AREAS : Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

6250 

O

4310

R

571815-01-04 FLOOR PANELS

GALLEY OR LAVATORY IF INSTALLED734 744147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

8800 

O

6710

N

571815-01-05 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED, 734 744 147AZ 148AZ.

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

7250 

O

5540

N

571815-01-06 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED, 734 744 147AZ 148AZ.

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 AND BETWEEN STIFFENERS 17 AND 18.

6610 

O

5290

D 571816-01-01 TASK DELETED IN ISSUE 11D 571816-01-02 TASK DELETED IN ISSUE 11

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

D 571816-01-03 TASK DELETED IN ISSUE 11D 571816-01-04 TASK DELETED IN ISSUE 11D 571816-01-05 TASK DELETED IN ISSUE 11D 571816-01-06 TASK DELETED IN ISSUE 11D 571816-01-07 TASK DELETED IN ISSUE 11D 571816-01-08 TASK DELETED IN ISSUE 11D 571816-01-09 TASK DELETED IN ISSUE 11D 571816-01-10 TASK DELETED IN ISSUE 11

571817-01-01 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL, UPPER FACE AT PUMP HOLES AREA, BETWEEN FR.44 AND FR.47.

6300 

O

4140

571817-01-02 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL, UPPER FACE AT PUMP HOLES AREA, BETWEEN FR.44 AND FR.47.

6300 

O

4240

571817-01-03 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL, UPPER FACE AT PUMP HOLES AREA, BETWEEN FR.44 AND FR.47.

6500 

O

4990

571817-01-04 FLOOR PANELS, GALLEY 

OR LAVATORY IF INSTALLED

SPECIAL DETAILED INSPECTION OF CWB, UPPER SKIN PANEL, UPPER FACE AT PUMP HOLES AREA, BETWEEN FR.44 AND FR.47.

6400 

O

5130

571818-01-01 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1080

O

7030

571818-01-02 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

6900 

O

4510

571818-01-03 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1440

O

9960

571818-01-04 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1040

O

7990

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

571818-01-05 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

8400 

O

6440

571818-01-06 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF UPPER PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1410

O

11320

571819-01-01 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

9500 

O

6200

571819-01-02 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

9500 

O

6200

571819-01-03 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

9300 

O

6400

571819-01-04 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1000

O

7670

571819-01-05 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

1000

O

7670

571819-01-06 147AZ 148AZ

734 744

GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL AND STIFFENERS AT CENTER WING BOX AREA.

9800 

O

7910

571831-02-01 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3400 

O

2230

571831-02-02 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3000 

O

2100

571831-02-03 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3600 

O

2800

571831-02-04 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3500 

O

2330

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

571831-02-05 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3800 

O

2930

571831-02-06 734 744

147AZ 148AZ

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.

3800 

O

3060

572206-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.

1140

O

6930

572206-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1 AND 12.

8200 

O

5640

572210-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 6 AND RIB 23.

1030

O

6260

572210-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 6 AND RIB 23.

1050

O

6360

572210-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 6 AND RIB 23.

9300 

O

6390

572211-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 6 AND RIB 9.

1320

O

8020

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572211-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 6 AND RIB 9.

1180

O

7190

572211-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO CENTER SPAR BETWEEN RIB 6 AND RIB 9.

1000

O

6870

572212-01-01 541AB 541AZ 541CZ 542AB 

542BZ 641AB 641AZ 641CZ 642AB 642BZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 BETWEEN RIB 4 AND RIB 8.

1160

O

7070

572212-01-02 541AB 541AZ 541CZ 542AB 

542BZ 641AB 641AZ 641CZ 642AB 642BZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 BETWEEN RIB 4 AND RIB 8.

9600 

O

6600

572213-01-01 542BB 542CB 542DB 542EB 

542FB 542GB 642BB 642CB 642DB 642EB 642FB 642GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 26 BETWEEN RIB 7 AND RIB 15.

1080

O

6580

572213-01-02 542BB 542CB 542DB 542EB 

542FB 542GB 642BB 642CB 642DB 642EB 642FB 642GB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 26 BETWEEN RIB 7 AND RIB 15.

1210

O

8340

572214-01-01 541AB 541AZ 541CZ 542AB 

542BZ 641AB 641AZ 641CZ 642AB 642BZ

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 4 AND RIB 8.

1170

O

7120

572214-01-02 541AB 541AZ 541CZ 542AB 

542BZ 641AB 641AZ 641CZ 642AB 642BZ

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 4 AND RIB 8.

9600 

O

6630

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572215-01-01 542BB 542CB 542DB 542EB 

542FB 542GB 642BB 642CB 642DB 642EB 642FB 642GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 26 BETWEEN RIB 7 AND RIB 15.

1100

O

6710

572215-01-02 542BB 542CB 542DB 542EB 

542FB 542GB 642BB 642CB 642DB 642EB 642FB 642GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 26 BETWEEN RIB 7 AND RIB 15.

1240

O

8560

572236-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3 AND RIB 7.

7900 

O

4830

572236-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3 AND RIB 7.

8600 

O

5250

572236-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3 AND RIB 7.

8000 

O

5520

572239-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIB BAY 3-4 AND RIB BAY 11-13.

1080

O

6540

572239-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIB BAY 3-4 AND RIB BAY 11-13.

9100 

O

5510

572239-01-03 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIB BAY 3-4 AND RIB BAY 11-13.

9300 

O

6430

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572241-02-01 573/673 BB, FB, DEPLOY 

FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER AND LOWER ATTACHMENT ANGLES.

1030

O

6240

572241-02-02 573/673 BB, FB, DEPLOY 

FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER AND LOWER ATTACHMENT ANGLES.

1110

O

6750

572244-01-02 541AB 641AB DETAILED INSPECTION OF OUTER WING REAR SPAR 

FORWARD FACE UPPER AND LOWER ROOT JOINT FITTINGS. 

1320

O

9070

572246-01-01 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB 5.

9700 

O

5910

572246-01-02 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB 5.

1060

O

6470

572246-01-03 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR 

SPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB 5.

9400 

O

6470

572247-01-01 573FB 673FB

DEPLOY FLAPS

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE JOINT PLATE AT RIB 9.

1230

O

8510

572264-01-03 522EB 622EB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE JOINT PLATE AT RIB 12. 

1400

O

9650

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572265-01-01 542BB 542CB 542CZ 542DZ 

642BB 642CB 642CZ 642DZ

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 8 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

1200

O

7310

572265-01-02 542BB 542CB 542CZ 542DZ 

642BB 642CB 642CZ 642DZ

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 8 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGES.

1070

O

7400

572276-02-01 542CB 542DB 542DZ 

542EZ 642CB 642DB 642DZ 642EZ 

DETAILED INSPECTION OF OUTER WING RIB 10 FORWARD, RIB 10A AND PYLON DIAPHRAGM. 

1180

O

8110

572277-02-01 542AB 542AZ 542BB 

542BZ 542CB 542CZ 542DB 542DZ 542EB 542EZ 642AB 642AZ 642BB 642BZ 642CB 642CZ 642DB 642DZ642EB 642EZ

DETAILED INSPECTION OF OUTER WING RIBS 10 AFT, 11 AND 12, FORWARD AND AFT OF CENTER SPAR, AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

7800 

O

5420

572278-01-01 542AB 642AB SPECIAL DETAILED INSPECTION OF OUTER WING RIB 7 AFT 

AT TOP AND BOTTOM CASTELLATIONS FOR STRINGERS.

1110

O

6750

572278-01-02 542AB 642AB SPECIAL DETAILED INSPECTION OF OUTER WING RIB 7 AFT 

AT TOP AND BOTTOM CASTELLATIONS FOR STRINGERS.

9100 

O

6260

572281-01-02 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPAR 

ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

1030

O

6290

572286-01-01 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPAR 

UPPER AND LOWER ROOT JOINT FITTINGS IN RIB BAY 1-2.

1170

O

7120

572286-01-02 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPAR 

UPPER AND LOWER ROOT JOINT FITTINGS IN RIB BAY 1-2.

1370

O

9470

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EASA APPROVED
Rev 

code

TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

572287-01-01 542/642 DB DETAILED INSPECTION OF OUTER WING CENTER SPAR TO 

UPPER AND LOWER STRINGER JOINTS IN RIB BAY 11-12.

7600 

O

4640

572287-01-02 542/642 DB DETAILED INSPECTION OF OUTER WING CENTER SPAR TO 

UPPER AND LOWER STRINGER JOINTS IN RIB BAY 11-12.

7900 

O

4790

572287-01-03 542/642 DB SPECIAL DETAILED INSPECTION OF OUTER WING CENTER 

SPAR TO UPPER AND LOWER STRINGER JOINTS IN RIB BAY 11-12.

7700 

O

5300

R

572288-01-01 542AB 542BB 542BZ 542CB 

542CZ 542DZ 642AB 642BB 642BZ 642CB 642CZ 642DZ

DETAILED INSPECTION OF OUTER WING CENTRE SPAR BETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACES INCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.

9200 

O

5580

R

572288-01-02 542AB 542BB 542BZ 542CB 

542CZ 542DZ 642AB 642BB 642BZ 642CB 642CZ 642DZ

DETAILED INSPECTION OF OUTER WING CENTRE SPAR BETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACES INCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.

1190

O

7220

572288-01-03 542AB 542BB 542BZ 542CB 

542CZ 542DZ 642AB 642BB 642BZ 642CB 642CZ 642DZ

DETAILED INSPECTION OF OUTER WING CENTRE SPAR BETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACES INCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.

1260

O

8690

572289-01-01 541AB 541AZ 541BB 541BZ 

541CZ 641AB 641AZ 641BB 641BZ 641CZ

DETAILED INSPECTION OF OUTER WING CENTRE SPAR BETWEEN RIB 2 AND RIB 6 FORWARD AND AFT FACES INCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES AND CONDUIT HOLES.

1060

O

7320

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572307-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR BETWEEN RIBS 12 AND 41.

9000 

O

5500

572307-01-04 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACK CANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR BETWEEN RIBS 12 AND 41.

8800 

O

6080

572313-01-02 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURE IN RIB BAY 12-13.

1380

O

8380

572313-01-04 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN VISIBLE SURFACES OF FUEL PUMP APERTURE IN RIB BAY 12-13.

1160

O

8030

572314-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT FUEL JETTISON HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 17 AND 18.

8500 

O

5160

572314-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT FUEL JETTISON HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 17 AND 18.

1050

O

7230

572315-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 23 AND RIB 36.

9400 

O

5750

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Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

572315-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 23 AND RIB 36.

1120

O

7730

572316-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT FRONT SPAR STRINGER RUNOUTS, STR 7 (RIB BAY 14-15), STR 8 (RIB BAY 17-18) AND STR 9 (RIB BAY 19-20).

1040

O

6340

572316-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT FRONT SPAR STRINGER RUNOUTS, STR 7 (RIB BAY 14-15), STR 8 (RIB BAY 17-18) AND STR 9 (RIB BAY 19-20).

9800 

O

6800

572317-01-01 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.

1030

O

6290

572317-01-02 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.

1120

O

7730

572318-01-01 543QB 543RB 543SB 543TB 

543UB 643QB 643RB 643SB 643TB 643UB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 BETWEEN RIB 25 & RIB 30.

1010

O

6120

572318-01-02 543QB 543RB 543SB 543TB 

543UB 643QB 643RB 643SB 643TB 643UB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 BETWEEN RIB 25 & RIB 30.

9000 

O

6250

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

572319-01-01 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.

1030

O

6290

572319-01-02 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.

1120

O

7730

572320-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT FRONT SPAR STRINGER RUNOUTS, STR 12 (RIB BAY 27-28), STR 13 (RIB BAY 29-30) AND STR 14 (RIB BAY 32-33).

8100 

O

4950

572320-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT FRONT SPAR STRINGER RUNOUTS, STR 12 (RIB BAY 27-28), STR 13 (RIB BAY 29-30) AND STR 14 (RIB BAY 32-33).

1060

O

7310

572321-01-01 543CB 543DB 543EB 543FB 

543GB 543QB 543RB 543SB 543TB 543UB 643CB 643DB 643EB 643FB 643GB 643QB 643RB 643SB 643TB 643UB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 25 & RIB 30.

1010

O

6170

572321-01-02 543CB 543DB 543EB 543FB 

543GB 543QB 543RB 543SB 543TB 543UB 643CB 643DB 643EB 643FB 643GB 643QB 643RB 643SB 643TB 643UB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 25 & RIB 30.

1050

O

7270

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AIRWORTHINESS LIMITATIONS SECTION

A340

572322-01-01 PYLON FAIRINGS

FLAP TRACK FAIRINGS

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO STRINGERS,RIBS AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

1160

O

7040

572322-01-02 PYLON FAIRINGS

FLAP TRACK FAIRINGS

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT ATTACHMENT TO STRINGERS,RIBS AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

1270

O

7710

572323-01-01 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 542NB 542PB 542QB 542SB 542SB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB 642NB 642PB 642QB 642SB 642SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS, STRINGER JOINTS AND BUTTSTRAPS BETWEEN RIB 11 AND RIB 23 EXCLUDING STRINGERS 13,18 AND 26.

1160

O

7050

572323-01-02 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 542NB 542PB 542QB 542SB 542SB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB 642NB 642PB 642QB 642SB 642SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS, STRINGER JOINTS AND BUTTSTRAPS BETWEEN RIB 11 AND RIB 23 EXCLUDING STRINGERS 13,18 AND 26.

1010

O

6120

572335-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT FRONT SPAR STRINGER RUNOUTS, RIB BAY 14-15.

1340

O

8160

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

572336-01-01 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

LOWER SURFACE STRINGER JOINTS, RIB BAY 12-13, STRINGER 20.

1330

O

8050

572336-01-02 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

LOWER SURFACE STRINGER JOINTS, RIB BAY 12-13, STRINGER 20.

8400 

O

5090

572336-01-03 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

LOWER SURFACE STRINGER JOINTS, RIB BAY 12-13, STRINGER 20.

1060

O

7290

572337-01-01 542HB 642HB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKIN 

LOWER SURFACE STRINGER JOINTS, RIB BAY 15-16, STRINGER 28.

1320

O

8000

572338-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE ABOVE FRONT SPAR BETWEEN RIB 11 AND RIB 22.

1060

O

6460

572340-01-01 542EB 542FB 542GB 542HB 

542JB 542KB 542LB 542MB 542NB 542PB 542QB 542RB 542SB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB 642NB 642PB 642QB 642RB 642SB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS AND BUTTSTRAPS BETWEEN RIBS 12 AND 23 AND STRINGER JOINTS 12,13,14 AT RIB BAY 22-23.

1140

O

6920

572362-01-02 523/623 DB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE SPAR JOINT PLATE AT RIB 26.

1120

O

7740

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

572367-01-01 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 542NB 542PB 542QB 542SB 542SB 543AB 543BB 543CB 543DB 543EB 543FB 543GB 543HB 543JB 543KB 543LB 543MB 543NB 543PB 543QB 543RB 543SB 543TB 543UV 543VB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB 642NB 642PB 642QB 642SB 642SB 643AB 643BB 643CB 643DB 643EB 643FB 643GB 643HB 643JB 643KB 643LB 643MB 643NB 643PB 643QB 643RB 643SB 643TB 643UV 643VB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 11 AND RIB 35 INCLUDING TOP AND BOTTOM FLANGES.

9900 

O

6000

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

572367-01-02 542DB 542EB 542FB 542GB 

542HB 542JB 542KB 542LB 542MB 542NB 542PB 542QB 542SB 542SB 543AB 543BB 543CB 543DB 543EB 543FB 543GB 543HB 543JB 543KB 543LB 543MB 543NB 543PB 543QB 543RB 543SB 543TB 543UV 543VB 642DB 642EB 642FB 642GB 642HB 642JB 642KB 642LB 642MB 642NB 642PB 642QB 642SB 642SB 643AB 643BB 643CB 643DB 643EB 643FB 643GB 643HB 643JB 643KB 643LB 643MB 643NB 643PB 643QB 643RB 643SB 643TB 643UV 643VB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 11 AND RIB 35 INCLUDING TOP AND BOTTOM FLANGES.

8900 

O

6140

572372-02-01 543BB 543CB 543PB

543QB 643BB 643CB643PB 643QBOUTBOARD PYLON FAIRINGSVENT PIPES DISPLACED FROM RIB 23 OUTBOARD

DETAILED INSPECTION OF OUTER WING RIBS, RIB 25 INCLUDING INTERNAL PYLON ATTACHMENT BRACKET.

6500 

O

4520

572373-02-01 542/642 EB, FB, KB, LB, QB, 

SB 543/643 AB, NB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 

AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGER 

CUTOUTS AND FORWARD FLAP TRACK BRACKETS.

9200 

O

5630

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

572373-02-02 542/642 EB, FB, KB, LB, QB, 

SB 543/643 AB, NB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18 

AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGER 

CUTOUTS AND FORWARD FLAP TRACK BRACKETS.

1230

O

8480

572655-01-02 573BB 573FB 673BB

673FB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE RIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAP TRACK 2 AFT PICK UP (INCLUDING BOX BRACKET, INTERFACE PLATE AND THRUST PADS).

1240

572656-02-01 532/632/533/633/534/634 SB DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 

AND 5 AFT PICK-UP, ASSEMBLY.

8200 

572656-02-02 532/632/533/633/534/634 SB DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 

AND 5 AFT PICK-UP, ASSEMBLY.

7000 

572659-01-01 523AB 523BB 523AT 523CT 

623AB 623BB 623AT 623CT

SPECIAL DETAILED INSPECTION OF OUTER WING OUTER PYLON INBOARD AND OUTBOARD FORWARD ATTACHMENT FITTINGS.

8000 

O

4800

572666-01-01 533VT 533WB 534VT 534WB 

633VT 633WB 634VT 634WB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 4 AND 5 FORWARD PICK-UP FITTING LUGS.

8300 

572666-01-02 533VT 533WB 534VT 534WB 

633VT 633WB 634VT 634WB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 4 AND 5 FORWARD PICK-UP FITTING LUGS.

8300 

572666-01-03 533VT 533WB 534VT 534WB 

633VT 633WB 634VT 634WB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 4 AND 5 FORWARD PICK-UP FITTING LUGS.

8000 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

574158-02-01 521/621 AB DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.

6900 

O

4220

574158-02-02 521/621 AB DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAIN ATTACHMENTS TO FRONT SPAR AND FUSELAGE.

1160

O

7080

574170-01-01 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 23 AND RIB 26.

1220

O

7410

574170-01-02 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 23 AND RIB 26.

9400 

O

5710

574170-01-03 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 23 AND RIB 26.

1050

O

7270

574171-01-01 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS AT SLAT TRACKS 7-9 AND SLAT TRACK 14.

1360

O

8290

574172-01-01 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS AT SLAT TRACKS 12 & 13

8000 

O

4800

574172-01-02 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS AT SLAT TRACKS 12 & 13

8100 

O

5570

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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Rev 

code

TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

N

574353-01-01 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 

ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 

9100 

O

6920

N

574353-01-02 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 

ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 

9400 

O

6110

N

574353-01-03 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 

ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 

8400 

O

6720

N

574353-01-04 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4 

ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS, BOLTS, LINKS AND LINK PLATE, LH/RH. 

8800 

O

6030

575071-02-01 FLAPS EXTENDED

734 744

DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, ROLLER TRACKS.

1200

575074-01-02 FLAPS EXTENDED

734 744

DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOX SUPPORT, FORK ASSEMBLY, DRIVE STRUT AND CARRIAGE.

1200

575074-01-03 FLAPS EXTENDED

734 744

DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOX SUPPORT, FORK ASSEMBLY, DRIVE STRUT AND CARRIAGE.

1200

575077-01-01 FLAPS EXTENDED

734 744

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 5, ROLLER TRACK.

1080

575077-01-02 FLAPS EXTENDED

734 744

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 5, ROLLER TRACK.

1080

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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TASK 

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AIRWORTHINESS LIMITATIONS SECTION

A340

575079-01-02 FLAPS EXTENDED, AFT 

FLAP TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELING BEAM AT TRACK NO 4.

1080

575079-01-03 FLAPS EXTENDED, AFT 

FLAP TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELING BEAM AT TRACK NO 4.

1080

575087-01-02 FWD FLAP TRACK 

FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575087-02-02.

1200

575087-01-03 FWD FLAP TRACK 

FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575087-02-03.

1200

575087-02-02 FWD FLAP TRACK 

FAIRINGS

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575087-01-02.

1200

575087-02-03 FWD FLAP TRACK 

FAIRINGS

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575087-01-03.

1200

575112-02-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING.

1360

O

9410

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

575114-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 9 AND RIB 12.

1010

O

6150

575114-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 9 AND RIB 12.

9100 

O

5510

575114-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 9 AND RIB 12.

9400 

O

6510

575122-01-02 575AB 675AB DETAILED INSPECTION OF OUTER WING TRAILING EDGEINNER AILERON HINGES 1-3 AND THE TOP AND BOTTOM 

SKIN OVERHANGS UPPER AND LOWER SURFACES AT THESE LOCATIONS.

1140

O

6960

575123-01-02 575CB 675CB DETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTER AILERON HINGES 1-3 AND THE TOP AND BOTTOM 

SKIN OVERHANGS UPPER AND LOWER SURFACES AT THESE LOCATIONS.

6300 

O

3820

575125-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

INNER BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 9 TO RIB 12.

1050

O

7280

575126-01-02 575/675 BB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

INNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS AND THE TOP AND BOTTOM SKINS UPPER AND LOWER SURFACES AT ATTACHMENTS TO THE POSTS.

8100 

O

4930

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
Rev 

code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

575126-01-03 575/675 BB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

INNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS AND THE TOP AND BOTTOM SKINS UPPER AND LOWER SURFACES AT ATTACHMENTS TO THE POSTS.

6600 

O

4010

575451-01-02 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD FLAP, 

EXTERNAL SURFACE OF UPPER AND LOWER SKIN.

3000 

575452-01-01 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN 

AND DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS TRACK NO. 2.

1200

575453-01-02 734 744

581/681 ABPLUGS

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575453-02-2.

1200

575453-02-02 734 744

581/681 AB, PLUGS, SPEED TAPES

SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575453-01-02.

1200

711351-01-01 415AL 416AR 425AL 426AR

435AL 436AR 445AL 446ARDISASSEMBLY ONE BY ONE OF THE HINGE BOLT IS REQUIRED.

DETAILED INSPECTION OF FAN COWL, FITTINGS AND SURROUNDING STRUCTURE (15 CM AROUND FITTINGS).

4000 

711352-01-01 415AL 416AR

425AL 426AR435AL 436AR445AL 446AR

DETAILED INSPECTION OF FAN COWL LATCH FITTINGS AND SURROUNDING STRUCTURE (15 CM AROUND FITTINGS).

4000 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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AIRWORTHINESS LIMITATIONS SECTION

A340

712152-01-01 415AL 416AR 417AL 418AR

425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448AR

DETAILED INSPECTION OF TRENT 500-ENGINE FORWARD MOUNT REAR TRUNNION CLEARANCE HOLE.NOTE: THE INSPECTION IS FOR LOSS OF CLEARANCE BETWEEN THE REAR TRUNNION AND VERTICAL FAILSAFE LOAD LINK ASSEMBLY.

4000 

O

2750

712153-01-01 415AL 416AR 417AL 418AR

425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448ARENGINE REMOVAL AND ENGINE MOUNT DISASSEMBLY

SPECIAL DETAILED INSPECTION OF TRENT 500-ENGINE FORWARD MOUNT THRUST TRUNNION.

8000 

O

5500

712252-01-01 415AL 416AR 417AL 418AR

425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448ARFAILSAFE PIN RETAINING BOLT & WASHERTORQUE LINK PIN RETAINING BOLTS & WASHER

DETAILED INSPECTION OF TRENT 500-ENGINE REAR MOUNT FAILSAFE PIN ,TORQUE LINK PIN.NOTE : INSPECTION OF THE FAILSAFE PIN IS FOR FREEDOM OF MOVEMENT. INSPECTION OF THE TORQUE LINK PIN IS FOR DAMAGE OF THE PIN AND RETAINING BOLTS.

2400 

O

1670

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRES

AIRWORTHINESS LIMITATIONS SECTION

A340

783251-01-02 417EL 418ER

427EL 428ER437EL 438ER447EL 448ERDISASSEMBLY ONE BY ONE OF HINGE BOLTS IS REQUIRED.

DETAILED INSPECTION OF THRUST REVERSER HINGE LUGS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE LUGS).

4000 

R

783252-01-01 415AL 416AR

417AL 417FL418AR 425AL426AR 427AL427FL 428AR435AL 436AR437AL 437FL438AR 445AL446AR 447AL447FL 448AR

DETAILED INSPECTION OF THRUST REVERSER 6 O'CLOCK BEAM LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

4000 

783253-01-01 414AL 414AR

415AL 416AR417AL 417FL418AR 424AL424AR 425AL426AR 427AL427FL 428AR434AL 434AR435AL 436AR437AL 437FL438AR 444AL444AR 445AL446AR 447AL447FL 448AR

DETAILED INSPECTION OF THRUST REVERSER AFT CORE COWL LATCH ASSEMBLY (ON 2 HALVES) AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTING).

4000 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

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code

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AIRWORTHINESS LIMITATIONS SECTION

A340

783254-01-02 415AL 416AR

417CL 417DL417EL 418CR418DR 418ER425AL 426AR427CL 427DL427EL 428CR428DR 428ER435AL 436AR437CL 437DL437EL 438CR438DR 438ER445AL 446AR447CL 447DL447EL 448CR448DR 448ERDISCONNECTION ONE BY ONE OF THE ACTUATOR FROM THE T/R COWL IS REQUIRED.

DETAILED INSPECTION OF THRUST REVERSER FORWARD FRAME AND TRANSCOWL ACTUATOR FITTINGS AND ITS ATTACHMENTS (6 PLACES ON EACH HALF).

4000 

783255-01-01 415/425/435/445 AL

416/426/436/446 AR417/427/437/447 FL417/427/437/447 AL418/428/438/448 AR

DETAILED INSPECTION OF THRUST REVERSER J-RING (V BLADE).

4000 

© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation Items

EASA APPROVED
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-1 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

 SECTION 2.1 – A340-200/300 AIRWORTHINESS LIMITATIONS 

R 523106-01-01 Access updated 

R 528104-01-01 Threshold/Interval updated 

R 528104-01-02 Threshold/Interval updated 

R 532101-01-01 Description updated to add the note on the alternative task 

Threshold/Interval updated 

N 532101-02-01 New task created as an alternative of task 532101-01-01 

R 532114-01-01 Interval updated 

R 532117-01-01 

Description updated to reduced the inspection area. Inspection is 

splitted with task 532166. 

Note added on the alternative task 

Interval updated 

N 532117-02-01 New task created as an alternative of task 532117-01-01 

R 532124-02-01 Threshold updated 

R 532124-02-02 Threshold updated 

R 532124-02-03 Interval updated 

Applicability updated due to the split of the task 

N 532124-02-05 New task created coming from the split of 532124-02-03 

R 532125-01-01 Threshold updated 

R 532125-01-02 Threshold updated 

R 532125-01-03 Interval updated 

Applicability updated due to the split of the task 

N 532125-01-05 New task created coming from the split of 532125-01-03 

R 532143-01-01 Applicability updated 

R 532144-01-01 Access updated for wording 

R 532147-01-01 Access updated for wording 

N 532166-01-01 New task created coming from the split of task 532117-01-01 

N 532166-02-01 New task created coming from the split of task 532117-01-01 and to 

propose an alternative task to 532166-01-01 

R 533005-01-01 

Threshold/interval FC figures updated 

Threshold/interval FH figures added 

Applicability updated due to the split of the task 

N 533005-01-02 New task created coming from the split of 533005-01-01 

R 533103-02-01 Interval FC figure updated 

Threshold/interval FH figures added 

R 533104-01-02 Description updated for wording 

Threshold/interval updated 

R 533105-01-01 Threshold/interval FC figures updated 

Threshold/interval FH figures added 

R 533106-01-01 Threshold/interval updated 

R 533107-01-01 Threshold/interval FC figures updated 

Threshold/interval FH figures added 

R 533107-01-02 Threshold/interval updated 

R 533111-01-01 Interval FC figure updated 

Threshold/interval FH figures added 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-2 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 533113-01-01 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 533113-01-02 Threshold FC figure updated 

Threshold/Interval FH figures added 

R 533113-01-03 Threshold/Interval updated 

R 533114-01-01 Threshold/Interval FH figures added 

R 533114-01-02 Threshold updated 

R 533115-01-01 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 533115-01-02 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 533115-01-03 Threshold/Interval updated 

R 533116-01-01 Threshold/Interval updated 

R 533125-01-02 Threshold/Interval FH figures added 

Applicability updated due to the split of the task 

N 533125-01-03 New task created coming from the split of 533125-01-02 

R 533126-01-02 Description updated for clarification 

Threshold/interval FH figure added 

R 533126-01-03 Description updated for clarification 

Threshold/interval FH figure added 

R 533126-01-04 Description updated for clarification 

Threshold/interval FH figure added 

R 533127-01-01 

Access updated to be simplified and to cover all configurations 

Threshold/interval FH figures added 

Applicability updated to merge the task with 533127-01-02 

D 533127-01-02 Task deleted and merged with 533127-01-01 and 533127-03-04 

R 533127-03-01 

Access updated to be simplified and to cover all configurations 

Threshold/interval FH figures added 

Applicability updated to merge the task with 533127-03-03 

R 533127-03-02 Access updated to be simplified 

Threshold/interval FH figures added 

D 533127-03-03 Task deleted and merged with 533127-03-01 

R 533132-02-02 Threshold/interval updated 

R 533134-02-01 

Access updated 

Threshold/Interval FC figure updated 

Threshold/Interval FH figure added 

Applicability updated due to the split of the task 

N 533134-02-02 New task created coming from the split of 533134-02-01 

R 533139-01-01 Interval FC figure updated 

Threshold/interval FH figures added 

R 533139-01-03 Interval FC figure updated 

Threshold/interval FH figures added 

R 533145-01-02 Threshold/Interval FC figures updated 

Threshold/interval FH figures added 

R 533154-01-01 Interval FC figure updated 

Threshold/interval FH figures added 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-3 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 533154-01-03 Interval FC figure updated 

Threshold/interval FH figures added 

R 533162-01-01 Threshold FC figure updated 

Threshold/interval FH figures added 

R 533163-01-01 

Description updated for clarification 

Threshold FC figure updated 

Threshold/interval FH figure added 

Applicability updated for wording 

R 533164-01-01 

Description updated for clarification 

Interval FC figure updated 

Threshold/interval FH figures updated 

R 533164-01-02 Description updated for clarification 

Threshold/interval updated 

R 533164-01-03 Description updated for clarification 

R 533165-01-01 Threshold/interval updated 

R 533180-01-01 Threshold/interval updated 

R 533180-01-02 Threshold updated 

R 533181-01-01 Interval updated 

R 533194-01-01 Description updated to delete the note 

Interval updated 

R 533194-01-02 Description updated to delete the note 

Applicability updated to exclude Post 42352 A/C 

R 533194-01-03 Description updated to delete the note 

R 533194-01-04 Description updated to delete the note 

Interval updated 

R 533194-01-05 Description updated to delete the note 

Applicability updated for clarification 

R 533194-01-06 Description updated to delete the note 

Threshold FH figure updated 

R 533194-01-09 Description updated to delete the note 

R 533195-02-01 Description updated to delete the note 

Interval updated 

R 533195-02-02 Description updated to delete the note 

R 533195-02-03 Description updated to delete the note 

R 533195-02-04 Description updated to delete the note 

Interval updated 

R 533195-02-05 Description updated to delete the note 

Applicability updated for clarification 

R 533195-02-06 Description updated to delete the note 

Threshold FH figure updated 

R 533195-02-09 Description updated to delete the note 

Threshold FH figure updated 

R 534102-01-01 Threshold/Interval updated 

R 534104-01-02 Threshold updated 

R 534104-01-03 Threshold updated 

R 534105-01-01 Threshold/Interval updated 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-4 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 534124-01-01 

Description updated to reduced the inspection area. Inspection is 

splitted with task 534177. 

Interval updated. 

R 534124-02-01 

Inspection level corrected 

Description updated to reduced the inspection area. Inspection is 

splitted with task 534177. 

Interval updated. 

R 534126-01-01 Threshold/interval updated 

R 534126-02-01 Threshold/interval updated 

R 534131-01-01 Interval updated 

Applicability updated due to the split of the task 

N 534131-01-03 New task created coming from the split of 534131-01-01 

R 534132-02-01 Interval updated 

Applicability updated due to the split of the task 

N 534132-02-03 New task created coming from the split of 534132-02-01 

R 534136-01-01 Threshold/Interval updated 

R 534143-01-01 Threshold/Interval updated 

R 534144-02-01 Access updated for door reference 

Threshold/Interval updated 

R 534144-02-02 Access updated for door reference 

R 534144-02-03 Access updated for door reference 

R 534150-01-01 Access updated for wording 

N 534177-01-01 New task created coming from the split of task 534124-01-01 

N 534177-02-01 New task created coming from the split of task 534124-01-01 and to 

propose an alternative task to 534177-01-01 

D 545104-01-01 Task superseded by ISB 54-4010 

D 545104-01-02 Task superseded by ISB 54-4010 

D 545104-01-06 Task superseded by ISB 54-4010 

R 545142-01-01 Threshold/Interval FH figures updated 

N 545146-01-01 New task created 

N 545146-01-02 New task created 

R 545166-01-01 Threshold FC figure updated 

Threshold/interval FH figures updated 

R 545166-01-03 Threshold/Interval updated 

R 545166-01-05 Threshold FC figure updated 

Threshold/interval FH figures updated 

R 545166-01-06 Threshold FC figure updated 

Threshold/interval FH figures updated 

R 545168-01-01 Threshold FC figure updated 

Threshold/interval FH figures updated 

R 545168-01-03 Threshold/Interval updated 

R 545168-01-05 Threshold FC figure updated 

Threshold/interval FH figures updated 

R 545168-01-06 Threshold FC figure updated 

Threshold/interval FH figures updated 

N 545174-01-01 New task created 

N 545174-01-02 New task created 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-5 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

N 545174-01-04 New task created 

N 545174-01-05 New task created 

R 545180-02-02 Threshold/Interval updated 

R 545180-02-03 Threshold/Interval updated 

Applicability updated to split the task 

R 545180-02-04 Threshold/Interval updated 

R 545180-02-05 Threshold/Interval updated 

R 545180-02-06 Threshold/Interval updated 

N 545180-02-07 New task created coming from the split of 545180-02-03 

R 551016-01-01 Threshold/interval FC figures updated 

Threshold/interval FH figures added 

R 571102-01-01 Threshold/Interval updated 

Applicability updated 

R 571102-01-02 Threshold/Interval updated 

R 571103-01-01 Threshold/interval updated 

R 571103-01-02 Threshold/interval updated 

R 571103-02-01 Threshold/interval updated 

R 571103-02-02 Threshold/interval updated 

R 571104-01-01 Access updated 

Threshold/interval updated 

R 571104-01-02 Access updated 

Threshold/interval updated 

R 571104-01-03 Access updated 

Threshold/interval updated 

R 571104-01-04 Access updated 

Threshold/interval updated 

R 571104-01-05 Access updated 

Threshold/interval updated 

R 571107-01-01 Threshold/interval updated 

R 571107-01-02 Threshold/interval updated 

R 571107-01-03 Threshold/interval updated 

R 571108-01-01 Threshold/interval updated 

R 571108-01-03 Threshold/interval updated 

R 571108-01-04 Threshold/interval updated 

R 571114-01-01 Threshold/interval updated 

R 571114-01-03 Threshold/interval updated 

R 571114-01-04 Threshold/interval updated 

R 571116-01-01 Threshold/interval updated 

R 571116-01-02 Threshold/interval updated 

R 571116-01-03 Threshold/interval updated 

R 571118-01-01 

Access updated to be simplified and to cover all configurations 

Threshold/interval updated 

Applicability updated to merge the task with 571118-01-02 

D 571118-01-02 Task deleted and merged with 571118-01-01 

R 571118-01-03 

Access updated to be simplified and to cover all configurations 

Threshold/interval updated 

Applicability updated to merge the task with 571118-01-04 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-6 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

D 571118-01-04 Task deleted and merged with 571118-01-03 

R 571118-01-05 

Access updated to be simplified and to cover all configurations 

Threshold/interval updated 

Applicability updated to merge the task with 571118-01-06 

D 571118-01-06 Task deleted and merged with 571118-01-05 

R 571122-01-02 Threshold/interval updated 

R 571122-01-03 Threshold/interval updated 

R 571123-01-01 

Description updated for wording 

Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 571123-01-02 

Description updated for wording 

Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 571123-01-03 Description updated for wording 

Threshold/Interval updated 

N 571123-01-04 New task created to cover Groups 42A and 43A Post 49404 

N 571123-01-05 New task created to cover Groups 42B and 43B Post 49404 and 43E 

R 571125-01-01 Threshold/interval updated 

R 571125-01-02 Threshold/interval updated 

R 571126-01-01 Threshold/interval updated 

R 571126-01-02 Threshold/interval updated 

R 571133-01-02 Threshold/interval updated 

R 571133-01-03 Threshold/interval updated 

R 571146-02-01 Threshold/interval updated 

R 571146-02-02 Threshold/interval updated 

R 571146-02-03 Threshold/interval updated 

R 571149-01-02 Threshold/interval updated 

R 571149-01-03 Threshold/interval updated 

R 571152-01-01 Threshold/interval updated 

N 571153-01-01 New task created 

N 571153-01-02 New task created 

N 571153-01-03 New task created 

N 571153-01-04 New task created 

R 571153-01-05 

Access updated 

Description updated 

Threshold/Interval updated 

N 571162-01-01 New task created 

N 571163-01-01 New task created 

R 571165-01-01 Threshold/interval updated 

R 571165-01-02 Threshold/interval updated 

N 572004-01-02 New task created 

R 572004-01-03 Threshold/Interval FH figures updated 

D 572004-01-05 Task deleted and superseded by task 572006-02-05 

N 572006-02-05 New task created to supersede task 572006-01-05 

N 572006-02-07 New task created 

N 572006-02-08 New task created 

N 572007-01-02 New task created 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-7 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 572007-01-03 Threshold/Interval FH figures updated 

N 572010-02-01 New task created 

N 572012-01-01 New task created 

N 572012-01-04 New task created 

N 572013-01-01 New task created 

N 572013-01-03 New task created 

N 572013-01-05 New task created 

N 572014-01-05 New task created 

N 572015-02-05 New task created 

R 572016-02-01 Threshold/Interval updated 

N 572016-02-02 New task created 

N 572016-02-05 New task created 

R 572017-01-05 Threshold/Interval updated 

R 572018-01-01 Description updated to extend the inspection area. 

Threshold/Interval updated 

N 572018-01-02 New task created 

N 572018-01-03 New task created 

R 572019-01-01 Threshold/Interval updated 

N 572019-01-02 New task created 

N 572019-01-03 New task created 

N 572019-01-06 New task created 

N 572021-01-01 New task created 

N 572021-01-04 New task created 

N 572022-01-01 New task created 

N 572023-02-01 New task created 

N 572023-02-04 New task created 

R 572027-01-01 Threshold/Interval updated 

R 572029-01-01 Threshold/Interval updated 

Applicability updated to split the task 

N 572029-01-04 New task created coming from the split of 572029-01-01 

R 572030-01-01 Threshold/Interval updated 

R 572030-01-02 Threshold/Interval updated 

R 572030-01-03 Threshold updated 

R 572032-01-01 Threshold/Interval updated 

R 572032-01-02 Threshold/Interval updated 

Applicability updated to split the task 

R 572032-01-03 Interval FH figure updated 

N 572032-01-05 New task created coming from the split of 572032-01-02 

R 572033-01-01 Threshold/Interval updated 

N 572033-01-02 New task created 

R 572034-01-01 Threshold/Interval FH figures updated 

R 572034-01-02 Threshold/Interval updated 

N 572034-01-05 New task created 

R 572035-01-01 Threshold/Interval updated 

R 572035-01-02 Threshold/Interval updated 

R 572036-01-01 Threshold/Interval updated 

R 572036-01-02 Threshold/Interval updated 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-8 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 572039-01-01 Threshold/Interval updated 

R 572039-01-02 Threshold/Interval updated 

R 572040-01-01 Interval FC figure updated 

Threshold/Interval FH figure updated 

R 572040-01-02 Threshold/Interval updated 

R 572046-01-01 Threshold/Interval updated 

R 572046-01-02 Threshold/Interval updated 

N 572046-01-05 New task created 

N 572047-01-01 New task created 

N 572047-01-04 New task created 

N 572047-01-05 New task created 

R 572050-01-01 Threshold/Interval updated 

R 572050-01-02 Threshold/Interval updated 

R 572050-01-03 Threshold updated 

R 572051-01-02 Threshold/Interval updated 

R 572051-01-03 Threshold/Interval updated 

R 572052-01-01 Threshold/Interval updated 

R 572052-01-02 Threshold/Interval updated 

N 572052-01-05 New task created 

R 572054-01-05 Description updated for clarification 

R 572054-01-06 

Description updated for clarification 

Threshold/Interval updated 

Applicability updated to exclude Post 46141 aircraft 

R 572054-01-07 

Description updated for clarification 

Threshold/Interval updated 

Applicability updated to exclude Post 46141 aircraft 

N 572054-01-08 New task created 

R 572063-01-01 Threshold/Interval updated 

N 572063-01-02 New task created 

N 572063-01-06 New task created 

R 572064-01-01 Threshold/Interval updated 

N 572064-01-02 New task created 

R 572065-01-01 Threshold/Interval updated 

R 572065-01-02 Threshold/Interval updated 

D 572068-01-01 Task deleted 

N 572068-01-05 New task created to cover Group 43B 

R 572073-01-01 Threshold/Interval updated 

N 572073-01-02 New task created 

R 572081-01-01 Threshold/Interval updated 

R 572081-01-02 Threshold/Interval updated 

R 572081-01-03 Threshold/Interval updated 

R 572082-01-01 Threshold/Interval updated 

R 572082-01-02 Threshold/Interval updated 

R 572082-01-03 Threshold/Interval updated 

N 572082-01-06 New task created to cover Group 43B Post 48437 

R 572093-01-01 Threshold/Interval updated 

R 572093-02-01 Threshold/Interval updated 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-9 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 572094-01-01 Threshold/Interval updated 

R 572095-01-01 Threshold/Interval updated 

N 572095-01-02 New task created to cover Post 40610 A/C 

N 572095-01-03 New task created to cover Group 42B and Group 43B Pre 48437 

N 572102-01-01 New task created 

N 572109-02-01 New task created 

N 572109-02-02 New task created 

N 572110-01-01 New task created 

N 572110-01-02 New task created 

N 572111-01-01 New task created 

N 572111-01-02 New task created 

N 572116-01-05 New task created 

N 572117-01-05 New task created 

N 572121-01-01 New task created 

N 572121-01-02 New task created 

R 572121-01-03 Threshold updated to correct typing mistake 

R 572122-01-01 Threshold/Interval updated 

N 572122-01-02 New task created 

N 572125-01-02 New task created 

N 572125-01-03 New task created 

N 572125-02-01 New task created 

N 572125-02-02 New task created 

N 572126-02-01 New task created 

N 572129-01-01 New task created 

N 572129-01-02 New task created 

N 572129-02-01 New task created 

N 572129-02-02 New task created 

N 572130-01-01 New task created 

N 572130-01-02 New task created 

N 572130-02-01 New task created 

N 572130-02-02 New task created 

R 572131-01-01 Interval updated 

R 572131-01-02 Threshold/Interval updated 

R 572133-01-01 Threshold/Interval updated 

R 572133-01-02 Threshold/Interval updated 

R 572135-01-01 Threshold/Interval updated 

R 572138-01-01 Threshold/Interval updated 

R 572139-01-01 Threshold/Interval updated 

R 572140-01-01 Threshold/Interval updated 

R 572141-01-01 Interval updated 

N 572141-01-02 New task created 

R 572144-01-01 Threshold/Interval updated 

N 572148-01-01 New task created 

N 572148-01-02 New task created 

N 572154-01-05 New task created 

R 572158-01-01 Threshold/Interval updated 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-10 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 572159-01-01 Threshold/Interval updated 

R 572162-01-01 Threshold/Interval updated 

R 572162-01-02 Threshold/Interval updated 

R 572164-01-01 Threshold/Interval updated 

N 572164-01-02 New task created 

N 572164-01-07 New task created 

R 572165-01-01 Threshold/Interval updated 

N 572165-01-02 New task created 

N 572174-01-01 New task created 

N 572180-01-01 New task created 

N 572180-01-02 New task created 

N 572180-01-05 New task created 

N 572181-01-01 New task created 

N 572181-01-02 New task created 

N 572184-01-01 New task created 

N 572184-01-02 New task created 

N 572184-02-01 New task created 

N 572184-02-02 New task created 

R 572605-01-04 Interval updated 

R 573003-02-02 Threshold/Interval updated 

R 574106-01-01 Threshold/Interval updated 

N 574106-01-02 New task created 

N 574107-02-02 New task created 

N 574107-02-04 New task created 

R 574109-01-01 Threshold/Interval updated 

R 574109-01-02 Threshold/Interval updated 

N 574110-01-01 New task created 

N 574110-01-02 New task created 

N 574114-01-01 New task created 

N 574114-01-02 New task created 

N 574115-01-01 New task created 

N 574115-01-02 New task created 

R 575011-01-01 Threshold/Interval updated 

R 575011-01-02 Threshold/Interval updated 

R 575011-01-03 Threshold/Interval updated 

R 575011-01-05 Threshold/Interval updated 

N 575012-01-01 New task created 

R 575012-01-02 Threshold/Interval updated 

N 575012-01-05 New task created 

N 575014-01-01 New task created 

N 575017-01-02 New task created 

R 575018-01-04 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

N 575018-01-05 New task created to cover Group 42B and Group 43B Pre 48437 

R 575022-01-01 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-11 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 575022-01-03 Threshold/Interval FH figures added 

R 575022-01-05 Threshold/Interval updated 

R 575023-01-01 

Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

Applicability updated to split the task 

R 575023-01-02 Threshold/Interval FC figures updated 

Threshold/Interval FH figures added 

R 575023-01-04 Threshold/Interval updated 

N 575023-01-05 New task created coming from the split of 575023-01-01 

N 575025-01-01 New task created 

N 575025-01-02 New task created 

R 575051-01-01 Applicability extended due to the merging with task 575051-01-03 

D 575051-01-03 Task deleted and merged with 575051-01-01 

R 575054-01-02 Interval updated 

R 575057-01-01 Applicability updated to merge the task with 575057-01-02 

D 575057-01-02 Task deleted and merged with 575057-01-01 

R 575067-01-02 Threshold/Interval updated 

Applicability updated to merge the task with 575067-01-03 

D 575067-01-03 Task deleted and merged with 575067-01-02 

R 575067-02-02 Threshold/Interval updated 

Applicability updated to merge the task with 575067-02-03 

D 575067-02-03 Task deleted and merged with 575067-02-02 

R 575401-01-01 Applicability updated to extend the task to Group 43E 

R 575401-02-01 Threshold/Interval updated 

Applicability updated to extend the task to Group 43E 

R 575403-01-02 Applicability updated to merge the task with 575403-01-04 

D 575403-01-04 Task deleted and merged with 575403-01-02 

R 575403-02-02 Applicability updated to merge the task with 575403-02-03 

D 575403-02-04 Task deleted and merged with 575403-02-02 

R 575405-01-02 Interval updated 

R 783205-01-01 Applicability updated 

R 783211-01-01 Access updated 

R 783212-01-01 Access updated 

 SECTION 2.2 – A340-500/600 AIRWORTHINESS LIMITATIONS 

R 532201-01-02 Description updated to add the note on the alternative task 

Threshold/Interval updated 

N 532201-02-02 New task created as an alternative of task 532201-01-02 

R 532217-01-02 

Description updated to reduce the inspection area. Inspection is 

splitted with task 532266. 

Note added on the alternative task 

Interval updated 

N 532217-02-02 New task created as an alternative of task 532201-01-02 

N 532266-01-02 New task created coming from the split of task 532217-01-01 

N 532266-02-02 New task created coming from the split of task 532217-01-01 and to 

propose an alternative task to 532266-01-02 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-12 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 533820-01-01 Threshold/interval updated 

Applicability updated to exclude Post 57860 A/C 

D 533820-01-02 Task deleted 

R 533820-01-03 Threshold/interval updated 

Applicability updated to exclude Post 57860 A/C 

D 533820-01-04 Task deleted 

R 533821-01-01 Threshold/interval updated 

Applicability updated to exclude aircraft Post 57290 or Post 57291 

R 533821-01-03 Threshold/interval updated 

Applicability updated to exclude aircraft Post 57290 or Post 57291 

N 533821-01-04 New task created coming from the split of task 533821-01-03 

N 533821-01-05 New task created coming from the split of task 533821-01-01 

R 533877-01-01 Interval updated 

R 533877-01-02 Interval updated 

R 533877-01-03 Interval updated 

R 533907-01-01 Threshold/Interval updated 

Applicability updated to take into account mod 57290 

D 533907-01-02 Task deleted 

R 533907-01-03 Threshold/Interval updated 

Applicability updated to take into account mod 57290 

D 533907-01-04 Task deleted 

R 533916-01-01 Threshold/Interval updated 

R 534224-01-02 

Description updated to reduce the inspection area. 

Inspection is splitted with task 534277. 

Note added on the alternative task 

Interval updated. 

N 534224-02-02 New task created as an alternative of task 534224-01-02 

R 534226-01-02 

Description updated. 

Note added on the alternative task. 

Interval updated. 

N 534226-02-02 New task created as an alternative of task 534226-01-02 

N 534277-01-01 New task created coming from the split of task 534224-01-01 

N 534277-02-01 New task created coming from the split of task 534224-01-01 and to 

propose an alternative task to 534277-01-01 

R 571801-01-01 Description updated. 

R 571811-01-01 Description simplified 

R 571811-01-02 Description simplified 

R 571811-01-03 Description simplified 

R 571811-01-05 Description simplified 

R 571815-01-01 

Access updated. 

Description updated 

Threshold/Interval updated 

Applicability updated 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: FEB 20/09 PAGE: APXA-13 

©AIRBUS SAS 2009. All rights reserved. 

A340

REV CODE TASK REFERENCE SUMMARY OF CHANGES 

R 571815-01-02 

Access updated. 

Description updated 

Threshold/Interval updated 

R 571815-01-03 

Access updated. 

Description updated 

Threshold/Interval updated 

Applicability updated 

R 571815-01-04 

Access updated. 

Description updated 

Threshold/Interval updated 

Applicability updated 

N 571815-01-05 New task coming from the split of task 571815-01-04. 

N 571815-01-06 New task coming from the split of task 571815-01-04. 

D 571816-01-01 Task deleted and superseded by ISB 57-5011 

D 571816-01-02 Task deleted and superseded by ISB 57-5011 

D 571816-01-03 Task deleted and superseded by ISB 57-5011 

D 571816-01-04 Task deleted and superseded by ISB 57-5011 

D 571816-01-05 Task deleted and superseded by ISB 57-5011 

D 571816-01-06 Task deleted and superseded by ISB 57-5011 

D 571816-01-07 Task deleted and superseded by ISB 57-5011 

D 571816-01-08 Task deleted and superseded by ISB 57-5011 

D 571816-01-09 Task deleted and superseded by ISB 57-5011 

D 571816-01-10 Task deleted and superseded by ISB 57-5011 

R 572288-01-01 Threshold/Interval updated 

R 572288-01-02 Threshold/Interval updated 

N 574353-01-01 New task created 

N 574353-01-02 New task created 

N 574353-01-03 New task created 

N 574353-01-04 New task created 

R 783252-01-01 Threshold/interval corrected 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX B – ABBREVIATIONS

ISSUE: FEB 20/09 PAGE: APXB-1 

©AIRBUS SAS 2009. All rights reserved. 

A340

ABBREVIATION MEANING 

AD Airworthiness Directive 

ALI Airworthiness Limitation Item 

ALS Airworthiness Limitations Section 

AMM Aircraft Maintenance Manual 

ATA Air Transport Association 

CPCP Corrosion Prevention and Control Program 

D Deleted 

EASA European Aviation Safety Agency 

FAA Federal Aviation Agency 

FC Flight Cycle 

FH Flight Hour 

FR Frame 

HFEC High Frequency Eddy Current (NDT inspection method) 

HTP Horizontal Tail Plane 

JAR Joint Aviation Requirements 

LOV Limit Of Validity 

MOD Modification 

MPD Maintenance Planning Document 

MRBR Maintenance Review Board Report 

MSN Manufacturer Serial Number 

N New 

N/A Not Applicable 

NDT Non Destructive Test 

NTM Non Destructive Test Manual 

R Revised 

RAS Repair Design Approval Sheet 

ROR Record Of Revisions 

SB Service Bulletins 

SRM Structural Repair Manual 

SSI Structural Significant Item 

STC Supplemental Type Certificate 

STR Stringer 

THS Trimmable Horizontal Stabilizer 

TPS Temporary Protection System 

TOC Table Of Contents 

US UltraSonic (NDT inspection method) 

WV Weight Variant 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX C – TERMS AND DEFINITIONS

ISSUE: FEB 20/09 PAGE: APXC-1 

©AIRBUS SAS 2009. All rights reserved. 

A340

TERM DEFINITION 

AIRCRAFT 

STRUCTURE 

Consists of all load-carrying members including wings, fuselage, 

empennage, engine mountings, landing gear, flight control surfaces, and 

related points of attachment. The actuating portions of items such as 

landing gear, flight controls, doors, etc. are treated as systems 

components. Attachment of the actuators to the airframe are treated as 

structure. 

CALENDAR TIME 

(Cal) 

In Years (Ye), in Months (Mo), etc... must be counted from the date of 

initial entry into service, unless otherwise stated. Storage, maintenance, 

etc... do not freeze calendar time accumulation. 

CONTINUED 

AIRWORTHINESS 

Is the process of ensuring that the level of airworthiness guaranteed by 

TC is maintained for each individual aircraft at the time of its entry into 

service and during all its service life. 

DAMAGE 

TOLERANCE 

CONCEPT 

The damage-tolerance evaluation of structure is intended to ensure that 

should serious fatigue, corrosion, or accidental damage occur within the 

operational life of the aeroplane, the remaining structure can withstand 

reasonable loads without failure or excessive structural deformation until 

the damage is detected. 

Damage-tolerance design is required, unless it entails such complications 

that an effective damage-tolerant structure cannot be achieved within the 

limitations of geometry, inspectability, or good design practice. Under 

these circumstances, a design that complies with the fatigue evaluation 

(safe life) requirements is used. 

DAMAGETOLERANT 

AIRWORTHINESS 

LIMITATION 

ITEMS (DT ALI) 

They are all those parts of the structure whose failure could result in 

catastrophic failure of the airplane and that are designed to fatigue and 

damage-tolerance concept. 

DESIGN SERVICE 

GOAL 

Is a reference figure selected for the design and certification of the 

aircraft. 

EXTENDED 

SERVICE GOAL Is an extension of the DSG. 

FLIGHT CYCLE 

(FC) A complete take-off and landing sequence 

FLIGHT HOUR 

(FH) The accumulated time intervals between ‘wheels-off’ and ‘wheels-on’. 

INTERVAL The maximum period expressed in usage parameters between the 

completion of a task and its next due accomplishment. 

LIMIT OF 

VALIDITY (LOV) Is a limitation to the validity of the Airworthiness Limitation Sections 

THRESHOLD 

The maximum period of time expressed in usage parameters between the 

first flight of the aircraft, and the frist due completion of the task. 

Subsequent accomplishment deadlines are obtained by adding the repeat 

interval and its multiples to the threshold. 

TOUCH AND GO A ‘Touch and go’ is a landing in which an aircraft touches the runway and 

does not come to a full stop prior to commencing an additional flight.