# AIRBUS

Customer Services Directorate



# A340 Airworthine ss 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 de scribed 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 COMPLIAN CE 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

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# A340

Issue Date Reason for revision Approved

by EASA

1 22 Aug 97 Section 2 of CMR docu ments 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.

# AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: FEB 20/09 PAGE: 2-ROR

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# 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

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# 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

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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

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INTRODUCTION

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# 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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# 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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# 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 relev ant 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

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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

A340-212 000, 001, 002 A340-200

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,

101, 102, 103 A340-500

A340-542 101, 102, 103

A340-642 000, 001,

101, 102, 103 A340-600

A340-643 101, 102, 103

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INTRODUCTION

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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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# 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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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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# 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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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.RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY521101-01-01 831 841 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 1 (FORWARD PASSENGER/CREW DOOR).11000 FC 11000 FC A340-200ORA340-300521103-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 1(FWD PASSENGER/CREW DOOR) SKIN, EXTERNALSURFACE.8500 FC 8500 FC A340-200ORA340-300521201-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 2(MID PASSENGER/CREW DOOR) SKIN,EXTERNAL SURFACE.8500 FC 8500 FC A340-200ORA340-300521203-01-01 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 2 (MID PASSENGER/CREW DOOR).11000 FC 11000 FC A340-200POST 42350ORA340-300POST 42350521203-01-02 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 2 (MID PASSENGER/CREW DOOR).6000 FC 6000 FC GROUP 42APRE 42350ORGROUP 43APRE 42350521301-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A340-200ORA340-300521303-01-01 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 4(AFT PASSENGER/CREW DOOR).11000 FC 11000 FC A340-200POST 42350ORA340-300POST 42350AIRWORTHINESS LIMITATIONS SECTION2 AIRWORTHINESS LIMITATIONSSECTION 2.1 - A340-200/300 AIRWORTHINESS LIMITATIONSA340© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 1RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340521303-01-02 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 4 (AFT PASSENGER/CREW DOOR).6000 FC 6000 FC GROUP 42APRE 42350ORGROUP 43APRE 42350522201-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNALSURFACE.8500 FC 8500 FC A340-200ORA340-300522203-01-01 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).11000 FC 11000 FC A340-200POST 42350ORA340-300POST 42350522203-01-02 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 3 (EMERGENCY/PASSENGER/ CREW DOOR).6000 FC 6000 FC GROUP 42APRE 42350ORGROUP 43APRE 42350R 523106-01-01 821CRDOOR LOCKING HANDLEUNLOCKEDDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR FR 20B BETWEEN BEAM 3 AND 4.10600 FC 2600 FC A340-200PRE 51038ANDPRE 50528ORA340-300PRE 51038ANDPRE 50528524101-01-01 N/A DETAILED INSPECTION OF AVIONICS COMPARTMENTLOWER ACCESS DOOR SKIN, EXTERNAL SURFACE.10400 FC 10400 FC A340-200ORA340-300R528104-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR MAINDOOR, CENTER FITTING AND SURROUNDING AREA (300MM AROUND), LH/RH.2650 FC 2650 FC GROUP 43APRE 41535ORGROUP 42APRE 41535© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 2RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R528104-01-02 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR MAINDOOR CENTER FITTING AND SURROUNDING AREA (300 MMAROUND), LH/RH.8300 FC 8300 FC GROUP 43BORGROUP 43CORGROUP 42BORGROUP 43APOST 41535ORGROUP 42APOST 41535ORGROUP 43E528203-01-01 713 714 DETAILED INSPECTION OF NOSE LANDING GEARFORWARD DOOR, HINGES (NO.1, NO.2, NO.3) INCLUDINGFITTINGS ON FUSELAGE, LH/RH.9600 FC 9600 FC A340-200ORA340-300528303-01-02 753 754 DETAILED INSPECTION OF CENTER LANDING GEAR, MAINDOOR FITTINGS, LH/RH.21600 FC 3950 FC GROUP 43C531110-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD,EXTERNAL SURFACE, LH/RH.18500 FC 18500 FC A340-200ORA340-300531112-02-01 N/A DETAILED INSPECTION OF FUSELAGE STRUCTUREAROUND DOOR 1 (FORWARD PASSENGER/CREW DOOR), ,EXTERNAL SURFACE, BETWEEN FR 13 AND FR 18 FROMLATERAL LONGITUDINAL LAP JOINT TO STR 9 AFT, LH/RH.9000 FC 9000 FC A340-200ORA340-300531118-01-01 713 714 121AL121ELGENERAL VISUAL INSPECTION OF GROUND SERVICESCONNECTING ACCESS DOORS CUTOUTS AND NOSELANDING GEAR CUTOUT, BETWEEN FR 4 AND FR 19 ONLOWER FUSELAGE.3100 FC 3100 FC A340-200ORA340-300531120-01-02 713 714 GENERAL VISUAL INSPECTION OF NLG BAY INTERNALSTRUCTURE, NOSE LANDING GEAR WELL PANELS.1400 FC 1400 FC A340-200ORA340-300© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 3RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531131-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR16A JOINT AREA BETWEEN STRS 28 AND30, LH/RH.NOTE : TASK TO BE PERFORMED IN CONJUCTION WITHTASK 531131-02-0118500 FC 9800 FC GROUP 42APRE 44258ORGROUP 43APRE 44258ORGROUP 43BPRE 44258531131-02-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 16A JOINT AREA BETWEEN STRS 28 AND30, LH/RH.NOTE : TASK TO BE PERFORMED IN CONJUNCTION WITHTASK 531131-01-01.18500 FC 9800 FC GROUP 42APRE 44258ORGROUP 43APRE 44258ORGROUP 43BPRE 44258531133-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONAIR DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAMJUNCTION ON FR12A AT STR 26 LEVEL LH/RH.22600 FC 9800 FC GROUP 43C531135-01-01 N/A SPECIAL DETAILED INSPECTION OF REAR LOWER CORNEROF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OFFR 10, EXTERNAL SURFACE, LH/RH4850 FC 4850 FC A340-200ORA340-300531136-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONCEILING PANELSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRS 12 AND 13 DOUBLER AREA AT CROWNCENTERLINE.17500 FC 10100 FC GROUP 42APRE 42481ORGROUP 43APRE 42481© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 4RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531140-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGS, 831GALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LATERAL FRAME 10 ATFLOOR LEVEL ATTACHMENT, ABOVE COCKPIT FLOOR,INTERNAL STRUCTURE, LH/RH.15700 FC 8400 FC GROUP 42APRE 42829ORGROUP 43APRE 42829ORGROUP 43BPRE 42829531141-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSDETAILED INSPECTION OF LATERAL FR11, SPLICE ABOVECOCKPIT FLOOR LEVEL ATTACHMENT, INTERNALSTRUCTURE, LH/RH.17600 FC 9080 FC GROUP 42APRE 41652ORGROUP 43APRE 41652531143-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONAIR DUCTSVACUUM PIPESDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING ATFR 14, LH/RH.16600 FC 4000 FC GROUP 42AORGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C531144-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGTOILETSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FR 14 ANDCRUCIFORM FITTING, LH/RH.16600 FC 7100 FC GROUP 42AORGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 5RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531154-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSSLIDING WINDOWSOPENEDDETAILED INSPECTION OF LOWER SURFACE OF UPPERCLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELDSIDE POST, INTERNAL STRUCTURE, LH/RH.13000FC 8100 FC GROUP 42AORGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43C531161-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSDETAILED INSPECTION OF PAX / CREW DOOR UPPER KEELFITTING AT FR 18 FORWARD AND AFT FACE AT STGR 12LEVEL, INTERNAL STRUCTURE, LH/RH.14100 FC 10700 FC GROUP 42APRE 41675ORGROUP 43APRE 41675531175-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE AT JUNCTION BETWEEN FR 17 AND MACHINEDSTIFFENERS AT STRS 14/18/22/24, LH/RH.22700 FC 8000 FC GROUP 43C531192-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FR 13 FORWARDFACE AND STR 9 FORWARD, AND FR 13 AFT FACE AND STR12, LH/RH.21900 FC 8100 FC GROUP 43C531194-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLININGSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, MACHINED STIFFENERS 14 AND 22 BETWEENFR 17 AND FR 18, LH/RH.21900 FC 8100 FC GROUP 43CR 532101-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 18 AND FR 38 FROMSTR 26 TO BOTTOM CENTER LINE, INCLUDING SKINSPLICES AND LAP JOINTS, EXCLUDING AREASUNDERNEATH BELLY FAIRING, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-022200 FC 2200 FC A340-200ORA340-300© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 6RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N 532101-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TOBOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAPJOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-016900 FC 6900 FC A340-200ORA340-300R 532114-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENTDOOR CUTOUT AT UPPER AND LOWER CORNERS.10800 FCOR60000 FH8500 FCOR51000 FHA340-200ORGROUP 43AORGROUP 43B532114-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENTDOOR CUTOUT AT UPPER AND LOWER CORNERS.10800 FCOR21600 FH9180 FCOR18360 FHGROUP 43C532114-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENTDOOR CUTOUT AT UPPER AND LOWER CORNERS.13000 FC 10000 FC GROUP 43E532115-01-02 821 GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERALFRAMES (FR 20A AND FR 25A).3500 FC 3500 FC A340-200ORA340-300R 532117-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROMSTR6 TO STR 26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-0213000 FC 2200 FC A340-200ORA340-300N 532117-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR18 AND FR 38 FROM STR6 TO STR26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-0113000 FC 6900 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 7RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 532124-02-01 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.10800 FC 2500 FC GROUP 42APRE 45293PRE 41856ORGROUP 43APRE 45293PRE 41856R 532124-02-02 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.13800 FC 8000 FC GROUP 42APOST 45293PRE 41856ORGROUP 43APOST 45293PRE 41856R 532124-02-03 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.16000 FC 3850 FC A340-200POST 41856ORGROUP 43APOST 41856ORGROUP 43BPOST 41856532124-02-04 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.16000 FC 4000 FC GROUP 43EN 532124-02-05 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.16000 FC 4200 FC GROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 8RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 532125-01-01 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNER, LH/RH.10800 FC 2500 FC GROUP 42APRE 45293PRE 41856ORGROUP 43APRE 45293PRE 41856R 532125-01-02 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNER, LH/RH.13800 FC 8000 FC GROUP 42APOST 45293PRE 41856ORGROUP 43APOST 45293PRE 41856R 532125-01-03 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNER, LH/RH.16000 FC 3890 FC A340-200POST 41856ORGROUP 43APOST 41856ORGROUP 43BPOST 41856532125-01-04 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNER, LH/RH.16000 FC 4000 FC GROUP 43EN 532125-01-05 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNER, LH/RH.16000 FC 4200 FC GROUP 43CPOST 41856532128-01-01 832 842 GENERAL VISUAL INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) STOP FITTINGS ON FR 33 ANDFR 35A, LH/RH.14000 FC 14000 FC A340-200ORA340-300© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 9RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340532129-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.21000 FCOR42000 FH11500 FCOR23000 FHGROUP 43C532130-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE 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.25000 FC 10000 FC GROUP 43C532138-01-01 821 131AGDRAINMASTDETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37 ANDFR 37.1, FROM STR 53 TO STR 54, LH ONLY.20000 FC 8000 FC GROUP 43C532142-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND TCAS ANTENNACUT-OUT BETWEEN FR 19 AND FR 20, ON CROWN CENTERLINE, EXTERNAL SURFACE.24000 FC 16000 FC GROUP 43CR 532143-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND GPS ANTENNACUT-OUTS BETWEEN- FR 35 AND FR 36 AND- FR 37 AND FR 37.1,ON CROWN CENTER LINE, EXTERNAL SURFACE.24000 FC 8600 FC GROUP 43CR 532144-01-01 832 842CEILING PANELSNOTE 1DETAILED INSPECTION OF FRAMES AND STRINGERCOUPLING AREA, BETWEEN FR 32 AND FR 34, FROM STR 9TO STR 13 LH/RH, INTERNAL STRUCTURE.20000 FC 10000 FC GROUP 43C532145-01-01 N/A GENERAL VISUAL INSPECTION OF SKIN AT SHEAR TIEATTACHMENTS 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, EXTERNALSURFACE.22800 FC 12000 FC GROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 10RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340532146-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 26 FROM STR 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.24000 FC 16000 FC GROUP 43CR 532147-01-01 821CARGO COMPARTMENTFLOOR PANELSLININGSNOTE1DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTSOF CARGO FLOOR ATTACHMENT FITTINGS,- FROM FR 20 TO FR 38 LH,- FROM FR 26 TO FR 38 RH,BETWEEN STR 34 AND STR 43.20000 FC 10000 FC GROUP 43C532148-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREA AT FR 31 FROM STR 9 TO STR 15 LH/RH, EXTERNALSURFACE.24000 FC 12000 FC GROUP 43C532149-01-01 832 842CEILING AND SIDE WALLPANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE AT FR 26, FROM- STR 4 TO STR 6,- STR 12 TO STR 14 AND- STR 21 TO STR 22,LH/RH.24000 FC 16000 FC GROUP 43C532150-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 ANDFR 37.1.20000 FCOR40000 FH4500 FCOR9000 FHGROUP 43C532152-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AT SHEAR TIEATTACHMENT BETWEEN FR 26 AND FR 37.1, FROM STR 13TO STR 31 LH/RH, EXTERNAL SURFACE.20000 FCOR40000 FH8000 FCOR16000 FHGROUP 43C532153-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOWVALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32AND FR 33, FROM STR 45 TO STR 49, LH ONLY.15000 FC 7000 FC A340-200ORA340-300532154-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE 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.20000 FC 6000 FC GROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 11RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340532155-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN DOUBLER ATPRESSURE RELIEF VALVE CUT-OUT, BETWEEN FR 24 ANDFR 25, FROM STR 26 TO STR 30, LH ONLY.20000 FC 6500 FC GROUP 43C532156-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE LH/RH.20000 FCOR40000 FH4500 FCOR9000 FHGROUP 43C532157-01-01 832 842SIDE WALL LININGINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR15, LH/RH.15000 FC 4500 FC A340-200PRE 46636ORGROUP 43APRE 46636ORGROUP 43BPRE 46636532158-01-01 833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 38, FROM STR 13 TOCROWN CENTERLINE, LH/RH.15000 FCOR90000 FH4500 FCOR27000 FHA340-200PRE 46636532158-02-01 833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTERLINE, LH/RH.15000 FCOR90000 FH4500 FCOR27000 FHGROUP 43APRE 46636ORGROUP 43BPRE 46636532159-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 1 ANTENNACUT-OUT BETWEEN FR 22 AND FR 23, ON CROWN CENTERLINE, EXTERNAL SURFACE.24000 FC 12000 FC GROUP 43C532160-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND ATC 1+2ANTENNA CUT-OUT BETWEEN FR 24 AND FR 25, ANDBETWEEN STR 2 AND STR 3, LH/RH, EXTERNAL SURFACE.24000 FC 12000 FC GROUP 43CPOST 40255532161-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND SATCOM(LG)ANTENNA CUT-OUT BETWEEN FR 26 AND FR 26.1 ONCROWN CENTER LINE, EXTERNAL SURFACE.24000 FC 12000 FC GROUP 43CPOST 43560ORGROUP 43CPOST 43956© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 12RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340532162-01-01 831 841OVERHEAD STOWAGECOMPARTMENT DOORMAINTENANCE DOORANTENNADETAILED INSPECTION OF SKIN AROUND SATCOM (45DEGREE) ANTENNA CUT-OUT BETWEEN FR 26.1 AND FR26.3 AND BETWEEN STR 12 AND STR 13, LH/RH, EXTERNALSURFACE.24000 FC 12000 FC GROUP 43CPOST 44620ORGROUP 43CPOST 41833ORGROUP 43CPOST 45503532163-01-01 ANTENNA REAR FAIRINGCOVER AND BRACKETDETAILED INSPECTION OF SKIN AROUND SATCOM (HG)ANTENNA CUT-OUT BETWEEN FR 26.4 AND FR 27, ONCROWN CENTER LINE, EXTERNAL SURFACE.24000 FC 12000 FC GROUP 43CPOST 43652532165-01-01 831 841CEILING PANELSLININGINSULATION .SPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 ANDFR 38.15000 FCOR90000 FH4500 FCOR27000 FHA340-200PRE 46636532165-02-01 831 841CEILING PANELSLININGINSULATION .SPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31 ANDFR 37.1.15000 FCOR90000 FH4500 FCOR27000 FHGROUP 43APRE 46636ORGROUP 43BPRE 46636N 532166-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROMSTR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-024500 FC 4500 FC A340-200ORA340-300N 532166-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TOCROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-016900 FC 6900 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 13RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533005-01-01 191AB 191AT 191BB191CB 192AT 192BB192CB 197AT 197FB197GB 197HB 198AT198GB 198HBDETAILED INSPECTION OF FUSELAGE SKIN AT BELLYFAIRING SEALING LIP ATTACHMENT FROM FR 37.1 TO FR 38AND FROM FR 53.6 TO FR 56.15200 FCOR103100 FH4750 FCOR32300 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43EN533005-01-02 191AB 191AT 191BB191CB 192AT 192BB192CB 197AT 197FB197GB 197HB 198AT198GB 198HBDETAILED INSPECTION OF FUSELAGE SKIN AT BELLYFAIRING SEALING LIP ATTACHMENT FROM FR 37.1 TO FR 38AND FROM FR 53.6 TO FR 56.15200 FCOR30500 FH5050 FCOR10100 FHGROUP 43CR533103-02-01 N/A DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, SKIN PANEL RIVETING ON FR 40 FROM STR17 TO STR 19, LH/RH.15100 FCOR102100 FH7300 FCOR49500 FHGROUP 42APRE 41652PRE 45749ORGROUP 43APRE 41652PRE 45749R533104-01-02 ANTICOLLISION LIGHT:LENS 7LVADF: LENSES 2RP1 & SEALAND 2RP2 & SEALPOST 49842: OBTURATOROF AIRLINE IN-FLIGHTINFORMATION SERVICESANTENNA CUTOUT.DETAILED INSPECTION OF FUSELAGE SKIN BETWEENSTRINGER 1 LH AND 1 RH 50MM AROUND:- UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 ANDFR.43- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEENFR.48 AND FR.49 AND BETWEEN FR.52 AND FR.53- AFIS ANTENNA CUTOUT BETWEEN FR.40 AND FR.40.1 (IFINSTALLED)25300 FCOR50700 FH7200 FCOR14400 FHGROUP 43CR533105-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING AND AIRCONDITIONINGDUCTS.SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER HOLE AREA ABOVE STRINGER 28AT FR 39.1 WEB JUNCTION ON HOIST FITTING, LH/RH.13600 FCOR92100 FH7850 FCOR53300 FHGROUP 42APRE 40391ORGROUP 43APRE 40391© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 14RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533106-01-01 N/A DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STR 18 AND STR22, FROM FRAME 38 TO 53.3, LH/RH.24900 FCOR49900 FH8450 FCOR16900 FHGROUP 43CR533107-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING AND AIRCONDITIONINGDUCTS.SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE , FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.18300 FCOR123700 FH10400 FCOR70600 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BR533107-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING AND AIRCONDITIONINGDUCTS.SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE , FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.24000 FCOR48100 FH12700 FCOR25400 FHGROUP 43CR533111-01-01 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FIRST FASTENERS ROW AREA ABOVE STR 39BETWEEN FR 53.2 AND FR 53.3, LH/RH.10000 FCOR67700 FH3750 FCOR25300 FHGROUP 42APRE 42607ORGROUP 43APRE 42607R533113-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENER ROWS AT FR 47 FROM BELOWSTR 22 TO ABOVE STR 24 LEVEL, LH/RH.17200 FCOR116300 FH9200 FCOR62300 FHGROUP 42AORGROUP 43AR533113-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENER ROWS AT FR 47 FROM BELOWSTR 22 TO ABOVE STR 24 LEVEL, LH/RH.12300 FCOR83000 FH6500 FCOR44000 FHGROUP 42BORGROUP 43BR533113-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENER ROWS AT FR 47 FROM BELOWSTR 22 TO ABOVE STR 24 LEVEL, LH/RH.15000 FCOR30000 FH6200 FCOR12400 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 15RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533113-01-04 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENER ROWS AT FR 47 FROM BELOWSTR 22 TO ABOVE STR 24 LEVEL, LH/RH.12300 FCOR83200 FH6100 FCOR41000 FHGROUP 43ER533114-01-01 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERSTRS 20 TO 23, LH/RH.13000 FCOR87700 FH6000 FCOR40500 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BR533114-01-02 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 WEB AT JUNCTION WITH STABILIZERSTRS 20 TO 23, LH/RH.15000 FCOR30000 FH6000 FCOR12000 FHGROUP 43CR533115-01-01 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 ,LH/RH.17000 FCOR115000 FH8450 FCOR57100 FHGROUP 42AORGROUP 43AR533115-01-02 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 ,LH/RH.12000 FCOR81200 FH6600 FCOR44600 FHGROUP 42BORGROUP 43BR533115-01-03 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 ,LH/RH.15700 FCOR31500 FH6900 FCOR13900 FHGROUP 43C533115-01-04 251XW 252XWINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 47 STABILIZERS FROM STRS 19 TO 23 ,LH/RH.12000 FCOR81000 FH6500 FCOR44000 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 16RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533116-01-01 753 754FASTENERSSPECIAL DETAILED INSPECTION OF CENTER LANDINGGEAR TRUNNION FITTING, BEAM Y = 450, FIRST 2FASTENER HOLES AT ATTACHMENT TO OUTER SKIN,LH/RH.7400 FCOR28500 FH5300 FCOR22500 FHGROUP 42APRE 45300PRE 46190S14154ORGROUP 43APRE 45300PRE 46190S14154ORGROUP 42BPRE 45300PRE 46190S14154ORGROUP 43BPRE 45300PRE 46190S14154R533125-01-02 734 744 753754GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENTAREA OF THE CENTER LANDING GEAR TRUNNIONFITTINGS.1500 FCOR10100 FH1500 FCOR10100 FHGROUP 42AORGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43EN533125-01-03 734 744 753754GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR53.2 PRESSURE BULKHEAD, INCLUDING THE ATTACHMENTAREA OF THE CENTER LANDING GEAR TRUNNIONFITTINGS.1500 FCOR3000 FH1500 FCOR3000 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 17RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533126-01-02 734 744 753754GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CENTER LANDING GEAR AND MAIN LANDINGGEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.3800 FCOR26200 FH3800 FCOR26200 FHGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43ER533126-01-03 734 744 753754GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CENTER LANDING GEAR AND MAIN LANDINGGEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.3300 FCOR22800 FH3300 FCOR22800 FHGROUP 42AR533126-01-04 734 744 753754GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CENTER LANDING GEAR AND MAIN LANDINGGEAR CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.4600 FCOR9250 FH4600 FCOR9250 FHGROUP 43CR533127-01-01 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0CM (6.0 IN) EXTERNAL SURFACE.3800 FCOR26200 FH3800 FCOR26200 FHGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43ED533127-01-02TASK DELETED IN ALI ISSUE 11R533127-03-01 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0CM (6.0 IN) EXTERNAL SURFACE.3300 FCOR22800 FH3300 FCOR22800 FHGROUP 42AR533127-03-02 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0CM (6.0 IN) EXTERNAL SURFACE.4600 FCOR9250 FH4600 FCOR9250 FHGROUP 43CD533127-03-03TASK DELETED IN ALI ISSUE 11R533132-02-02 753 754 SPECIAL DETAILED INSPECTION OF CLG TRUNNIONFITTING, BEAM Y = 450 LOWER INBOARD AND OUTBOARDFLANGES RADIUS, LH/RH.20700 FCOR41500 FH9550 FCOR19100 FHGROUP 43CPRE 46190-S14212© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 18RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533134-02-01 753 754SPHERICAL BEARINGACTUATORDISCONNECTEDSPECIAL DETAILED INSPECTION OF ATTACH FITTING FORCLG ACTUATOR AND ITS ATTACHMENT TO THE CENTERLINE STIFFENER AT FR 53.2.14300 FCOR96700 FH6000 FCOR40500 FHGROUP 42AORGROUP 42BORGROUP 43AORGROUP 43BORGROUP 43EN533134-02-02 753 754SPHERICAL BEARINGACTUATORDISCONNECTEDSPECIAL DETAILED INSPECTION OF ATTACH FITTING FORCLG ACTUATOR AND ITS ATTACHMENT TO THE CENTERLINE STIFFENER AT FR 53.2.14300 FCOR28600 FH6000 FCOR12000 FHGROUP 43CR533139-01-01 753 754 755756SPECIAL DETAILED INSPECTION OF VERTICAL BEAM AT Y =0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLGACTUATOR FITTING UPPER END.15250 FCOR102900 FH5550 FCOR37600 FHGROUP 42APOST 42606S11993ORGROUP 43APOST 42606S11993R533139-01-03 753 755 754756SPECIAL DETAILED INSPECTION OF VERTICAL BEAM AT Y =0 AT FRAME LEVEL 53.2, FASTENERS AREA AT CLGACTUATOR FITTING UPPER END.20600 FCOR41200 FH8050 FCOR16100 FHGROUP 43CR533145-01-02 197AT 197HB 198AT198HBSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 31 LEVEL FROM FR 53.3TO FR 54, LH/RH.13000 FCOR26000 FH6050 FCOR12100 FHGROUP 43CR533154-01-01 CABIN FLOOR PANELSGALLEYS AND TOILETS (IFINSTALLED)DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1,LH/RH.13000 FCOR88000 FH8050 FCOR54600 FHGROUP 42APRE 41652ORGROUP 43APRE 41652© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 19RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533154-01-03 CABIN FLOOR PANELSGALLEYS AND TOILETS (IFINSTALLED)DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FR 48 TO FR 53.1,LH/RH.20000 FCOR40000 FH13300 FCOR26600 FHGROUP 43CR533162-01-01 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEARBAY, LOWER FLANGE OF GANTRY Y = 1456, 40 FASTENERSFORWARD AND AFT OF FR 48 DATUM, LH/RH.16200 FCOR109600 FH9000 FCOR61000 FHGROUP 42APRE 43852ORGROUP 43APRE 43852ORGROUP 43BPRE 43852R533163-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY ,CANTED DIAPHRAGMS AND CANTED DIAPHRAGMSJUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48FROM Y = 0 TO Y = 450, LH/RH.9200 FCOR62300 FH4000 FCOR27100 FHGROUP 42APRE 41652PRE 46354ORGROUP 43APRE 41652PRE 46354R533164-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY ,CANTED DIAPHRAGMS AND CANTED DIAPHRAGMSJUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48FROM Y = 450 TO Y = 1959, LH/RH.16900 FCOR114100 FH8800 FCOR59600 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BR533164-01-02 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY ,CANTED DIAPHRAGMS AND CANTED DIAPHRAGMSJUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48FROM Y = 450 TO Y = 1959, LH/RH.21300 FCOR42600 FH9900 FCOR19800 FHGROUP 43CR533164-01-03 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR BAY ,CANTED DIAPHRAGMS AND CANTED DIAPHRAGMSJUNCTION ON FLOOR BEAMS BETWEEN FR 47 AND FR 48FROM Y = 450 TO Y = 1959, LH/RH.17800 FCOR120000 FH8300 FCOR56300 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 20RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533165-01-01 251MG 251SG 252MG252SGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONGALLEYS AND TOILETS (IFINSTALLED).DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FR 48 TO FR 53.1, HORIZONTAL LEG ATSTRINGER PASSAGE, LH/RH.11900 FCOR80300 FH8400 FCOR56900 FHGROUP 42APOST 43904ORGROUP 43APOST 43904R 533180-01-01 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEEN FR53.6 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)15000 FCOR100000 FH3540 FCOR26000 FHA340-200ORGROUP 43AORGROUP 43BR 533180-01-02 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEEN FR53.6 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)15000 FCOR100000 FH3800 FCOR7600 FHGROUP 43CR 533181-01-01 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL 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)16000 FCOR80000 FH6550 FCOR49000 FHA340-200ORGROUP 43AORGROUP 43B533181-01-02 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL 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)16000 FCOR32000 FH7200 FCOR14400 FHGROUP 43C533181-01-03 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL 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)13000 FCOR95700 FH8000 FCOR58900 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 21RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533184-01-01 N/A DETAILED INSPECTION OF SKIN AT SHEAR TIEATTACHMENTS BETWEEN FR 53,4 AND FR 53,9 FROMSTRINGER 13 LH/RH TO CROWN CENTER LINE, EXTERNALSURFACE.22800 FCOR48000 FH12000 FCOR24000 FHGROUP 43C533192-01-01 834 844 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGSOF DOOR 3 EMERGENCY/PASSENGER/CREW DOOR) AT FR53.5 AND 53.7 A, LH/RH.14000 FC 14000 FC A340-200ORA340-300533193-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN(INCLUDING DOOR 3 CUTOUT) BETWEEN FR 53.3 AND FR 54FROM UPPER EDGE OF BELLY FAIRING TO CROWNCENTER LINE, EXTERNAL SURFACE, LH/RH.3600 FC 3600 FC A340-200ORA340-300R 533194-01-01 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.10800 FCOR78000 FH4800 FCOR37300 FHGROUP 42ADOOR TYPE 1ORGROUP 43ADOOR TYPE 1ORGROUP 43BDOOR TYPE 1R 533194-01-02 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.18000 FCOR130000 FH6750 FCOR48750 FHGROUP 42ADOOR TYPE APOST 42351PRE 42352ORGROUP 43ADOOR TYPE APOST 42351PRE 42352© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 22RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 533194-01-03 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.18000 FCOR130000 FH4050 FCOR29250 FHGROUP 42ADOOR TYPE APOST 42352ORGROUP 43ADOOR TYPE APOST 42352R 533194-01-04 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.10800 FCOR78000 FH7400 FCOR58100 FHGROUP 42ADOOR TYPE APOST 41848ORGROUP 43ADOOR TYPE APOST 41848ORGROUP 43BDOOR TYPE APOST 41848R 533194-01-05 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.13000 FCOR101000 FH6000 FCOR46600 FHGROUP 43ER 533194-01-06 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS LH/RH.10800 FCOR21500 FH5580 FCOR11160 FHGROUP 43CDOOR TYPE 1R 533194-01-09 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS, LH/RH.10800 FCOR21600 FH8640 FCOR17280 FHGROUP 43CDOOR TYPE APOST 41848© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 23RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 533195-02-01 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.10800 FCOR78000 FH4800 FCOR37300 FHGROUP 42ADOOR TYPE 1ORGROUP 43ADOOR TYPE 1ORGROUP 43BDOOR TYPE 1R 533195-02-02 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.18000 FCOR130000 FH6750 FCOR48750 FHGROUP 42ADOOR TYPE APOST 42351ORGROUP 43ADOOR TYPE APOST 42351R 533195-02-03 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.18000 FCOR130000 FH4050 FCOR29250 FHGROUP 42ADOOR TYPE APOST 42352ORGROUP 43ADOOR TYPE APOST 42352R 533195-02-04 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.10800 FCOR78000 FH7400 FCOR58100 FHGROUP 42ADOOR TYPE APOST 41848ORGROUP 43ADOOR TYPE AR 533195-02-05 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.13000 FCOR101000 FH6000 FCOR46600 FHGROUP 43ER 533195-02-06 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH10800 FCOR21500 FH5580 FCOR11160 FHGROUP 43CDOOR TYPE 1© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 24RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 533195-02-09 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.10800 FCOR21500 FH8640 FCOR17280 FHGROUP 43CDOOR TYPE APOST 41848R 534102-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 58 FROM STR 13 TO CROWN CENTERLINE,EXTERNAL SURFACE, LH/RH.8290 FCOR58000 FH8290 FCOR58000 FHGROUP 42APRE 40556ORGROUP 43APRE 40556534102-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 58 FROM STR 13 TO CROWN CENTERLINE,EXTERNAL SURFACE, LH/RH.22000 FCOR44000 FH11800 FCOR23600 FHGROUP 43C534104-01-01 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 2212750 FCOR90000 FH8500 FCOR60000 FHA340-200POST 40556ORGROUP 43APOST 40556ORGROUP 43BPOST 40556R 534104-01-02 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 226970 FCOR48800 FH5950 FCOR42000 FHGROUP 42APRE 40556R 534104-01-03 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM:- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 229920 FCOR69400 FH8500 FCOR60000 FHGROUP 43APRE 40556© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 25RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340534104-01-05 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 2212750 FCOR25500 FH8500 FCOR17000 FHGROUP 43CPOST 40556534104-01-06 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, LH/RH, FROM :- STR 4 TO STR 6- STR 12 TO STR 14- STR 21 TO STR 2213000 FCOR101000 FH8000 FCOR56000 FHGROUP 43ER 534105-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STR 13 TO CROWN CENTERLINE,EXTERNAL SURFACE, LH/RH.13000 FCOR92000 FH7000 FCOR50000 FHGROUP 42APRE 40556ORGROUP 43APRE 40556534105-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STR 13 TO CROWN CENTERLINE,EXTERNAL SURFACE, LH/RH.24000 FCOR48000 FH16000 FCOR32000 FHGROUP 43C534107-01-01 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.12750 FCOR97500 FH8500 FCOR65000 FHA340-200ORGROUP 43AORGROUP 43B534107-01-03 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.12750 FCOR25500 FH8500 FCOR17000 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 26RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340534107-01-04 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.13000 FCOR116300 FH8000 FCOR71500 FHGROUP 43E534108-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 76 FROM STRINGER 13 LH/RH TO CROWNCENTER LINE, EXTERNAL SURFACE.22800 FCOR45600 FH15200 FCOR30400 FHGROUP 43C534110-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKINCIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80FROM STRINGERS 6 TO 13 LH/RH, EXTERNAL SURFACE22800 FCOR45600 FH15200 FCOR30400 FHGROUP 43C534120-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGING BETWEEN FR 53.8 AND FR 73AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNALSURFACE.22800 FCOR45600 FH13490 FCOR26980 FHGROUP 43C534122-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN ATSHEAR 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 FINTO FUSELAGE FAIRING.22800 FCOR45600 FH12000 FCOR24000 FHGROUP 43CR 534124-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR 54 AND 80 FROM STR6 TO STR 26 LH/RH,EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-02-01.13000 FC 2200 FC A340-200ORA340-300R 534124-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR54 AND 80 FROM STR6 TO STR 26 LH/RH, EXTERNALSURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534124-01-13000 FC 6900 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 27RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 534126-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 54 AND FR 80 FROMSTR 26 LH/RH TO BOTTOM CENTERLINE, INCLUDING SKINSPLICES AND LAP JOINTS AND INCLUDING THE LOWER,UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRINGAND FORWARD OF FR 54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-02-012200 FC 2200 FC A340-200ORA340-300R 534126-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 LH/RHTO BOTTOM CENTERLINE, INCLUDING SKIN SPLICES ANDLAP JOINTS AND INCLUDING THE LOWER, UNCOVEREDAREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARDOF FR 54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-01-016900 FC 6900 FC A340-200ORA340-300R 534131-01-01 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.10800 FC 7700 FC A340-200ORGROUP 43AORGROUP 43B534131-01-02 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.13000 FCOR102600 FH8000 FCOR63100 FHGROUP 43EN 534131-01-03 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.10800 FC 8000 FC GROUP 43CR 534132-02-01 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.10800 FC 7700 FC A340-200ORGROUP 43AORGROUP 43B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 28RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340534132-02-02 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.13000 FCOR102600 FH8000 FCOR63100 FHGROUP 43EN 534132-02-03 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE, LH/RH.10800 FC 8000 FC GROUP 43C534135-01-01 833 843 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGSOF DOOR 4 (AFT PASSENGER /CREW DOOR) AT FR 73AAND FR 75A, LH/RH.14000 FC 14000 FC A340-200ORA340-300R 534136-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN OFAFT CARGO COMPARTMENT DOOR CUT-OUT AT UPPERREAR AND LOWER FORWARD CORNERS, EXTERNALSURFACE.10100 FCOR67800 FH2200 FCOR14700 FHGROUP 42APRE 41045ORGROUP 43APRE 41045534137-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER AND LOWERCORNERS, EXTERNAL SURFACE.10800 FCOR66000 FH5940 FCOR36300 FHA340-200ORGROUP 43AORGROUP 43B534137-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER AND LOWERCORNERS, EXTERNAL SURFACE.10800 FCOR21600 FH5940 FCOR11880 FHGROUP 43C534137-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER AND LOWERCORNERS, EXTERNAL SURFACE.13000 FCOR86600 FH7000 FCOR46600 FHGROUP 43E534139-01-02 822 GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR 59A AND FR 65) AS FAR AS VISIBLE.3500 FC 3500 FC A340-200ORA340-300534140-02-02 822 GENERAL VISUAL INSPECTION OF LOCK FITTINGS BUSHESFOR AFT CARGO COMPARTMENT DOOR AT 10 POSITIONSBETWEEN FR 59A AND FR 65.7500 FC 7500 FC A340-200ORA340-300© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 29RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 534143-01-01 N/A DETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERSEXTERNAL SURFACE.9700 FCOR71700 FH5600 FCOR41900 FHA340-200ORGROUP 43AORGROUP 43B534143-01-03 N/A DETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERSEXTERNAL SURFACE.10200 FCOR24000 FH6375 FCOR12750 FHGROUP 43C534143-01-04 N/A DETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERSEXTERNAL SURFACE.13000 FCOR95700 FH8000 FCOR58900 FHGROUP 43ER 534144-02-01 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.9700 FCOR71700 FH5600 FCOR41900 FHA340-200ORGROUP 43AORGROUP 43BR 534144-02-02 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.10200 FCOR24000 FH6375 FCOR12750 FHGROUP 43CR 534144-02-03 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.13000 FCOR95700 FH8000 FCOR58900 FHGROUP 43E534146-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT DOOR STOP FITTINGS AT 10 POSITIONS ATFR 67 AND FR 69.10000 FC 10000 FC A340-200ORA340-300534148-01-01 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNACUT-OUT BETWEEN FR 56 AND FR 57 FROM STRINGERS 2LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.22800 FCOR45600 FH8170 FCOR16340 FHGROUP 43C534149-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR 67 AND FR 69) AS FAR AS VISIBLE.3500 FC 3500 FC A340-200ORA340-300© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 30RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 534150-01-01 823LININGNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTSOF 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 50.20000 FC 10000 FC GROUP 43C534154-01-01 833 843LININGINSULATIONDETAILED INSPECTION OF INTERNAL STRUCTURE OFTORSION BOX, INCLUDING SKIN AND SPLICE PLATE,BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 AND FR76, LH/RH.20000 FC 8000 FC GROUP 43C534155-01-01 833 843LININGINSULATIONSPECIAL DETAILED INSPECTION OF TORSION BOXLONGITUDINAL BEAM ADJACENT TO RUN OUT OF CORNERDOUBLER BETWEEN FR 73A AND FR 74, LH/RH.20000 FC 8000 FC GROUP 43C534156-01-02 822LININGCARGO FLOOR PANELSINSULATIONDETAILED INSPECTION OF INTERNAL STRUCTURE BELOWAFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR59 AND FR 67, FROM CARGO FLOOR LEVEL TO STR 47 RH.15000 FC 8000 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 31RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340534166-01-01 ANTENNA SPECIAL DETAILED INSPECTION OF SKIN AROUND VHF 2ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROMSTR 56 TO STR 57, RH.13000 FC 4700 FC A340-200POST 46025PRE 46849PRE 48442ORGROUP 43APOST 46025PRE 46849PRE 48442ORGROUP 43BPOST 46025PRE 46849PRE 48442ORGROUP 43CPOST 46025PRE 46849PRE 48442N 534177-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR 54 AND 80 FROM STR6 LH/RH TO CROWNCENTER LINE EXCLUDING AREA UNDER VERTICALSTABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-014500 FC 4500 FC A340-200ORA340-300N 534177-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINEEXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING,EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-01-016900 FC 6900 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 32RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340535103-01-02 312AR DETAILED INSPECTION OF REAR PRESSURE BULKHEADAFT FACE, INCLUDING ATTACHMENT TO SKIN, BETWEENSTRINGERS 26 LH/RH AND CROWN CENTERLINE.16500 FC 7500 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C535104-02-01 312AR GENERAL VISUAL INSPECTION OF REAR PRESSUREBULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN,BETWEEN STRINGERS 26 LH/RH AND BOTTOM CENTERLINE.3600 FC 3600 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C535109-01-01 313ALHINGE ARMSSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER HINGE SUPPORT MEMBERS AND UPPER ANDLOWER ATTACHMENT LUGS OF FR 91, LH/RH.20000 FC 20000 FC GROUP 43CD545104-01-01 TASK DELETED IN ALI ISSUE 11D545104-01-02 TASK DELETED IN ALI ISSUE 11D545104-01-06 TASK DELETED IN ALI ISSUE 11R545142-01-01 453CL 453CR 463CL463CR 473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.13000 FCOR87700 FH13000 FCOR87700 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43B545142-01-02 453CL 453CR 463CL463CR 473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.13000 FCOR26000 FH13000 FCOR26000 FHGROUP 43C545142-01-03 453CL 453CR 463CL463CR 473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.13000 FCOR88000 FH13000 FCOR88000 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 33RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N545146-01-01 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR 453AL 453AR463AL 463AR 473AL473AR 483AL 483ARDETAILED INSPECTION OF PYLON LOWER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4.20000 FCOR80000 FH6000 FCOR42900 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BN545146-01-02 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448AR 453AL 453AR463AL 463AR 473AL473AR 483AL 483ARDETAILED INSPECTION OF PYLON LOWER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 2 AND RIB 4.30000 FCOR60000 FH6000 FCOR12000 FHGROUP 43CR545166-01-01 452DR 452EL 452FR462DL 462FR 462GR472ER 472FL 472GL482DL 482ER 482FLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APRE 41371ORGROUP 43APRE 41371545166-01-02 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.13000 FCOR26000 FH6000 FCOR12000 FHGROUP 43CR545166-01-03 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.12800 FCOR86300 FH4150 FCOR28100 FHGROUP 42BORGROUP 43B545166-01-04 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.13000 FCOR88000 FH4220 FCOR28500 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 34RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R545166-01-05 452DR 452FR 452GL462DL 462FR 462GR472ER 472FL 472GL482FL 482GL 482HRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APOST 41371PRE 42283ORGROUP 43APOST 41371PRE 42283R545166-01-06 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUGS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APOST 42283ORGROUP 43APOST 42283R545168-01-01 452DR 452EL 452FR462DL 462FR 462GR472ER 472FL 472GL482DL 482ER 482FLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APRE 41371ORGROUP 43APRE 41371545168-01-02 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.13000 FCOR26000 FH6000 FCOR12000 FHGROUP 43CR545168-01-03 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.12800 FCOR86300 FH4150 FCOR28100 FHGROUP 42BORGROUP 43B545168-01-04 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.13000 FCOR88000 FH4220 FCOR28500 FHGROUP 43E© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 35RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R545168-01-05 452DR 452FR 452GL462DL 462FR 462GR472ER 472FL 472GL482FL 482GL 482HRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APOST 41371PRE 42283ORGROUP 43APOST 41371PRE 42283R545168-01-06 452KL 452KR 452MR462DL 462FR 462GR472ER 472FL 472GL482ML 482MR 482NLDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 8.11900 FCOR80300 FH4000 FCOR27300 FHGROUP 42APOST 42283ORGROUP 43APOST 42283N545174-01-01 454BL 454BR 464BL464BR 474BL 474BR484BL 484BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUG AND LINKS AT RIB 14.20000 FCOR80000 FH6000 FCOR28200 FHGROUP 42APRE 41371ORGROUP 43APRE 41371N545174-01-02 454BL 454MR 464KL464KR 474KL 474KR484NL 484NRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUG AND LINKS AT RIB 14.30000 FCOR60000 FH6000 FCOR12000 FHGROUP 43CN545174-01-04 454BL 454BR 464KL464KR 474KL 474KR484BL 484BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUG AND LINKS AT RIB 14.20000 FCOR80000 FH6000 FCOR28200 FHGROUP 42APOST 41371PRE 42283ORGROUP 43APOST 41371PRE 42283N545174-01-05 454BL 454MR 464KL464KR 474KL 474KR484NL 484NRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LUG AND LINKS AT RIB 14.20000 FCOR80000 FH6000 FCOR28200 FHGROUP 42APOST 42283ORGROUP 42BORGROUP 43APOST 42283ORGROUP 43B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 36RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 545180-02-02 ENGINE, LINKS, BOLTS,SLEEVES454NR 454QL 464JL 464JR474JL 474JR 484PL 484PRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).21300 FCOR42600 FH21300 FCOR42600 FHGROUP 43CR545180-02-03 ENGINE, LINKS, BOLTS,SLEEVES454NR 454QL 464JL 464JR474JL 474JR 484PL 484PRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).12000 FCOR81200 FH12000 FCOR81200 FHGROUP 42BORGROUP 43BR545180-02-04 ENGINE, LINKS, BOLTS,SLEEVES454FL 454FR 464FL 464FR474FL 474FR 484FL 484FRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).13300 FCOR89600 FH13300 FCOR89600 FHGROUP 42APRE 43183ORGROUP 43APRE 43183R545180-02-05 ENGINE, LINKS, BOLTS,SLEEVES454FL 454FR 464JL 464JR474JL 474JR 484FL 484FRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).13300 FCOR89600 FH13300 FCOR89600 FHGROUP 42APOST 43183PRE 42283ORGROUP 43APOST 43183PRE 42283R545180-02-06 ENGINE, LINKS, BOLTS,SLEEVES454NR 454QL 464JL 464JR474JL 474JR 484PL 484PRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).13300 FCOR89600 FH13300 FCOR89600 FHGROUP 42APOST 42283ORGROUP 43APOST 42283N545180-02-07 ENGINE, LINKS, BOLTS,SLEEVES454NR 454QL 464JL 464JR474JL 474JR 484PL 484PRSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 14 (3PLACES PER PYLON).12400 FCOR83700 FH12400 FCOR83700 FHGROUP 43E© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 37RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 551016-01-01 313AL SPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGEJUST OUTBOARD OF RIB 3, LH/RH.28300 FCOR113300 FH22500 FCOR85300 FHA340-200ORGROUP 43AORGROUP 43BORGROUP 43CR571102-01-01 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING AND AIRCONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.13300 FCOR89800 FH5450 FCOR37000 FHGROUP 42APOST 44360PRE 52094ORGROUP 42BPRE 52094ORGROUP 43BPOST 44360PRE 49202PRE 52094R571102-01-02 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING AND AIRCONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.16900 FCOR33900 FH6160 FCOR12300 FHGROUP 43CPRE 52094© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 38RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571103-01-01 191HB 192HB 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING ANDAIR CONDITIONINGDUCTSFASTENER REMOVALSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREAOF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- ROTOTEST INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-01.13100 FCOR88400 FH6350 FCOR43000 FHGROUP 42APOST 44360PRE 50745ORGROUP 42BPOST 44360PRE 50745ORGROUP 43BPOST 44360PRE 49202PRE 50745R571103-01-02 191HB 192HB 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING ANDAIR CONDITIONINGDUCTSFASTENER REMOVALSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREAOF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- ROTOTEST INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-02.13000 FCOR26000 FH7150 FCOR14300 FHGROUP 43CPRE 50745R571103-02-01 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING ANDAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREAOF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- HIGH FREQUENCY EDDY CURRENT INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-01.13100 FCOR88400 FH1350 FCOR9300 FHGROUP 42APOST 44360PRE 50745ORGROUP 42BPOST 44360PRE 50745ORGROUP 43BPOST 44360PRE 49202PRE 50745© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 39RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571103-02-02 821INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONLINING ANDAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREAOF FASTENERS BETWEEN STR 39 AND STR 40, LH/RH.NOTE :- HIGH FREQUENCY EDDY CURRENT INSPECTION.- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-02.13000 FCOR26000 FH1550 FCOR3100 FHGROUP 43CPRE 50745R571104-01-01 191FB 192GB 192JB821131CX 131DX 132CX 132DXFASTENER TO BEREMOVEDINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR 38 AND STR 39, LH/RH.13000 FCOR88100 FH5050 FCOR34200 FHGROUP 43BPRE 44360POST 52094R571104-01-02 191FB 192GB 192JB821131CX 131DX 132CX 132DXFASTENER TO BEREMOVEDINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR 38 AND STR 39, LH/RH.11100 FCOR75300 FH6400 FCOR43200 FHGROUP 43APRE 52094ORGROUP 42APRE 52094R571104-01-03 191FB 192GB 192JB821131CX 131DX 132CX 132DXFASTENER TO BEREMOVEDINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR 38 AND STR 39, LH/RH.8000 FCOR54600 FH5050 FCOR34200 FHGROUP 43BPRE 44360PRE 52094R571104-01-04 191FB 192GB 192JB821131CX 131DX 132CX 132DXFASTENER TO BEREMOVEDINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR 38 AND STR 39, LH/RH.11800 FCOR79800 FH5050 FCOR34200 FHGROUP 43BPOST 44360PRE 49202PRE 52094ORGROUP 42BPRE 52094© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 40RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571104-01-05 191FB 192 GB 192JB821131CX 131DX 132CX 132DXFASTENER TO BEREMOVEDINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR 38 AND STR 39, LH/RH.17000 FCOR34100 FH5600 FCOR11200 FHGROUP 43CPRE 52094R571107-01-01 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEENSTRINGERS 20 AND 21, LH/RH.14000 FCOR94500 FH5700 FCOR38500 FHGROUP 42AORGROUP 43AR571107-01-02 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEENSTRINGERS 20 AND 21, LH/RH.12900 FCOR87300 FH4500 FCOR30500 FHGROUP 42BORGROUP 43BR571107-01-03 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEENSTRINGERS 20 AND 21, LH/RH.18900 FCOR37800 FH4900 FCOR9850 FHGROUP 43C571107-01-04 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y = 2427 BETWEENSTRINGERS 20 AND 21, LH/RH.13600 FCOR92000 FH4620 FCOR31200 FHGROUP 43ER571108-01-01 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.12800 FCOR87000 FH5050 FCOR34100 FHGROUP 43APRE 40123R571108-01-03 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.17300 FCOR117400 FH5900 FCOR40000 FHGROUP 42BORGROUP 43BR571108-01-04 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.20600 FCOR41200 FH6700 FCOR13400 FHGROUP 43C571108-01-05 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.19200 FCOR130000 FH6500 FCOR43900 FHGROUP 43ER571114-01-01 147AZ 734 148AZ744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.13500 FCOR91500 FH8850 FCOR59800 FHGROUP 43APRE 40123© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 41RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571114-01-03 147AZ 734 148AZ744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.10800 FCOR72900 FH6300 FCOR42800 FHGROUP 42BORGROUP 43BR571114-01-04 147AZ 734 148AZ744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.12800 FCOR25600 FH7150 FCOR14300 FHGROUP 43CR571116-01-01 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 AND 22, AT Y =-567.5.14000 FCOR94500 FH5700 FCOR38500 FHGROUP 42AORGROUP 43AR571116-01-02 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 AND 22, AT Y =-567.5.12900 FCOR87300 FH4500 FCOR30500 FHGROUP 42BORGROUP 43BR571116-01-03 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 AND 22, AT Y =-567.5.18900 FCOR37800 FH4900 FCOR9850 FHGROUP 43C571116-01-04 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 AND 22, AT Y =-567.5.13600 FCOR92000 FH4620 FCOR31200 FHGROUP 43ER571118-01-01 FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF THE CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180BETWEEN STR 27 AND STR 28.14000 FCOR94500 FH5700 FCOR38500 FHGROUP 42AORGROUP 43AD571118-01-02TASK DELETED IN ALI ISSUE 11R571118-01-03 FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF THE CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180BETWEEN STR 27 AND STR 28.12900 FCOR87300 FH4500 FCOR30500 FHGROUP 42BORGROUP 43BD571118-01-04TASK DELETED IN ALI ISSUE 11R571118-01-05 FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF THE CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180BETWEEN STR 27 AND STR 28.18900 FCOR37800 FH4900 FCOR9850 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 42RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340D571118-01-06TASK DELETED IN ALI ISSUE 11571118-01-07 192QB 195CB SPECIAL DETAILED INSPECTION OF THE CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTOR AREA AT Y =-2230 BETWEEN STR 25 AND STR 26 AND AT Y = 180BETWEEN STR 27 AND STR 28.13600 FCOR92000 FH4620 FCOR31200 FHGROUP 43ER571122-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXEXTERNAL STRUCTURE, FASTENER AREA AT REAR SPARLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION,FROM Y = 953 TO Y = 1959, LH/RH.13800 FCOR93400 FH4250 FCOR28800 FHGROUP 42BORGROUP 43BR571122-01-03 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXEXTERNAL STRUCTURE, FASTENER AREA AT REAR SPARLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION,FROM Y = 953 TO Y = 1959, LH/RH.20100 FCOR40300 FH4650 FCOR9350 FHGROUP 43C571122-01-04 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXEXTERNAL STRUCTURE, FASTENER AREA AT REAR SPARLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION,FROM Y = 953 TO Y = 1959, LH/RH.14600 FCOR99000 FH4360 FCOR29400 FHGROUP 43ER571123-01-01 251AG 251FG 252AG252FGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERALFRAME FROM FR 40.3 TO FR 45, LH/RH.8800 FCOR60000 FH4100 FCOR28100 FHGROUP 42APRE 49404ORGROUP 43APRE 49404R571123-01-02 251AG 251FG 252AG252FGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERALFRAME FROM FR 40.3 TO FR 45, LH/RH.8600 FCOR58200 FH4300 FCOR29000 FHGROUP 42BPRE 49404ORGROUP 43BPRE 49404© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 43RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571123-01-03 251AG 251FG 252AG252FGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERALFRAME FROM FR 40.3 TO FR 45, LH/RH.17000 FCOR34100 FH8100 FCOR16300 FHGROUP 43CPRE 49404N571123-01-04 251AG 251FG 252AG252FGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERALFRAME FROM FR 40.3 TO FR 45, LH/RH.19600 FCOR132700 FH9400 FCOR64000 FHGROUP 42APOST 49404ORGROUP 43APOST 49404N571123-01-05 251AG 251FG 252AG252FGINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEINSPECTIONSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERALFRAME FROM FR 40.3 TO FR 45, LH/RH.18200 FCOR123400 FH9200 FCOR62600 FHGROUP 42BPOST 49404ORGROUP 43BPOST 49404ORGROUP 43ER571125-01-01 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR AFT FACE, FASTENERS AREA BETWEENY=2219 AND FR 47 LOWER CORNER FITTING, LH/RH.14200 FCOR96000 FH3850 FCOR26000 FHGROUP 42BORGROUP 43BR571125-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR AFT FACE, FASTENERS AREA BETWEENY=2219 AND FR 47 LOWER CORNER FITTING, LH/RH.20700 FCOR41500 FH4200 FCOR8400 FHGROUP 43CR571126-01-01 734 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR WEB AT APU FUEL PUMP APERTURE IN THELEFT SIDE LOWER CORNER.11800 FCOR80000 FH9600 FCOR65000 FHGROUP 42BORGROUP 43BR571126-01-02 734 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR WEB AT APU FUEL PUMP APERTURE IN THELEFT SIDE LOWER CORNER.14800 FCOR29700 FH10900 FCOR21800 FHGROUP 43CR571133-01-02 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX, STRUTLUGS ON LONGITUDINAL STIFFENERS AND ROD FITTINGCONNECTIONS (63 PLACES).14400 FCOR97700 FH4700 FCOR31900 FHGROUP 42BORGROUP 43B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 44RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571133-01-03 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX, STRUTLUGS ON LONGITUDINAL STIFFENERS AND ROD FITTINGCONNECTIONS (63 PLACES).21100 FCOR42300 FH5450 FCOR10900 FHGROUP 43C571133-01-04 147AZ 734 148AZ744DETAILED INSPECTION OF CENTER WING BOX, STRUTLUGS ON LONGITUDINAL STIFFENERS AND ROD FITTINGCONNECTIONS (63 PLACES).15300 FCOR103000 FH6600 FCOR44800 FHGROUP 43E571145-01-01 734 744 147AZ 148AZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF CWB, INTERNALSTRUCTURE, RIB1 LOWER TEE FITTING INBOARD FLANGE;FASTENERS IN RADIUS AREA AT STR16, STR20, STR21 ANDSTR25 TO STR29, LH/RH.18700 FCOR126000 FH5230 FCOR35300 FHGROUP 43ER571146-02-01 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROWON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16,STR20, STR21 AND STR25 TO STR29, LH/RH.17400 FCOR117900 FH9500 FCOR64100 FHGROUP 42AORGROUP 43AR571146-02-02 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROWON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16,STR20, STR21 AND STR25 TO STR29, LH/RH.11500 FCOR77800 FH6850 FCOR46200 FHGROUP 42BORGROUP 43BR571146-02-03 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROWON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16,STR20, STR21 AND STR25 TO STR29, LH/RH.13600 FCOR27300 FH7750 FCOR15500 FHGROUP 43C571146-02-04 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROWON EACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16,STR20, STR21 AND STR25 TO STR29, LH/RH.11800 FCOR80000 FH7100 FCOR47600 FHGROUP 43E© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 45RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R571149-01-02 191HB 192HB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGEFROM FR 40 DATUM TO STR 1 LEVEL, LH/RH.12900 FCOR87400 FH5900 FCOR39800 FHGROUP 42APOST 44360PRE 45968ORGROUP 42BPOST 44360PRE 45968ORGROUP 43BPOST 44360PRE 45968R571149-01-03 191HB 192HB SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, KEEL BEAM FITTING OUTBOARD EDGEFROM FR 40 DATUM TO STR 1 LEVEL, LH/RH.16900 FCOR33800 FH7200 FCOR14400 FHGROUP 43CPRE 45968R571152-01-01 147AZ 148AZ734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, CENTER SPAR FITTING FLANGE,RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGEAT FASTENERS 3 TO 12, LH/RH.15200 FCOR103200 FH5900 FCOR40000 FHGROUP 42APRE 41652ORGROUP 43APRE 41652N571153-01-01 147AZ 148AZ734 744SEALANT REMOVALSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.8900 FCOR60500 FH6000 FCOR40700 FHGROUP 42APOST 43577ORGROUP 43APOST 43577ORPOST 44440S13324© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 46RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N571153-01-02 147AZ 148AZ734 744SEALANT REMOVALSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.13600 FCOR92800 FH6000 FCOR40700 FHGROUP 42APOST 44360ORPOST 44440S13276ORPOST 44440S13090ORGROUP 43APOST 44440S13276N571153-01-03 147AZ 148AZ734 744SEALANT REMOVALSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.11900 FCOR80800 FH6000 FCOR40700 FHGROUP 42BORGROUP 43BN571153-01-04 147AZ 148AZ734 744SEALANT REMOVALSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.16000 FCOR32000 FH6000 FCOR12000 FHGROUP 43CR571153-01-05 147AZ 148AZ734 744SEALANT REMOVALSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.17100 FCOR116000 FH12100 FCOR82000 FHGROUP 43EN571162-01-01 191HB 192HB SPECIAL DETAILED INSPECTION OF KEEL BEAM FITTING,TWO FASTENERS HOLES AT STIFFENER 1 LEVEL, LH/RH.13600 FCOR92200 FH5700 FCOR38500 FHGROUP 42APOST 43577POST 54459ORGROUP 43APOST 43577POST 54459© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 47RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N571163-01-01 191HB 192HB SPECIAL DETAILED INSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.11000 FCOR74700 FH4150 FCOR28000 FHGROUP 42APOST 41652PRE 44360POST 56467ORGROUP 43APOST 41652POST 56467ORGROUP 43BPRE 44360POST 56467R571165-01-01 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR, FILLET RADIUS FROM Y=1959 TO Y=2219 ANDFROM Z=-1859.6 TO Z=-2073, LH/RH.11200 FCOR75600 FH8700 FCOR58800 FHGROUP 42APRE 43865ORGROUP 43APRE 43865R571165-01-02 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOXREAR SPAR, FILLET RADIUS FROM Y=1959 TO Y=2219 ANDFROM Z=-1859.6 TO Z=-2073, LH/RH.10100 FCOR68200 FH7350 FCOR49700 FHGROUP 43BPRE 43865N572004-01-02 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVEREDBY MAIN LANDING GEAR REINFORCING PLATE, FLAPTRACK 2 FAIRING AND PYLON FAIRING.13500 FCOR77300 FH3600 FCOR20500 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437R572004-01-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVEREDBY MAIN LANDING GEAR REINFORCING PLATE, FLAPTRACK 2 FAIRING AND PYLON FAIRING.21700 FCOR43500 FH5700 FCOR11500 FHGROUP 43CD572004-01-05TASK DELETED IN ALI ISSUE 11N572006-02-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWERSURFACE MAIN LANDING GEAR REINFORCING PLATE.24500 FCOR49000 FH5400 FCOR10800 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 48RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572006-02-07 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWERSURFACE MAIN LANDING GEAR REINFORCING PLATE.15200 FCOR86900 FH2800 FCOR16300 FHGROUP 42AORGROUP 43AN572006-02-08 N/A GENERAL VISUAL INSPECTION OF OUTER WING LOWERSURFACE MAIN LANDING GEAR REINFORCING PLATE.14400 FCOR82600 FH3100 FCOR18000 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437N572007-01-02 464GL 464GR 531AB474GL 474GR 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR INAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARDPYLON FAIRING.13500 FCOR77300 FH6700 FCOR38500 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437R572007-01-03 464GL 464GR 531AB474GL 474GR 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR INAREA COVERED BY FLAP TRACK 2 FAIRING AND INBOARDPYLON FAIRING.21700 FCOR43500 FH10800 FCOR21700 FHGROUP 43CN572010-02-01 541AB 541BB 541CB 541DB541EB 541FB 641AB 641BB641CB 641DB 641EB 641FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUTOUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10AND 11-12.15000 FCOR85900 FH3900 FCOR22600FHGROUP 42AORGROUP 43AN572012-01-01 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY PYLON FAIRINGAND PYLON REINFORCING PLATE.18100 FCOR103300 FH3400 FCOR19400 FHGROUP 42AORGROUP 43AN572012-01-04 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TO REARSPAR EXCLUDING AREAS COVERED BY PYLON FAIRINGAND PYLON REINFORCING PLATE.18700 FCOR107100 FH3300 FCOR19300 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 49RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572013-01-01 464AL 464AR 464BL 464BR464FL 464FR 464GL 464GR464HL 474AL 474AR 474BL474BR 474FL 474FR 474GL474GR 474HLDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY INBOARD PYLONFAIRING, EXCLUDING AREA COVERED BY PYLONREINFORCING PLATE AND AFT ATTACHMENT FITTING SKINREINFORCING PLATE.15300 FCOR87100 FH3400 FCOR19400 FHGROUP 42APRE 43183ORGROUP 43APRE 43183N572013-01-03 464AL 464GL 464GR 464HL464JL 464JR 464KL 464KR464M 474AL 474GL 474GR474HL 474JL 474JR 474KL474KR 474MRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY INBOARD PYLONFAIRING, EXCLUDING AREA COVERED BY PYLONREINFORCING PLATE AND AFT ATTACHMENT FITTING SKINREINFORCING PLATE.15300 FCOR87100 FH3400 FCOR19400 FHGROUP 42APOST 43183ORGROUP 43APOST 43183N572013-01-05 464AL 464GL 464GR 464HL464JL 464JR 464KL 464KR464M 474AL 474GL 474GR474HL 474JL 474JR 474KL474KR 474MRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY INBOARD PYLONFAIRING, EXCLUDING AREA COVERED BY PYLONREINFORCING PLATE AND AFT ATTACHMENT FITTING SKINREINFORCING PLATE.18600 FCOR106200 FH3300 FCOR19300 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437N572014-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINTS AT STR 13 ANDSTR 20 BETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY FAIRINGS.15500 FCOR88400 FH6000 FCOR34300 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572015-02-05 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFTOF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEENRIB 1 AND RIB 12.16800 FCOR95700 FH6100 FCOR34800 FHGROUP 42APOST 45416ORGROUP 43APOST 45416R572016-02-01 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.13900 FCOR79500 FH2800 FCOR16100 FHGROUP 42AORGROUP 43AN572016-02-02 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.18000 FCOR102900 FH2900 FCOR16800 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 50RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572016-02-03 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.29300 FCOR58600 FH4800 FCOR9600 FHGROUP 43CN572016-02-05 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.18600 FCOR105100 FH5600 FCOR31700 FHGROUP 43BPOST 48437R572017-01-05 541AB 641AB DETAILED INSPECTION OF OUTER WING BOTTOM SKINROOT JOINT FITTINGS ON STR 13 AND STR 20.10300 FCOR59200 FH5800 FCOR33100 FHGROUP 42APRE 43283ORGROUP 43APRE 43283R572018-01-01 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 ANDSTR 20 BETWEEN RIB 5 AND RIB 7.11600 FCOR66500 FH4900 FCOR27900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572018-01-02 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 ANDSTR 20 BETWEEN RIB 5 AND RIB 7.18100 FCOR103500 FH4900 FCOR27900 FHGROUP 42APOST 40610ORGROUP 43APOST 40610N572018-01-03 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 1 AND RIB 9, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20 ANDSTR 20 BETWEEN RIB 5 AND RIB 7.18800 FCOR107500 FH5100 FCOR29400 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 51RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572019-01-01 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.11600 FCOR66500 FH4900 FCOR27900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572019-01-02 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.18100 FCOR103500 FH4900 FCOR27900 FHGROUP 42APOST 40610ORGROUP 43APOST 40610N572019-01-03 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.18800 FCOR107500 FH5100 FCOR29400 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437N572019-01-06 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER BETWEEN RIB 9 AND RIB 12, EXCLUDING STR 15AND STR 18 AND BUTTSTRAPS AT STR 13 AND STR 20.18500 FCOR104700 FH10000 FCOR56400 FHGROUP 43BPOST 48437N572021-01-01 474FL 474FR 474GL 474GR464FL 464FR 464GL 464GR531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINT AT STR 13 ANDSTR 20 IN AREAS COVERED BY INBOARD PYLON FAIRINGAND FLAP TRACK 2 FAIRING.15500 FCOR88400 FH7900 FCOR45000 FHGROUP 42APRE 40610PRE 43183ORGROUP 43APRE 40610PRE 43183N572021-01-04 464GL 464GR 464JL 464JR474GL 474GR 474JL 474JR531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINT AT STR 13 ANDSTR 20 IN AREAS COVERED BY INBOARD PYLON FAIRINGAND FLAP TRACK 2 FAIRING.15500 FCOR88400 FH7900 FCOR45000 FHGROUP 42APRE 40610POST 43183ORGROUP 43APRE 40610POST 43183© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 52RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572022-01-01 541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE HOT FUEL RECIRCULATION HOLE INRIB BAY 10-11, FROM STR 6 TO STR 7.16800 FCOR95700 FH5100 FCOR29600 FHGROUP 42AORGROUP 43AN572023-02-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAINLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2FAIRING.18100 FCOR103300 FH3400 FCOR19400 FHGROUP 42AORGROUP 43AN572023-02-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENT BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAINLANDING GEAR REINFORCING PLATE AND FLAP TRACK 2FAIRING.18700 FCOR107100 FH3300 FCOR19300 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437R572027-01-01 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 20BETWEEN RIB 1 AND RIB 9.11600 FCOR66400 FH8900 FCOR50900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610R572029-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB1 AND RIB 12.16600 FCOR86200 FH3800 FCOR20100 FHGROUP 42AORGROUP 43A572029-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB1 AND RIB 12.23500 FCOR47000 FH5300 FCOR10600 FHGROUP 43CN572029-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB1 AND RIB 12.16200 FCOR84300 FH3800 FCOR20100 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 53RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572030-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 9AND RIB 11.5600 FCOR29300 FH3800 FCOR20100 FHGROUP 42APRE 41300ORGROUP 43APRE 41300R572030-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB9 AND RIB 11.8400 FCOR43500 FH3800 FCOR20100 FHGROUP 42APOST 41300ORGROUP 43APOST 41300ORGROUP 42BORGROUP 43BPRE 48437R572030-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 9AND RIB 11.11800 FCOR23700 FH5200 FCOR10400 FHGROUP 43CR572032-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.9700 FCOR50200 FH4000 FCOR21000 FHGROUP 42APOST 46110ORGROUP 43APOST 46110R572032-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.9200 FCOR47900 FH3000 FCOR15900 FHGROUP 42BPOST 46110PRE 48437ORGROUP 43BPOST 46110PRE 48437R572032-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.13000 FCOR26000 FH6200 FCOR12500 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 54RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572032-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.15700 FCOR72300 FH8900 FCOR41000 FHGROUP 43EN572032-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.16000 FCOR76600 FH9100 FCOR43500 FHGROUP 43BPOST 46110POST 48437R572033-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPARTO REAR SPAR.17900 FCOR93100 FH3900 FCOR20700 FHGROUP 42AORGROUP 43AN572033-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPARTO REAR SPAR.19900 FCOR103000 FH4300 FCOR22400 FHGROUP 42BPRE 48437ORGROUP 43BPRE 48437572033-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPARTO REAR SPAR.28200 FCOR56400 FH6100 FCOR12200 FHGROUP 43CR572034-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEENRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS11 AND 13.9800 FCOR51100 FH6400 FCOR33400 FHGROUP 42AORGROUP 43AR572034-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEENRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS11 AND 13.13300 FCOR69300 FH12600 FCOR65500 FHGROUP 42BORGROUP 43BPRE 48437572034-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEENRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS11 AND 13.17800 FCOR35600 FH13000 FCOR26000 FHGROUP 43C© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 55RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572034-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEENRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS11 AND 13.15400 FCOR71100 FH15400 FCOR70800 FHGROUP 43EN572034-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGER 12 AND 19 BETWEENRIB 1 AND RIB 18 EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 and 8 AND STRINGER 19 BETWEEN RIBS11 AND 13.15700 FCOR75300 FH15600 FCOR74900 FHGROUP 43BPOST 48437R572035-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TORIB 8.9000 FCOR46800 FH5400 FCOR28300 FHGROUP 42AORGROUP 43AR572035-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TORIB 8.10000 FCOR52100 FH10000 FCOR52100 FHGROUP 42BORGROUP 43BPRE 48437572035-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE FROM STRINGERS 12 TO 19 AND FROM RIB 4 TORIB 8.13000 FCOR26000 FH13000 FCOR26000 FHGROUP 43CR572036-01-01 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONTTO REAR SPARS.16100 FCOR83500 FH4100 FCOR21600 FHGROUP 42AORGROUP 43AR572036-01-02 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONTTO REAR SPARS.15400 FCOR79800 FH3400 FCOR17900 FHGROUP 42BORGROUP 43BPRE 48437572036-01-03 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGER CROWN FITTINGS AT ROOT JOINT FROM FRONTTO REAR SPARS.21400 FCOR42800 FH6200 FCOR12400 FHGROUP 43CR572039-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TORIB 9 AND FROM RIB 11 TO RIB 12.16100 FCOR83500 FH3800 FCOR20100 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 56RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572039-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TORIB 9 AND FROM RIB 11 TO RIB 12.16800 FCOR87300 FH3800 FCOR20100 FHGROUP 42BORGROUP 43BPRE 48437572039-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TORIB 9 AND FROM RIB 11 TO RIB 12.23100 FCOR46200 FH5200 FCOR10400 FHGROUP 43CR572040-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 ANDRIB 13.13000 FCOR67600 FH6300 FCOR32800 FHGROUP 42AORGROUP 43AR572040-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 ANDRIB 13.14500 FCOR75100 FH12400 FCOR64400 FHGROUP 42BORGROUP 43BPRE 48437572040-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STINGER 19 BETWEEN RIB 11 ANDRIB 13.19400 FCOR38800 FH13000 FCOR26000 FHGROUP 43CR572046-01-01 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDINGTOP AND BOTTOM FLANGES.5800 FCOR33200 FH5800 FCOR33200 FHGROUP 42APOST 46111ORGROUP 43APOST 46111R572046-01-02 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDINGTOP AND BOTTOM FLANGES.8500 FCOR48900 FH6200 FCOR35600 FHGROUP 42BORGROUP 43BPRE 48437572046-01-03 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDINGTOP AND BOTTOM FLANGES.12500 FCOR25000 FH9100 FCOR18200 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 57RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572046-01-04 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDINGTOP AND BOTTOM FLANGES.13800 FCOR62200 FH8700 FCOR39500 FHGROUP 43EN572046-01-05 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDINGTOP AND BOTTOM FLANGES.13000 FCOR70300 FH8200 FCOR44700 FHGROUP 43BPOST 48437N572047-01-01 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6,FORWARD PINTLE FITTING, RETRACTION JACK FITTINGAND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1AND RIB 7.19100 FCOR108700 FH13000 FCOR60000 FHGROUP 42AORGROUP 43A572047-01-02 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6,FORWARD PINTLE FITTING, RETRACTION JACK FITTINGAND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1AND RIB 7.27200 FCOR54400 FH13000 FCOR26000 FHGROUP 43C572047-01-03 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6,FORWARD PINTLE FITTING, RETRACTION JACK FITTINGAND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1AND RIB 7.19100 FCOR86100 FH19100 FCOR86100 FHGROUP 43EN572047-01-04 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6,FORWARD PINTLE FITTING, RETRACTION JACK FITTINGAND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1AND RIB 7.17500 FCOR99800 FH13000 FCOR60000 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 58RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572047-01-05 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6,FORWARD PINTLE FITTING, RETRACTION JACK FITTINGAND SIDESTAY FITTING) BOLTING AREAS BETWEEN RIB 1AND RIB 7.18000 FCOR97100 FH13000 FCOR60000 FHGROUP 43BPOST 48437R572050-01-01 573DB 673DBFLAPS EXTENDEDDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.10500 FCOR60100 FH10500 FCOR60100 FHGROUP 42AORGROUP 43AR572050-01-02 573DB 673DBFLAPS EXTENDEDDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.12100 FCOR69300 FH10600 FCOR60500 FHGROUP 42BORGROUP 43BPRE 48437R572050-01-03 573DB 673DBFLAPS EXTENDEDDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.15400 FCOR30900 FH13000 FCOR26000 FHGROUP 43CR572051-01-02 FLAPS EXTENDEDSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.12100 FCOR68900 FH3800 FCOR21900 FHGROUP 42APOST 42547ORGROUP 43APOST 42547R572051-01-03 FLAPS EXTENDEDSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.12500 FCOR71500 FH12500 FCOR60000 FHGROUP 42BORGROUP 43BPRE 48437572051-01-04 FLAPS EXTENDEDSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 AND 2.18800 FCOR37600 FH13000 FCOR26000 FHGROUP 43CR572052-01-01 541AB 541BB 541BZ541CZ 641AB 641BB641BZ 641CZSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7INCLUDING TOP AND BOTTOM FLANGES.9100 FCOR52200 FH4600 FCOR26500 FHGROUP 42APOST 46110ORGROUP 43APOST 46110© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 59RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572052-01-02 541AB 541BB 541BZ541CZ 641AB 641BB641BZ 641CZSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7INCLUDING TOP AND BOTTOM FLANGES.8700 FCOR49700 FH4400 FCOR25400 FHGROUP 42BPOST 46110ORGROUP 43BPOST 46110PRE 48437572052-01-03 541AB 541BB 541BZ541CZ 641AB 641BB641BZ 641CZSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7INCLUDING TOP AND BOTTOM FLANGES.13000 FCOR26000 FH5700 FCOR11400 FHGROUP 43C572052-01-04 541AB 541BB 541BZ541CZ 641AB 641BB641BZ 641CZSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7INCLUDING TOP AND BOTTOM FLANGES.16500 FCOR74700 FH5200 FCOR23500 FHGROUP 43EN572052-01-05 541AB 541BB 541BZ541CZ 641AB 641BB641BZ 641CZSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7INCLUDING TOP AND BOTTOM FLANGES.15600 FCOR84300 FH4900 FCOR26500 FHGROUP 43BPOST 46110POST 48437R572054-01-05 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.17100 FCOR77100 FH5600 FCOR25400 FHGROUP 43ER572054-01-06 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.11300 FCOR64700 FH3300 FCOR19100 FHGROUP 42APRE 43692PRE 46141ORGROUP 43APRE 43692PRE 46141R572054-01-07 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.13500 FCOR77000 FH2400 FCOR14100 FHGROUP 42BPRE 43692PRE 46141ORGROUP 43BPRE 43692PRE 48437PRE 46141© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 60RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572054-01-08 FLAPS DEPLOYED SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 AND 5.16100 FCOR87000 FH5300 FCOR28700 FHGROUP 43BPOST 43692POST 48437R572063-01-01 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS INREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTINGINBOARD OF RIB 12.10400 FCOR59700 FH5100 FCOR29500 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572063-01-02 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS INREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTINGINBOARD OF RIB 12.17700 FCOR101100 FH5100 FCOR29500 FHGROUP 42APOST 40610ORGROUP 43APOST 40610572063-01-05 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS INREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTINGINBOARD OF RIB 12.14500 FCOR65500 FH14500 FCOR65500 FHGROUP 43EN572063-01-06 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10AND RIB 12 INCLUDING TOP AND BOTTOM FLANGES,BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS INREGION OF RIB BAY 10-10A AND SPAR JOINT BOLTINGINBOARD OF RIB 12.13700 FCOR74100 FH13000 FCOR60000 FHGROUP 43BPOST 48437R572064-01-01 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10.10400 FCOR59700 FH5100 FCOR29500 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572064-01-02 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10.17900 FCOR102200 FH5100 FCOR29500 FHGROUP 42APOST 40610ORGROUP 43APOST 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 61RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572065-01-01 522DB 522EB 622DB622EBDETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 12.13500 FCOR76800 FH5000 FCOR28800 FHGROUP 42AORGROUP 43AR572065-01-02 522DB 522EB 622DB622EBDETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 12.12100 FCOR68900 FH4800 FCOR27400 FHGROUP 42BORGROUP 43BPRE 48437572065-01-03 522DB 522EB 622DB622EBDETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 12.22400 FCOR44800 FH9900 FCOR19800 FHGROUP 43CD572068-01-01 TASK DELETED IN ALI ISSUE 11572068-01-04 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7 FORWARDAND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTSINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OFSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.19600 FCOR88600 FH5200 FCOR23600 FHGROUP 43EN572068-01-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7 FORWARDAND AFT OF THE CENTER SPAR AT SKIN ATTACHMENTSINCLUDING CLEATS, SPAR ATTACHMENTS, REGION OFSTRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.18500 FCOR100200 FH4900 FCOR26700 FHGROUP 43BPOST 48437R572073-01-01 541FB 541GB 641FB641GBDETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT,RIB 11 FORWARD AND AFT, AND RIB 12 AT SKINATTACHMENTS (INCLUDING CLEATS), SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.12200 FCOR69100 FH10600 FCOR59700 FHGROUP 42AORGROUP 43AN572073-01-02 541FB 541GB 641FB641GBDETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT,RIB 11 FORWARD AND AFT, AND RIB 12 AT SKINATTACHMENTS (INCLUDING CLEATS), SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.14100 FCOR79400 FH9000 FCOR50900 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 62RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572073-01-03 541FB 541GB 641FB641GBDETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT,RIB 11 FORWARD AND AFT, AND RIB 12 AT SKINATTACHMENTS (INCLUDING CLEATS), SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.24900 FCOR49800 FH13000 FCOR26000 FHGROUP 43CR572081-01-01 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.10600 FCOR60300 FH5500 FCOR31400 FHGROUP 42APOST 43021MSN 114 ANDSUBSORGROUP 43APOST 43021MSN 114 ANDSUBSR572081-01-02 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.NOTE: TASK APPLICABLE IF MOD 43021 CARRIED OUT BYRETROFIT SOLUTION13900 FCOR79300 FH5500 FCOR31400 FHGROUP 42APOST 43021UP TO MSN 104NOTEORGROUP 43APOST 43021UP TO MSN 104NOTER572081-01-03 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.13100 FCOR75000 FH3500 FCOR20200 FHGROUP 42BORGROUP 43BPRE 48437572081-01-04 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.20700 FCOR41400 FH5500 FCOR11000 FHGROUP 43CR572082-01-01 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.11800 FCOR67700 FH6200 FCOR35600 FHGROUP 42APRE 40610ORGROUP 43APRE 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 63RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572082-01-02 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.14400 FCOR82400 FH6200 FCOR35600 FHGROUP 42APOST 40610ORGROUP 43APOST 40610R572082-01-03 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.12500 FCOR71700 FH7900 FCOR45100 FHGROUP 42BORGROUP 43BPRE 48437572082-01-04 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.22100 FCOR44200 FH16300 FCOR32600 FHGROUP 43C572082-01-05 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.18000 FCOR81300 FH15700 FCOR70800 FHGROUP 43EN572082-01-06 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLESAND CONDUIT HOLES.17000 FCOR91900 FH14800 FCOR80000 FHGROUP 43BPOST 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 64RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572084-01-05 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR11, STR14, STR18 TOSTR20 AND AT STR23 TO STR28, LH/RH.16000 FCOR108000 FH7000 FCOR47400 FHGROUP 43ER572093-01-01 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-02-019600 FCOR54900 FH6900 FCOR39700 FHGROUP 42APRE 40610POST 45415ORGROUP 43APRE 40610POST 45415R572093-02-01 541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-01-019600 FCOR54900 FH6900 FCOR39700 FHGROUP 42APRE 40610POST 45415ORGROUP 43APRE 40610POST 45415R572094-01-01 541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 20BETWEEN RIB 9 AND RIB 12.11600 FCOR66400 FH8900 FCOR50900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610R572095-01-01 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.11600 FCOR66500 FH4900 FCOR27900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572095-01-02 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.18100 FCOR103500 FH4900 FCOR27900 FHGROUP 42APOST 40610ORGROUP 43APOST 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 65RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572095-01-03 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.18800 FCOR107500 FH5100 FCOR29400 FHGROUP 42BORGROUP 43BPRE 48437N572102-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE IN REGION OF RIB 27 SKIN JOINTAREA.17500 FCOR99900 FH3900 FCOR22500FHGROUP 42AORGROUP 43AN572109-02-01 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER SURFACES AROUND ACCESSDOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYSBETWEEN RIBS 27 AND 39.17500 FCOR99700 FH7700 FCOR44100 FHGROUP 42AORGROUP 43AN572109-02-02 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER SURFACES AROUND ACCESSDOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYSBETWEEN RIBS 27 AND 39.16800 FCOR96000 FH5500 FCOR31800 FHGROUP 42BORGROUP 43BPRE 48437572109-02-03 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER SURFACES AROUND ACCESSDOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYSBETWEEN RIBS 27 AND 39.28500 FCOR57000 FH9400 FCOR18800 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 66RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572110-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY FLAP TRACK FAIRINGS 3, 4 AND 5.15300 FCOR87400 FH7200 FCOR41400 FHGROUP 42AORGROUP 43AN572110-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY FLAP TRACK FAIRINGS 3, 4 AND 5.15500 FCOR88400 FH6500 FCOR37200 FHGROUP 42BORGROUP 43BPRE 48437572110-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY FLAP TRACK FAIRINGS 3, 4 AND 5.24700 FCOR49400 FH10400 FCOR20800 FHGROUP 43CN572111-01-01 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3, 4 AND 5.15300 FCOR87400 FH7200 FCOR41400 FHGROUP 42AORGROUP 43AN572111-01-02 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3, 4 AND 5.15500 FCOR88400 FH6500 FCOR37200 FHGROUP 42BORGROUP 43BPRE 48437572111-01-03 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3, 4 AND 5.24700 FCOR49400 FH10400 FCOR20800 FHGROUP 43CN572116-01-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE SPANWISE SKIN JOINTS ATSTRINGER 13 AND STRINGER 20 BETWEEN RIB 12 AND RIB27, AS FAR AS VISIBLE.15500 FCOR88400 FH5500 FCOR31400 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572117-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4AND 5.15500 FCOR88400 FH6700 FCOR38500 FHGROUP 42APRE 40610ORGROUP 43APRE 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 67RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572121-01-01 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.13800 FCOR78800 FH3300 FCOR18800 FHGROUP 42AORGROUP 43AN572121-01-02 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.15300 FHOR87300 FC3300 FCOR19200 FHGROUP 42BORGROUP 43BPRE 48437R 572121-01-03 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.24500 FCOR49000 FH5400 FCOR10800 FHGROUP 43CR572122-01-01 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642FB642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIBBAYS 26 TO 28 AND STRINGERS 15 AND 18.13800 FCOR78800 FH5600 FCOR32300 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 68RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572122-01-02 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642FB642GB 642HB 642JB650AB 650BB 650CB650DB 650EB 650FB660CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIBBAYS 26 TO 28 AND STRINGERS 15 AND 18.15300 FCOR87300 FH5900 FCOR33700 FHGROUP 42BORGROUP 43BPRE 48437572122-01-03 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIBBAYS 26 TO 28 AND STRINGERS 15 AND 18.24500 FCOR49000 FH9400 FCOR18800 FHGROUP 43CN572125-01-02 542DB 542EB 642DB 642EBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-0118000 FCOR102800 FH8400 FCOR48000 FHGROUP 42AORGROUP 43AN572125-01-03 542DB 542EB 642DB 642EBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-0219000 FCOR108400 FH8000 FCOR45700 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 69RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572125-02-01 542DB 542EB 642DB 642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-0218000 FCOR102800 FH8400 FCOR48000 FHGROUP 42AORGROUP 43AN572125-02-02 542DB 542EB 642DB 642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-0319000 FCOR108400 FH8000 FCOR45700 FHGROUP 42BORGROUP 43BPRE 48437N572126-02-01 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER SURFACE AT CHORDWISE JOINT AT RIB 27.17500 FCOR99900 FH4300 FCOR24600 FHGROUP 42AORGROUP 43AN572129-01-01 541SB 641SBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-02-0115300 FCOR87400 FH4100 FCOR23800 FHGROUP 42AORGROUP 43AN572129-01-02 541SB 641SBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-02-0215300 FCOR87300 FH4000 FCOR23000 FHGROUP 42BPRE 44245ORGROUP 43BPRE 44245PRE 48437N572129-02-01 541SB 641SBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-01-0115300 FCOR87400 FH4100 FCOR23800 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 70RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572129-02-02 541SB 641SBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-01-0215300 FCOR87300 FH4000 FCOR23000 FHGROUP 42BPRE 44245ORGROUP 43BPRE 44245PRE 48437N572130-01-01 542AB 560CB 642AB 660CBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572130-02-0115300 FCOR87400 FH5600 FCOR32300 FHGROUP 42AORGROUP 43AN572130-01-02 542AB 560CB 642AB 660CBSEALANT REMOVAL ASPER NTMDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572130-02-0215300 FCOR87300 FH5900 FCOR33700 FHGROUP 42BPRE 44245ORGROUP 43BPRE 44245PRE 48437N572130-02-01 542AB 560CB 642AB 660CBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572130-01-0115300 FCOR87400 FH5600 FCOR32300 FHGROUP 42AORGROUP 43AN572130-02-02 542AB 560CB 642AB 660CBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572130-01-0215300 FCOR87300 FH5900 FCOR33700 FHGROUP 42BPRE 44245ORGROUP 43BPRE 44245PRE 48437R572131-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REARSPAR BETWEEN RIB 12 AND RIB 27.13000 FCOR60000 FH3800 FCOR20100 FHGROUP 42AORGROUP 43AR572131-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REARSPAR BETWEEN RIB 12 AND RIB 27.15900 FCOR82400 FH3800 FCOR20100 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 71RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572131-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REARSPAR BETWEEN RIB 12 AND RIB 27.21300 FCOR42600 FH5300 FCOR10600 FHGROUP 43CR572133-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.16700 FCOR86700 FH3900 FCOR20400 FHGROUP 42AORGROUP 43AR572133-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.18000 FCOR93500 FH3800 FCOR20100 FHGROUP 42BORGROUP 43BPRE 48437572133-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.24600 FCOR49200 FH5300 FCOR10600 FHGROUP 43CR572135-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE SPANWISE SKIN JOINT AT STRINGER 12BETWEEN RIB 18 AND RIB 27 AND SPANWISE SKIN JOINTAT STRINGER 19 BETWEEN RIB 18 AND RIB 24.18100 FCOR93900 FH5800 FCOR30500 FHGROUP 42AORGROUP 43AR572138-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA.15200 FCOR79000 FH8800 FCOR45700 FHGROUP 42AORGROUP 43A572138-01-03 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 27 CHORDWISE SKIN JOINT AREA.29900 FCOR59800 FH13000 FCOR26000 FHGROUP 43CR572139-01-01 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.15200 FCOR79000 FH9700 FCOR50600 FHGROUP 42AORGROUP 43A572139-01-03 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.29900 FCOR59800 FH13000 FCOR26000 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 72RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572140-01-01 541EB 541FB 541GB541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDINGBUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGERJOINTS.18400 FCOR95400 FH10300 FCOR53600 FHGROUP 42AORGROUP 43A572140-01-03 541EB 541FB 541GB541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDINGBUTTSTRAPS AT STR 12 AND STR 19 AND ALL STRINGERJOINTS.29100 FCOR58200 FH8200 FCOR16400 FHGROUP 43CR572141-01-01 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 560CB 642AB642BB 642CB 642DB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB660CBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUTIN RIB BAY 23-24.13000 FCOR60000 FH7800 FCOR40600 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 73RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572141-01-02 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUTIN RIB BAY 23-24.19800 FCOR102900 FH5600 FCOR29000 FHGROUP 42BORGROUP 43BPRE 48437572141-01-03 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAP RUNOUTIN RIB BAY 23-24.29700 FCOR59400 FH7600 FCOR15200 FHGROUP 43CR572144-01-01 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.15200 FCOR79000 FH4400 FCOR23000 FHGROUP 42AORGROUP 43A572144-01-03 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.29900 FCOR59800 FH6900 FCOR13800 FHGROUP 43CN572148-01-01 542DB 542EB 642DB 642EB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDINGBUTTSTRAPS.18000 FCOR102800 FH8400 FCOR48000 FHGROUP 42AORGROUP 43AN572148-01-02 542DB 542EB 642DB 642EB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDINGBUTTSTRAPS.19000 FCOR108400 FH8000 FCOR45700 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 74RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572154-01-04 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BERWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES, AND SPAR JOINT BOLTING ATRIB 27.17700 FCOR79900 FH14700 FCOR66500 FHGROUP 43EN572154-01-05 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BERWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES, AND SPAR JOINT BOLTING ATRIB 27.16700 FCOR90300 FH13900 FCOR75200 FHGROUP 43BPOST 48437R572158-01-01 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12AND RIB 23.11600 FCOR66400 FH4600 FCOR26600 FHGROUP 42APRE 40610ORGROUP 43APRE 40610R572159-01-01 542AB 542BB 542CB560CB 642AB 642BB642CB 660CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 ANDRIB 26.11600 FCOR66400 FH4600 FCOR26600 FHGROUP 42APRE 40610ORGROUP 43APRE 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 75RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R572162-01-01 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 27.13500 FCOR76800 FH5000 FCOR28800 FHGROUP 42AORGROUP 43AR572162-01-02 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 27.12100 FCOR68900 FH4800 FCOR27400 FHGROUP 42BORGROUP 43BPRE 48437572162-01-03 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 27.20100 FCOR40200 FH8900 FCOR17800 FHGROUP 43CR572164-01-01 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.10400 FCOR59700 FH3100 FCOR17900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572164-01-02 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.18400 FCOR104700 FH3100 FCOR17900 FHGROUP 42APOST 40610ORGROUP 43APOST 40610© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 76RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572164-01-07 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB560CB 641GB 641HB641JB 641KB 641LB641MB 641NB 641PB641QB 641RB 641SB642AB 642BB 642CB642DB 660CBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.19200 FCOR104000 FH7600 FCOR41200 FHGROUP 43BPOST 48437R572165-01-01 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP ANDBOTTOM FLANGES.10400 FCOR59700 FH3100 FCOR17900 FHGROUP 42APRE 40610ORGROUP 43APRE 40610N572165-01-02 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 27 AND RIB 39 INCLUDING TOP ANDBOTTOM FLANGES.18400 FCOR104700 FH3100 FCOR17900 FHGROUP 42APOST 40610ORGROUP 43APOST 40610N572174-01-01 541GB 541HB 541MB 541NB541SB 542AB 641GB 641HB641MB 641NB 641SB 642ABDETAILED INSPECTION OF OUTER WING RIBS 13, 18 AND23, AT SKIN ATTACHMENTS, REGION OF STRINGERCUTOUTS AND FORWARD FLAP TRACK BRACKETS.13400 FCOR75800 FH3800 FCOR21500 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 77RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572180-01-01 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.15500 FCOR88600 FH3400 FCOR19500 FHGROUP 42AORGROUP 43AN572180-01-02 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.15500 FCOR88600 FH3700 FCOR21300 FHGROUP 42BORGROUP 43BPRE 48437572180-01-03 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.24800 FCOR49600 FH5900 FCOR11800 FHGROUP 43C572180-01-04 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.17300 FCOR75000 FH7400 FCOR32000 FHGROUP 43E© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 78RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572180-01-05 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.15900 FCOR89900 FH6800 FCOR38300 FHGROUP 43BPOST 48437N572181-01-01 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.15500 FCOR88600 FH3400 FCOR19500 FHGROUP 42AORGROUP 43AN572181-01-02 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.15500 FCOR88600 FH3700 FCOR21300 FHGROUP 42BORGROUP 43BPRE 48437572181-01-03 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.24800 FCOR49600 FH5900 FCOR11800 FHGROUP 43CN572184-01-01 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-02-0115300 FCOR87400 FH4100 FCOR23800 FHGROUP 42AORGROUP 43AN572184-01-02 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-02-0215300 FCOR87300 FH4000 FCOR23000 FHGROUP 42BORGROUP 43BPRE 48437572184-01-03 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-02-0324500 FCOR49000 FH6400 FCOR12800 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 79RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N572184-02-01 541QB 641QBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-01-0115300 FCOR87400 FH4100 FCOR23800 FHGROUP 42AORGROUP 43AN572184-02-02 541QB 641QBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-01-0215300 FCOR87300 FH4000 FCOR23000 FHGROUP 42BORGROUP 43BPRE 48437572184-02-03 541QB 641QBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572184-01-0324500 FCOR49000 FH6400 FCOR12800 FHGROUP 43C572605-01-03 573BB 573FB 673BB673FBDETAILED INSPECTION OF OUTER WING TRAILING EDGERIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAPTRACK 2 AFT PICK UP (INCLUDING BOX BRACKET,INTERFACE PLATE AND THRUST PADS).16600 FC 16100 FC GROUP 43ER572605-01-04 573BB 573FB 673BB673FBDETAILED INSPECTION OF OUTER WING TRAILING EDGERIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAPTRACK 2 AFT PICK UP (INCLUDING BOX BRACKET,INTERFACE PLATE AND THRUST PADS).16600 FC 13000 FC GROUP 43BPOST 48437572606-01-02 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK_UP ASSEMBLY.10400 FC 10400 FC GROUP 43E572606-01-03 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK_UP ASSEMBLY.10400 FC 10400 FC GROUP 43BPOST 48437R573003-02-02 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP ANDWINGLET).17400 FCOR90300 FH5500 FCOR28700 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 80RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340573003-02-03 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP ANDWINGLET).23200 FCOR46400 FH7300 FCOR14600 FHGROUP 43CR574106-01-01 521BB 521CB 521DB521EB 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 660ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1TO TRACK RIB 16.11800 FCOR67300 FH11800 FCOR67300 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 81RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N574106-01-02 521BB 521CB 521DB521EB 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 623FBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1TO TRACK RIB 16.15600 FCOR88800 FH13000 FCOR60000 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 82RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574106-01-03 521BB 521CB 521DB521EB 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 623FBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1TO TRACK RIB 16.21600 FCOR43200 FH13000 FCOR26000 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 83RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574107-01-04 521FB 521GB 521HB521JB 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 623EBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE TOP SPREADER PLATE AND SUB-SPAR JOINTSTRAPS AT TRACK RIB 3 TO TRACK RIB 12.12900 FCOR58300 FH5200 FCOR23400 FHGROUP 43EN574107-02-02 521FB 521GB 521HB521JB 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 623EBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE TOP SPREADER PLATE AND SUB-SPARJOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.17700 FCOR101000 FH6700 FCOR38700 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 84RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574107-02-03 521FB 521GB 521HB521JB 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 623EBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE TOP SPREADER PLATE AND SUB-SPARJOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.24600 FCOR49200 FH9400 FCOR18800 FHGROUP 43CN574107-02-04 521FB 521GB 521HB521JB 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 623EBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE TOP SPREADER PLATE AND SUB-SPARJOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.12100 FCOR65800 FH3400 FCOR18800 FHGROUP 43BPOST 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 85RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R574109-01-01 521AB 521BB 521CB521DB 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 660ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLDDOWN RIBS.7800 FCOR44600 FH3100 FCOR18100 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 86RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R574109-01-02 521AB 521BB 521CB521DB 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 623QBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLDDOWN RIBS.7800 FCOR44800 FH3100 FCOR17700 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 87RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574109-01-03 521AB 521BB 521CB521DB 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 623NB623QBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLDDOWN RIBS.11900 FCOR23800 FH4700 FCOR9400 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 88RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574109-02-04 521AB 521BB 521CB521DB 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 623NB623QBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATES ANDSUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS(INCLUDING CLOSING RIBS AND TELESCOPE RIBS) ANDSLAT HOLD DOWN RIBS.19800 FCOR89200 FH5200 FCOR23400 FHGROUP 43EN574110-01-01 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 915500 FCOR88700 FH6600 FCOR38000 FHGROUP 42AORGROUP 43AN574110-01-02 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 919100 FCOR109200 FH8000 FCOR46000 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 89RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574110-01-03 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 1 TO RIB 927700 FCOR55400 FH11600 FCOR23200 FHGROUP 43CN574114-01-01 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 ANDRIB 26 TO RIB 39.15500 FCOR88700 FH6600 FCOR38000 FHGROUP 42AORGROUP 43AN574114-01-02 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 ANDRIB 26 TO RIB 39.19100 FCOR109200 FH8000 FCOR46000 FHGROUP 42BORGROUP 43BPRE 48437574114-01-03 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 24 ANDRIB 26 TO RIB 39.27700 FCOR55400 FH11600 FCOR23200 FHGROUP 43CN574115-01-01 522AB 522BB 522CB 523AB523BB 523CB 560AB 622AB622BB 622CB 623AB 623BB623CB 660ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGBOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OFFRONT SPAR FROM RIB 9 TO RIB 11 AND RIB 24 TO RIB 26.19200 FCOR109500 FH3400 FCOR19900 FHGROUP 42AORGROUP 43AN574115-01-02 522AB 522BB 522CB 523AB523BB 523CB 560AB 622AB622BB 622CB 623AB 623BB623CB 660ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGBOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OFFRONT SPAR FROM RIB 9 TO RIB 11 AND RIB 24 TO RIB 26.19200 FCOR109500 FH2900 FCOR16700 FHGROUP 42BORGROUP 43BPRE 48437R575011-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 1 AND RIB 14.9800 FCOR51100 FH2900 FCOR15000 FHGROUP 42APOST 42274ORGROUP 43APOST 42274R575011-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 1 AND RIB 14.11000 FCOR57000 FH2800 FCOR14600 FHGROUP 42BORGROUP 43BPRE 48437© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 90RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R575011-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 1 AND RIB 14.15700 FCOR31400 FH4900 FCOR9800 FHGROUP 43C575011-01-04 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 1 AND RIB 14.15700 FCOR72400 FH5200 FCOR23900 FHGROUP 43ER575011-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 1 AND RIB 14.16000 FCOR76600 FH4900 FCOR23400 FHGROUP 43BPOST 48437N575012-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.13400 FCOR76500 FH2100 FCOR12300 FHGROUP 42AORGROUP 43AR575012-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.12700 FCOR72400 FH4700 FCOR26900 FHGROUP 42BORGROUP 43BPRE 48437575012-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.22900 FCOR45800 FH9400 FCOR18800 FHGROUP 43CN575012-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.19400 FCOR109600 FH4200 FCOR23900 FHGROUP 43BPOST 48437N575014-01-01 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLGREINFORCING.16000 FCOR91400 FH6300 FCOR36400 FHGROUP 42AORGROUP 43A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 91RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N575017-01-02 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT,INTERNAL AND EXTERNAL, AFT OR REAR SPAR JUSTOUTBOARD OF GEAR SUPPORT RIB 6.17100 FCOR97400 FH1800 FCOR10600 FHGROUP 42BORGROUP 43BPRE 48437575018-01-02 147 AT 148 AT 191CT192 CTFLAPS DEPLOYEDDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.29800 FCOR59600 FH9200 FCOR18400 FHGROUP 43C575018-01-03 147 AT 148 AT 191CT192 CTFLAPS DEPLOYEDDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.15500 FC 12300 FC GROUP 43ER575018-01-04 147 AT 148 AT 191CT192 CTFLAPS DEPLOYEDDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.13400 FCOR75900 FH10700 FCOR60500 FHGROUP 43BPOST 48437N575018-01-05 147 AT 148 AT 191CT192 CTFLAPS DEPLOYEDDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.18800 FCOR107200 FH4600 FCOR26300 FHGROUP 42BORGROUP 43BPRE 48437R575022-01-01 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES 1 TO 3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.10100 FCOR57800 FH7600 FCOR43500 FHGROUP 42AORGROUP 43AR575022-01-03 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES 1 TO 3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.20200 FCOR40500 FH10600 FCOR21300 FHGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 92RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575022-01-04 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES 1 TO 3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.12300 FCOR55600 FH12300 FCOR55600 FHGROUP 43ER575022-01-05 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES 1 TO 3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.11600 FCOR62700 FH11600 FCOR62700 FHGROUP 43BPOST 48437R575023-01-01 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.9100 FCOR52100 FH2400 FCOR13700 FHGROUP 42AORGROUP 43AR575023-01-02 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.13700 FCOR27400 FH3300 FCOR6600 FHGROUP 43C575023-01-03 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.11800 FCOR53200 FH11800 FCOR53200 FHGROUP 43E© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 93RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R575023-01-04 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.11100 FCOR60300 FH11100 FCOR60300 FHGROUP 43BPOST 48437N575023-01-05 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKINOVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENTTO HINGEPOST AND ATTACHMENT OF HINGEPOST TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.10200 FCOR58100 FH2400 FCOR14200 FHGROUP 42BORGROUP 43BPRE 48437N575025-01-01 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.17500 FCOR99800 FH3600 FCOR20500 FHGROUP 42APOST 45739ORGROUP 43APOST 45739N575025-01-02 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.14700 FCOR83800 FH2500 FCOR14400 FHGROUP 42BORGROUP 43BPRE 48437575025-01-03 523AB 623AB DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.26500 FCOR53000 FH5000 FCOR10000 FHGROUP 43CR 575051-01-01 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK BEAM NO.1, UPPERFLANGES RADII OF ROLLER TRACKS.12000 FC 7300 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 94RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575051-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK BEAM NO.1, UPPERFLANGES RADII OF ROLLER TRACKS.13000 FC 7300 FC GROUP 43ED 575051-01-03 TASK DELETED IN ALI ISSUE 11575053-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO.1, DRIVE LINK,DRIVE LEVER, DRIVE STRUT AND CARRIAGE.12000 FC 7300 FC A340-200PRE 45326ORGROUP 43APRE 45326ORGROUP 43BPRE 45326ORGROUP 43CPRE 45326575054-01-01 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOXSUPPORT, FORK ASSEMBLY DRIVE STRUT AND CARRIAGE.13000 FC 7300 FC GROUP 43ER 575054-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO.1, GEAR BOXSUPPORT, FORK ASSEMBLY DRIVE STRUT AND CARRIAGE.12000 FC 7300 FC A340-200POST 45326ORGROUP 43APOST 45326ORGROUP 43BPOST 45326575055-01-02 734 744 DETAILED INSPECTION OF FLAP TRACK NO.1,ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITHLUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENTFITTING.12000 FC 7300 FC A340-200PRE 45326ORGROUP 43APRE 45326ORGROUP 43BPRE 45326ORGROUP 43CPRE 45326© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 95RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575055-01-03 734 744 DETAILED INSPECTION OF FLAP TRACK NO.1,ATTACHMENTS TO FUSELAGE (SWINGING LINKS WITHLUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENTFITTING.13000 FC 7300 FC GROUP 43ER 575057-01-01 FLAPS EXTENDEDAFT FLAP TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAM NO.2, 3, 4AND 5, UPPER FLANGES RADII.16000 FC 13400 FC A340-200ORA340-300D 575057-01-02 TASK DELETED IN ALI ISSUE 11575059-01-02 FLAPS EXTENDEDAFT FLAP TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5,DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITHTRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORTLINK AND TRAVELLING BEAM AT TRACK NO.4.16000 FC 13400 FC A340-200ORA340-300575061-01-02 FLAPS EXTENDED DETAILED INSPECTION OF FLAP TRACKS NO. 2, 3, 4 AND 5,CARRIAGE ASSEMBLIES.16000 FC 4000 FC A340-200POST 43303ORGROUP 43APOST 43303ORGROUP 43BPOST 43303ORGROUP 43CPOST 43303575061-01-03 FLAPS EXTENDEDAFT FLAP TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO.2, 3, 4 AND 5,CARRIAGE ASSEMBLIES.16000 FC 6200 FC GROUP 43E575063-01-01 FLAP TRACK FAIRINGS DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4AND 5 LOWER FLANGES, STRAP AND ANGLES.16000 FC 13400 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 96RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 575067-01-02 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: TASK MUST BE PERFORMED AT THE SAME TIME ASTASK 575067-02-02.13200 FC 5200 FC A340-200ORA340-300D 575067-01-03 TASK DELETED IN ALI ISSUE 11R 575067-02-02 FWD FLAP TRACKFAIRINGSSPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMSNO.2, 3, 4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: TASK MUST BE PERFORMED AT THE SAME TIME ASTASK 575067-01-0213200 FC 5200 FC A340-200ORA340-300D 575067-02-03 TASK DELETED IN ALI ISSUE 11575069-01-02 FLAPS EXTENDED DETAILED INSPECTION OF FLAP TRACK BEAMS NO.2, 3, 4AND 5, AFT ATTACHMENT SPIGOTS.15900 FC 10100 FC A340-200ORA340-300R 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 575401-02-013000 FC 3000 FC A340-200ORA340-300R 575401-02-01 FLAPS EXTENDED DETAILED INSPECTION OF INBOARD FLAP, EXTERNALSURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 575401-01-015700 FC 5700 FC A340-200ORA340-300575402-01-01 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKINAND DOUBLER IN CUT-OUT AREA FOR ATTACHMENTFITTINGS AT TRACK 2, LH/RH.13000 FC 4700 FC A340-200PRE 49008ORGROUP 43APRE 49008ORGROUP 43BPRE 49008ORGROUP 43CPRE 49008© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 97RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575402-01-02 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKINAND DOUBLER IN CUT-OUT AREA FOR ATTACHMENTFITTINGS AT TRACK 2, LH/RH.13000 FC 8600 FC GROUP 43E575402-01-03 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKINAND DOUBLER IN CUT-OUT AREA FOR ATTACHMENTFITTINGS AT TRACK 2, LH/RH.13000 FC 8000 FC A340-200POST 49008ORGROUP 43APOST 49008ORGROUP 43BPOST 49008R 575403-01-02 581AB 734 681AB744DETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO.1 AND TRUNNION,INTERNAL AND EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575403-02-0216000 FC 7900 FC A340-200ORA340-300D 575403-01-04 TASK DELETED IN ALI ISSUE 11R 575403-02-02 581AB 734 681AB744SPECIAL DETAILED INSPECTION OF INBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO.1 ANDTRUNNION, INTERNAL AND EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575403-01-0216000 FC 7900 FC A340-200ORA340-300D 575403-02-04 TASK DELETED IN ALI ISSUE 11© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 98RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 575405-01-02 531AT 531CB 631AT631CBFLAPS EXTENDEDDETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO.2 AND EXTERNAL DRIVESTRUT BRACKET, CARRIAGE ATTACHMENT BRACKET ANDGUIDE ARM ATTACHMENT BRACKET.16000 FC 11000 FC A340-200PRE 49008ORGROUP 43APRE 49008ORGROUP 43BPRE 49008ORGROUP 43CPRE 49008575503-01-02 532AT 532CB 632AT632CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO.3, AND EXTERNAL DRIVESTRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGEWITH ASSOCIATED ATTACH FITTING AND GUIDE ARMATTACH FITTING.16000 FC 13400 FC A340-200ORA340-300575503-02-02 532AT 532CB 632AT632CBSPEED TAPEFLAPS EXTENDEDSPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO.3.16000 FC 13400 FC A340-200ORA340-300575505-01-02 533AT 533CB 633AT633CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO.4, AND EXTERNAL FWD.SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.16000 FC 13400 FC A340-200ORA340-300575505-02-02 533AT 533CB 633AT633CBSPEED TAPEFLAPS EXTENDEDSPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO.4.16000 FC 13400 FC A340-200ORA340-300575507-01-02 534AT 534CB 634AT634CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO.5, AND EXTERNAL DRIVESTRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITHASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.16000 FC 13400 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 99RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575507-02-02 534AT 534CB 634AT634CBSPEED TAPEFLAPS EXTENDEDSPECIAL DETAILED INSPECTION OF OUTBOARDFLAP,INTERNAL SUPPORT FITTING AT TRACK NO.5.16000 FC 13400 FC A340-200ORA340-300575509-01-02 RUBBER SEALFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INNER ENDRIB INCLUDING ROLLER AND INTERCONNECTION STRUTATTACHMENT BRACKET, EXTERNAL.16000 FC 13400 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C575509-02-02 RUBBER SEALSPEED TAPEFLAPS EXTENDEDSPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INNER END RIB INCLUDING ROLLER ANDINTERCONNECTION STRUT ATTACHMENT BRACKET,INTERNAL.16000 FC 13400 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C577003-01-02 SPOILERS DEPLOYEDFLAPS EXTENDEDDETAILED INSPECTION OF SPOILER NO.1, HINGE ANDACTUATOR ATTACHMENT FITTINGS (6 PLACES).12000 FC 6000 FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C577003-01-03 SPOILERS DEPLOYEDFLAPS EXTENDEDDETAILED INSPECTION OF SPOILER NO.1, HINGE ANDACTUATOR ATTACHMENT FITTINGS (6 PLACES).13000 FC 6000 FC GROUP 43E711311-01-01 415AL 416AR 425AL426AR 435AL 436AR445AL 446ARDISASSEMBLY ONE BYONE OF THE HINGE BOLTIS REQUIREDDETAILED INSPECTION OF FAN COWL HINGE FITTINGS ,SLEEVES, PINS AND SURROUNDING STRUCTURE (15 CMAROUND HINGE FITTINGS).4500 FC 4500 FC A340-200ORA340-300711312-01-01 415AL 416AR 425AL426AR 435AL 436AR445AL 446ARDETAILED INSPECTION OF FAN COWL LATCHES ANDSURROUNDING STRUCTURE (15 CM AROUND FITTINGS).1500 FC 1500 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 100RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340712101-01-01 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARDETAILED INSPECTION OF FORWARD ENGINE MOUNTINSTALLATION.2800 FCOR14000 FH2800 FCOR14000 FHGROUP 42AORGROUP 43AORGROUP 42BORGROUP 43BORGROUP 43E712101-01-02 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARDETAILED INSPECTION OF FORWARD ENGINE MOUNTINSTALLATION.2800 FCOR5600 FH2800 FCOR5600 FHGROUP 43C712201-01-01 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARDETAILED INSPECTION OF AFT ENGINE MOUNTINSTALLATION.4500 FCOR22500 FH4500 FCOR22500 FHGROUP 42AORGROUP 43AORGROUP 42BOR712201-01-02 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARDETAILED INSPECTION OF AFT ENGINE MOUNTINSTALLATION.4500 FCOR9000 FH4500 FCOR9000 FHGROUP 43C722301-01-01 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARSPECIAL DETAILED INSPECTION OF THE FAN CASE VGROOVE INNER RADIUS.10800FC 10800FC A340-200ORGROUP 43AORGROUP 43BORGROUP 43C© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 101RevcodeTASKREFERENCEACCESS TASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R 783205-01-01 415AL 416AR 417AL418AR 425AL 426AR427AL 428AR 435AL436AR 437AL 438AR445AL 446AR 447AL448ARSPECIAL DETAILED INSPECTION OF THE THRUSTREVERSER 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)"13000 FC 1580 FC A340-200PRE 51179ORA340-300PRE 51179R783211-01-01 417AL, 418AR, 427AL,428AR, 437AL, 438AR,447AL, 448AR,415AL, 425AL, 435AL,445AL,416AR, 426AR, 436AR,446ARDISASSEMBLY ONE BYONE OF HINGE BOLTS ISREQUIREDDETAILED INSPECTION OF THRUST REVERSER HINGEFITTINGS , SLEEVES, PINS AND SURROUNDINGSTRUCTURE (15 CM AROUND HINGE FITTINGS).4500 FC 4500 FC A340-200ORA340-300R783212-01-01 417AL, 418AR, 427AL,428AR, 437AL, 438AR,447AL, 448AR415AL, 425AL, 435AL,445AL,416AR, 426AR, 436AR,DETAILED INSPECTION OF THRUST REVERSER LATCHASSEMBLY, AND SURROUNDING STRUCTURE (15 CMAROUND LATCH ATTACHMENTS).1500 FC 1500 FC A340-200ORA340-300© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.1 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 102RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY521121-01-01 831 841 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONFWD PASSENGER/CRES DOORS, LH/RH.11000 FC 11000 FC A340-500ORA340-600521123-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A340-500ORA340-600521221-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A340-500ORA340-600521223-01-01 832 842 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 2 (MID PASSENGER/CREW DOOR).11000 FC 11000 FC A340-500ORA340-600521321-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A340-500ORA340-600521323-01-01 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 4 (AFT PASSENGER/CREW DOOR).11000 FC 11000 FC A340-500ORA340-600522121-01-02 N/A GENERAL VISUAL INSPECTION OF OVERWING EMERGENCYEXIT DOOR SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A340-600POST 47050522123-01-01 836 846 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONOVERWING EMERGENCY EXIT DOOR.11000 FC 11000 FC A340-600522221-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNALSURFACE.8500 FC 8500 FC A340-500ORA340-600522223-01-01 834 844 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).11000 FC 11000 FC A340-500ORA340-600AIRWORTHINESS LIMITATIONS SECTIONSECTION 2.2 - A340-500/600 AIRWORTHINESS LIMITATIONSA340© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 1RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340523126-01-01 DOOR LINING DETAILED INSPECTION OF FWD CARGO COMPARTMENTDOOR, FRAME 20B BETWEEN BEAM 3 AND BEAM 4.10600 FC 2600 FC A340-500PRE 51038PRE 50528ORA340-600PRE 51038PRE 50528524121-02-01 N/A DETAILED INSPECTION OF AVIONICS COMPARTMENTACCESS DOOR SKIN, EXTERNAL SURFACE.10400 FC 10400 FC A340-500ORA340-600528123-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS,FWD AND AFT HINGES, INCLUDING FITTINGS ONKEELBEAM, LH/RH.5700 FC 5700 FC A340-500ORA340-600528125-01-01 734 744 DETAILED INSPECTION OF MAIN LANDING GEAR DOORS,CENTER HINGE, INCLUDING FITTINGS ON KEELBEAM,LH/RH.4000 FC 4000 FC A340-500ORA340-600528223-01-01 713 714 DETAILED INSPECTION OF NOSE LANDING GEAR,FORWARD DOORS, HINGES (NO.1, NO.2, NO.3) INCLUDINGFITTINGS ON FUSELAGE, LH/RH.7300 FC 7300 FC A340-500ORA340-600528323-01-01 753 754 DETAILED INSPECTION OF CENTER LANDING GEAR, MAINDOORS, HINGES (NO.1, NO.2, NO.3), INCLUDING FITTINGSON KEELBEAM, LH/RH.2500 FC 2500 FC A340-500ORA340-600531810-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD,EXTERNAL SURFACE, LH/RH.12200 FCOR97600 FH12200 FCOR97600 FHA340-500ORGROUP 46A531810-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.10 AND FR.13 FROM FLOOR LEVEL TO STR.9 FWD,EXTERNAL SURFACE, LH/RH.12400 FCOR85200 FH12400 FCOR85200 FHGROUP 46B531812-01-02 N/A DETAILED INSPECTION OF FUSELAGE STRUCTUREAROUND DOOR 1 (FWD PAX/CREW DOOR), EXTERNALSURFACE BETWEEN FR.13 AND FR.18 FROM LATERALLONGITUDINAL LAP JOINT TO STR.9 AFT, LH/RH.8800 FCOR52800 FH8800 FCOR52800 FHA340-500ORA340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 2RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531816-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN ANDJOINT SURFACES BETWEEN FR.0 AND FR.18/19 BELOWCABIN FLOOR LEVEL, EXTERNAL SURFACE.5800 FCOR35100 FH5800 FCOR35100 FHGROUP 45AORGROUP 46A531816-01-04 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN ANDJOINT SURFACES BETWEEN FR.0 AND FR.18/19 BELOWCABIN FLOOR LEVEL, EXTERNAL SURFACE.4450 FCOR30600 FH4450 FCOR30600 FHGROUP 45BORGROUP 46B531818-01-02 121EL713 714715 716811DETAILED INSPECTION OF FUSELAGE LOWER SKIN ATAVIONICS COMPARTMENT ACCESS DOOR CUTOUT,GROUND SERVICES CONNECTION ACCESS DOOR CUTOUTAND NOSE LANDING GEAR CUTOUT, BETWEEN FR.7 ANDFR.19.8000 FCOR50000 FH8000 FCOR50000 FHA340-500ORA340-600531820-01-02 713 714715 716GENERAL VISUAL INSPECTION OF NOSE LANDING GEARBAY INTERNAL STRUCTURE, NOSE LANDING GEAR WELLPANELS.4100 FCOR28800 FH4100 FCOR28800 FHA340-500ORA340-600531824-01-01 713 714715 716DETAILED INSPECTION OF NOSE LANDING GEAR BAYINTERNAL STRUCTURE, BEAM BETWEEN LANDING GEARBEARINGS, LH/RH.5950 FCOR35900 FH5950 FCOR35900 FHA340-500ORA340-600531827-01-02 713 714715 716GENERAL VISUAL INSPECTION OF NOSE LANDING GEARBAY, ANGLE FITTINGS LINKING FORWARD CANTED PANELTO ROOF PANEL.6800 FCOR40800 FH6800 FCOR40800 FHA340-500ORA340-600531830-01-02 711/712/713/714/715/716,NLG, BEARING811SPECIAL DETAILED INSPECTION OF NLG MAINATTACHMENT BEARING BORE.8000 FCOR50000 FH4000 FCOR32000 FHA340-500ORA340-600531831-01-02 711/712/713/714/715/716,BEARING, DRAG STRUT811SPECIAL DETAILED INSPECTION OF NLG DRAG STRUTBEARING HOLE IN LATERAL PANEL.8000 FCOR50000 FH4000 FCOR32000 FHA340-500ORA340-600531832-01-01 711/712/713/714/715/716,NLG, BEARINGSPECIAL DETAILED INSPECTION OF NLG MAINATTACHMENT BEARING LUBRICATION HOLE.8000 FCOR50000 FH4000 FCOR32000 FHA340-500ORA340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 3RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531833-01-03 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, AIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAMJUNCTION ON FRAME 12A AT STRINGER 26 LEVEL, LH/RH.13200 FC 8300 FC A340-500ORA340-600531835-01-01 N/A SPECIAL DETAILED INSPECTION OF REAR LOWER CORNEROF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OFFR.10, EXTERNAL SURFACE, LH/RH.4600 FCOR27600 FH4600 FCOR27600 FHA340-500ORA340-600531843-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, AIR CONDITIONINGDUCTS, VACUUM PIPESDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING ATFR.14, LH/RH.12700 FC 3700 FC A340-500ORA340-600531844-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, AIR CONDITIONINGDUCTS, VACUUM PIPESSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FR.14 ANDCRUCIFORM FITTING, LH/RH.12700 FC 6700 FC A340-500ORA340-600531854-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGS, SLIDINGWINDOWS OPENEDDETAILED INSPECTION OF LOWER SURFACE OF UPPERCLOSING PANEL BETWEEN FR.7 AND FRONT WINDSHIELDSIDE POST, INTERNAL STRUCTURE, LH/RH.11800 FC 7800 FC A340-500ORA340-600531877-01-01 811 SPECIAL DETAILED INSPECTION OF FREE FLANGE ANDWEB OF FRAME 17 AT JUNCTION WITH THE ROD FITTING.8000 FCOR50000 FH4000 FCOR27500 FHGROUP 45AORA340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 4RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340531877-01-02 811 SPECIAL DETAILED INSPECTION OF FREE FLANGE ANDWEB OF FRAME 17 AT JUNCTION WITH THE ROD FITTING.8000 FCOR50000 FH3600 FCOR29400 FHGROUP 45B531878-01-01 713 714715 716GENERAL VISUAL INSPECTION OF STRUCTURE AROUNDCENTRAL HOLE OF NLG BAY AFT PANEL.8000 FCOR50000 FH4000 FCOR25000 FHA340-500ORA340-600531879-02-01 811 DETAILED INSPECTION OF NLG BAY LOWER ARCH FRAMES12 TO 16 SPLICINGS, LH/RH.8000 FCOR50000 FH4300 FCOR25900 FHGROUP 45AORGROUP 46A531879-02-02 811 DETAILED INSPECTION OF NLG BAY LOWER ARCH FRAMES12 TO 16 SPLICINGS, LH/RH.8000 FCOR50000 FH3800 FCOR26200 FHGROUP 45BORGROUP 46B531881-01-01 811 SPECIAL DETAILED INSPECTION OF NLG BAY LOWER ARCHFRAMES 16A SPLICING.8000 FCOR50000 FH4000 FCOR25000 FHA340-500ORA340-600531894-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, GUSSET AND MACHINED STIFFENERSBETWEEN STRINGERS 14 AND 24, AND BETWEEN FR.17AND FR.18, LH/RH.12400 FC 7000 FC A340-500ORA340-600R532201-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR.18 AND FR.38 FROMSTR.26 LH/RH TO BOTTOM CENTER LINE, EXCLUDING AREAUNDERNEATH BELLY FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532201-02-02.2200 FC 2200 FC A340-500ORA340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 5RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N532201-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR.18 AND FR.38 FROM STR.26 LH/RHTO BOTTOM CENTER LINE, EXCLUDING AREAUNDERNEATH BELLY FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532201-01-02.6900 FC 6900 FC A340-500ORA340-600532214-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENTDOOR CUT-OUT AT UPPER AND LOWER CORNERS.10000 FCOR77700 FH6000 FCOR46600 FHA340-500ORA340-600532215-01-02 821 GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR.20A AND FR.25A).3500 FC 3500 FC A340-500ORA340-600R532217-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR.18 AND FR.38 FROMSTR.6 TO STR.26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532217-02-02.11000 FC 2200 FC A340-500ORA340-600N532217-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR.18 AND FR.38 FROM STR.6 TOSTR.26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532217-01-02.11000 FC 6900 FC A340-500ORA340-600532224-02-01 832/842SCUFF PLATESPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.9000 FC 5300 FC A340-500ORA340-600532225-01-01 832/842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 CUT-OUT UPPER CORNERS, LH/RH.9000 FC 5300 FC A340-500ORA340-600532253-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOWVALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR.32AND FR.33, FROM STR.45 TO STR.49, LH ONLY.9300 FC 4000 FC A340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 6RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340532253-02-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOWVALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR.37.2AND FR.37.3, FROM STR.45 TO STR.49, LH ONLY.12500 FC 5500 FC A340-500N532266-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR18 AND FR 38 FROMSTR6 LH/RH TO CROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532266-02-024500 FC 4500 FC A340-500ORA340-600N532266-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR18 AND FR 38 FROM STR6 LH/RH TOCROWN CENTERLINE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532266-0-026900 FC 6900 FC A340-500ORA340-600533720-01-02 191AB 192AB 192GB192KB 193CB 193FBLEFT RAM AIR INLETDETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TOFR40.3, ANGLE FITTING BETWEEN LATERAL PANEL ANDSKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE,LH/RH.6900 FCOR45000 FH6900 FCOR45000 FHGROUP 46A533720-01-03 191AB 192AB 192GB192KB 193CB 193FBLEFT RAM AIR INLETDETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TOFR40.3, ANGLE FITTING BETWEEN LATERAL PANEL ANDSKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE,LH/RH.6800 FCOR47200 FH6800 FCOR47200 FHGROUP 46B533720-01-04 191AB 192AB 192GB192KB 193CB 193FBLEFT RAM AIR INLETDETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TOFR40.3, ANGLE FITTING BETWEEN LATERAL PANEL ANDSKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE,LH/RH.6800 FCOR52500 FH6800 FCOR52500 FHGROUP 45A533720-01-05 191AB 192AB 192GB192KB 193CB 193FBLEFT RAM AIR INLETDETAILED INSPECTION OF KEEL BEAM, FROM FR38.1 TOFR40.3, ANGLE FITTING BETWEEN LATERAL PANEL ANDSKIN OF FORWARD LOWER SHELL, EXTERNAL SURFACE,LH/RH.6800 FCOR54800 FH6800 FCOR54800 FHGROUP 45B533722-01-02 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR53.8, ANGLE FITTINGS BETWEEN LATERAL PANEL AND SKINOF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.6900 FCOR44900 FH6900 FCOR44900 FHGROUP 46A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 7RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533722-01-03 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKINOF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.6800 FCOR47200 FH6800 FCOR47200 FHGROUP 46B533722-01-04 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKINOF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.6800 FCOR52500 FH6800 FCOR52500 FHGROUP 45A533722-01-05 197EB 198EB DETAILED INSPECTION OF KEEL BEAM, FROM FR 53 TO FR53.8, ANGLE FITTING BETWEEN LATERAL PANEL AND SKINOF AFT LOWER SHELL, EXTERNAL SURFACE, LH/RH.6800 FCOR54800 FH6800 FCOR54800 FHGROUP 45B533730-01-02 143AB 753754DETAILED INSPECTION OF KEEL BEAM, TORQUE BOXEXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.7800 FCOR51100 FH7800 FCOR51100 FHGROUP 46A533730-01-03 143AB 753754DETAILED INSPECTION OF KEEL BEAM, TORQUE BOXEXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.7700 FCOR53300 FH7700 FCOR53300 FHGROUP 46B533730-01-04 143AB 753754DETAILED INSPECTION OF KEEL BEAM, TORQUE BOXEXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.6200 FCOR47700 FH6200 FCOR47700 FHGROUP 45A533730-01-05 143AB 753754DETAILED INSPECTION OF KEEL BEAM, TORQUE BOXEXTERNAL SURFACE AND ATTACHMENT FITTINGS, LH/RH.6100 FCOR49100 FH6100 FCOR49100 FHGROUP 45B533733-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF FWD AND AFT CORNERFITTINGS OF MLG DOOR ACTUATOR, INNER RADIUS OFINTERMEDIATE WEB, LH/RH.5900 FC 3400 FC A340-600POST 49655PRE 52694ORA340-500POST 49655PRE 52694533801-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLYFAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE,LH/RH.12300 FCOR80500 FH2300 FCOR15100 FHGROUP 46A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 8RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533801-01-03 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLYFAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE,LH/RH.14000 FCOR96600 FH2600 FCOR18100 FHGROUP 46B533801-01-04 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLYFAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE,LH/RH.14300 FCOR109200 FH2100 FCOR16400 FHGROUP 45A533801-01-05 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR.38 AND FR.54 FROM UPPER EDGE OF BELLYFAIRING TO CROWN CENTERLINE, EXTERNAL SURFACE,LH/RH.15000 FCOR120200 FH2800 FCOR22500 FHGROUP 45B533805-01-01 N/A SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXITDOOR CORNERS, LH/RH.10200 FCOR77800 FH5100 FCOR39000 FHGROUP 45A533805-01-02 N/A SPECIAL DETAILED INSPECTION OF THE EMERGENCY EXITDOOR CORNERS, LH/RH.13300 FCOR106400 FH3700 FCOR30100 FHGROUP 45B533806-01-01 N/A DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR,PANELS AND DOUBLER ENTRIES BETWEEN FR.53.4 ANDFR.53.8 AND FROM STR.12 TO STR.18 AND FROM STR.23 TOSTR.29, EXTERNAL SURFACE, LH/RH.16300 FCOR124300 FH4500 FCOR34900 FHGROUP 45A533806-01-02 N/A DETAILED INSPECTION OF THE EMERGENCY EXIT DOOR,PANELS AND DOUBLER ENTRIES BETWEEN FR.53.4 ANDFR.53.8 AND FROM STR.12 TO STR.18 AND FROM STR.23 TOSTR.29, EXTERNAL SURFACE, LH/RH.15900 FCOR127300 FH3000 FCOR24400 FHGROUP 45B533808-01-01 834, 822FLOOR PANELS ANDINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF THE EMERGENCY EXIT DOOR,INTERNAL STRUCTURE, FRAMES 53.5 AND 53.6A FROMSTGR 9 TO 31, AND FRAMES 53.4 TO FR. 53.7, FROM STGR 9TO STGR 11 AND FROM STGR 28 TO STGR 30, LH/RH.15100 FCOR115800 FH2700 FCOR20700 FHGROUP 45A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 9RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533808-01-02 834, 822FLOOR PANELS ANDINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF THE EMERGENCY EXIT DOOR,INTERNAL STRUCTURE, FRAMES 53.5 AND 53.6A FROMSTGR 9 TO 31, AND FRAMES 53.4 TO FR. 53.7, FROM STGR 9TO STGR 11 AND FROM STGR 28 TO STGR 30, LH/RH.14900 FCOR119600 FH3500 FCOR28400 FHGROUP 45B533811-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF THE EMERGENCY EXITDOOR, INTERNAL STRUCTURE, SPLICES BETWEEN BEAMSAND STRINGERS 14, 15, 26 AND 27, AT FR.53.3, FR.53.4 AND53.8, LH/RH.10800 FCOR82300 FH3200 FCOR25000 FHGROUP 45A533811-01-02 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF THE EMERGENCY EXITDOOR, INTERNAL STRUCTURE, SPLICES BETWEEN BEAMSAND STRINGERS 14, 15, 26 AND 27 AT FR.53.3, FR.53.4 AND53.8, LH/RH.8100 FCOR65200 FH2400 FCOR19400 FHGROUP 45B533816-01-01 834,FLOOR PANELS,INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF THE UPPER FRAMESTO FOOT FRAME SPLICINGS FROM FRAMES 48 TO 53.2,INTERNAL STRUCTURE, LH/RH.11600 FCOR88700 FH2800 FCOR22000 FHGROUP 45A533819-01-01 INSULATION TO BEDISPLACED AS REQUIRED,LINING, GALLEY ORLAVATORY IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGSAT CIRCUMFERENTIAL JUNCTION AT FR.45 AND FR.54,FROM STR.15 LH TO STR.15 RH.6600 FCOR42900 FH1500 FCOR9700 FHGROUP 46A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 10RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533819-01-02 INSULATION TO BEDISPLACED AS REQUIRED,LINING, GALLEY ORLAVATORY IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGSAT CIRCUMFERENTIAL JUNCTION AT FR.45 AND FR.54,FROM STR.15 LH TO STR.15 RH.4700 FCOR32100 FH1400 FCOR10000 FHGROUP 46B533819-01-03 INSULATION TO BEDISPLACED AS REQUIRED,LINING, GALLEY ORLAVATORY IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGSAT CIRCUMFERENTIAL JUNCTION AT FR45 AND FR54, FROMSTR15 LH TO STR15 RH.7800 FCOR60000 FH1600 FCOR12600 FHGROUP 45A533819-01-04 INSULATION TO BEDISPLACED AS REQUIRED,LINING, GALLEY ORLAVATORY IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGERS SPLICINGSAT CIRCUMFERENTIAL JUNCTION AT FR45 AND FR54, FROMSTR15 LH TO STR15 RH.5300 FCOR42900 FH1600 FCOR12900 FHGROUP 45BR533820-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FOOT FRAME RADIIFROM FR.48 TO FR.53.1, INCLUDING AREA AROUNDFASTENER HOLES OF BRACKETS WHERE INSTALLED,LH/RH.7700FCOR50200 FH3300 FCOR21500 FHGROUP 46APRE 57860D533820-01-02 TASK DELETED IN ISSUE 11R533820-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FOOT FRAME RADIIFROM FR.48 TO FR.53.1, INCLUDING AREA AROUNDFASTENER HOLES OF BRACKETS WHERE INSTALLED,LH/RH.8200FCOR63000 FH3500FCOR27000 FHGROUP 45APRE 57860D533820-01-04 TASK DELETED IN ISSUE 11R533821-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF PRESSURIZEDMEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.8820 FCOR57300 FH4150 FCOR27000 FHGROUP 46APRE 57290PRE 57291R533821-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF PRESSURIZEDMEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.10900 FCOR83400 FH6030 FCOR46000 FHGROUP 45APRE 57290PRE 57291© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 11RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N533821-01-04 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF PRESSURIZEDMEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.7340FCOR58700 FH3400 FCOR27200 FHGROUP 45BPRE 54510ANDPRE 57291N533821-01-05 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF PRESSURIZEDMEMBRANES, UPPER FACE, AT FR.47, Y+/-953 AND Y+/-1959AND AT FR.48, Y+/-450, Y+/-953, Y+/- 1456 AND Y+/-1959.9320 FCOR64000 FH4160 FCOR28600 FHGROUP 46BPRE 54510ANDPRE 57291533822-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAMWEB AROUND FIXED SUPPORT HOLES AT FR.53.3.11100 FCOR72400 FH3200 FCOR20800 FHGROUP 46APRE49432533822-01-02 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAMWEB AROUND FIXED SUPPORT HOLES AT FR.53.3.10600 FCOR73300 FH3000 FCOR20900 FHGROUP 46BPRE 49432533822-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAMWEB AROUND FIXED SUPPORT HOLES AT FR.53.3.13300 FCOR86900 FH3200 FCOR21300 FHGROUP 46APOST49432533822-01-04 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF FLOOR CROSSBEAMWEB AROUND FIXED SUPPORT HOLES AT FR.53.3.13800 FCOR94900 FH3500 FCOR24000 FHGROUP 46BPOST 49432533824-01-01 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEELBEAM LOWER FITTING IN SPLICING AREA BETWEEN KEELBEAM AND FR.53.2, LH/RH.4000 FCOR26400 FH4000 FCOR26400 FHGROUP 46A533824-01-02 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEELBEAM LOWER FITTING IN SPLICING AREA BETWEEN KEELBEAM AND FR.53.2, LH/RH.6400 FCOR44300 FH6400 FCOR44300 FHGROUP 46B533824-01-03 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEELBEAM LOWER FITTING IN SPLICING AREA BETWEEN KEELBEAM AND FR.53.2, LH/RH.4100 FCOR31200 FH4100 FCOR31200 FHGROUP 45A533824-01-04 734 744 SPECIAL DETAILED INSPECTION OF Y FITTING AND KEELBEAM LOWER FITTING IN SPLICING AREA BETWEEN KEELBEAM AND FR.53.2, LH/RH.6400 FCOR48900 FH6400 FCOR48900 FHGROUP 45B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 12RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533825-01-02 734 744753 754GENERAL VISUAL INSPECTION OF FWD FACE OF FR.53.2PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET ANDCONNECTION PLATES LATERAL PANEL, BETWEENSTIFFENER 1 TO 9.4200 FCOR27700 FH4200 FCOR27700 FHGROUP 46A533825-01-03 734 744753 754GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET ANDCONNECTION PLATES LATERAL PANEL, BETWEENSTIFFENER 1 TO 9.4100 FCOR28800 FH4100 FCOR28800 FHGROUP 46B533825-01-04 734 744753 754GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET ANDCONNECTION PLATES LATERAL PANEL.6700 FCOR51800 FH6700 FCOR51800 FHGROUP 45A533825-01-05 734 744753 754GENERAL VISUAL INSPECTION OF FWD FACE OF FR 53.2PRESSURE BULKHEAD INCLUDING FOOTFRAME, FLAPTRACK BRACKETS, UPPER SUPPORT BRACKET ANDCONNECTION PLATES LATERAL PANEL.6700 FCOR54300 FH6700 FCOR54300 FHGROUP 45B533828-01-02 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEARSUPPORT FITTINGS ON FR.53.2, INCLUDING RIVET ROWSAT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORTSTRUT.10500 FCOR69100 FH10500 FCOR69100 FHGROUP 46A533828-01-03 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEARSUPPORT FITTINGS ON FR.53.2, INCLUDING RIVET ROWSAT JUNCTION WITH FR.53.2, AND HALFWAY SUPPORTSTRUT.8200 FCOR56400 FH8200 FCOR56400 FHGROUP 46B533828-01-04 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEARSUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS ATJUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.8600 FCOR65600 FH8600 FCOR65600 FHA340-500PRE 48487533828-01-05 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEARSUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS ATJUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.7000 FCOR53700 FH7000 FCOR53700 FHGROUP 45APOST 48487© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 13RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533828-01-06 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEARSUPPORT FITTING ON FR.53.2, INCLUDING RIVET ROWS ATJUNCTION WITH FR.53.2, AND HALFWAY SUPPORT STRUT.6100 FCOR49100 FH6100 FCOR49100 FHGROUP 45B533829-01-01 FLOOR PANELLININGDETAILED INSPECTION OF FLOOR IN LOWER DECKFACILITIES CONFIGURATION FROM FR.53.8 TO FR.54, FROMY+1456 TO Y-1456.16200 FCOR105300 FH3900 FCOR25500 FHGROUP 46APOST 48487ANDPOST 49432533829-01-02 FLOOR PANELLININGDETAILED INSPECTION OF FLOOR IN LOWER DECKFACILITIES CONFIGURATION FROM FR.53.8 TO FR.54, FROMY+1456 TO Y-1456.15600 FCOR107700 FH3400 FCOR23500 FHGROUP 46BPOST 49432533831-01-02 734 744753 754DETAILED INSPECTION OF FORWARD FACE OF FR.53.2PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.7300 FCOR47900 FH7300 FCOR47900 FHGROUP 46A533831-01-03 734 744753 754DETAILED INSPECTION OF FORWARD FACE OF FR.53.2PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.7300 FCOR50500 FH7300 FCOR50500 FHGROUP 46B533831-01-04 734 744753 754DETAILED INSPECTION OF FORWARD FACE OF FR.53.2PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.6700 FCOR51800 FH6700 FCOR51800 FHGROUP 45A533831-01-05 734 744753 754DETAILED INSPECTION OF FORWARD FACE OF FR.53.2PRESSURE BULKHEAD, LOWER PART BELOW STIFFENER 9.6700 FCOR54300 FH6700 FCOR54300 FHGROUP 45B533835-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGER 22 AT LONGITUDINALJUNCTION FROM FR.38 TO FR.54, LH/RH.15300 FCOR99700 FH9000 FCOR58600 FHGROUP 46A533835-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGER 22 AT LONGITUDINALJUNCTION FROM FR.38 TO FR.54, LH/RH.15300 FCOR105200 FH9400 FCOR64800 FHGROUP 46B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 14RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533835-01-03 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGER 22 AT LONGITUDINALJUNCTION FROM FR.38 TO FR.54, LH/RH.15800 FCOR120800 FH8400 FCOR64700 FHGROUP 45A533835-01-04 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGER 22 AT LONGITUDINALJUNCTION FROM FR.38 TO FR.54, LH/RH.15800 FCOR126500 FH5800 FCOR46600 FHGROUP 45B533837-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TOFR.54, LH/RH.15300 FCOR99700 FH8700 FCOR56800 FHGROUP 46A533837-01-02 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TOFR.54, LH/RH.15300 FCOR105200 FH8600 FCOR59700 FHGROUP 46B533837-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TOFR.54, LH/RH.15800 FCOR120800 FH8400 FCOR64700 FHGROUP 45A533837-01-04 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STRINGER 22 FROM FR.38 TOFR.54, LH/RH.15800 FCOR126500 FH5800 FCOR46600 FHGROUP 45B533839-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.8400 FCOR54800 FH2200 FCOR14400 FHGROUP 46APRE 47131533839-01-02 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.16500 FCOR114000 FH5900 FCOR41000 FHGROUP 46BPRE 49432PRE 47533© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 15RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533839-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.8400 FCOR54800 FH3500 FCOR22900 FHGROUP 46APOST 48924533839-01-04 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.8400 FCOR54800 FH3000 FCOR19600 FHGROUP 46APOST 47131PRE 48924533839-01-05 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.10500 FCOR72100 FH3400 FCOR23900 FHGROUP 46BPOST 49432ORPOST 47533533839-01-06 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDDETAILED INSPECTION OF FRAMES AND CROSSBEAMSSPLICINGS AND SURROUNDING AREA AT STR.26, FROMFR.53.3 TO FR.54, LH/RH.14100 FCOR107800 FH4100 FCOR31900 FHGROUP 45A533845-01-01 822LDF FURNISHING ANDEQUIPMENTSPECIAL DETAILED INSPECTION OF FRAME SPLICES ANDCROSSBEAMS AT SPLICING LEVEL FROM FR.53.3 TO FR.54OF AFT CARGO STRUCTURE LOWER DECK FACILITIES(LDF), LH/RH.14900 FCOR97300 FH2800 FCOR18100 FHGROUP 46APOST 49431533845-01-02 822LDF FURNISHING ANDEQUIPMENTSPECIAL DETAILED INSPECTION OF FRAME SPLICES ANDCROSSBEAMS AT SPLICING LEVEL FROM FR.53.3 TO FR.54OF AFT CARGO STRUCTURE LOWER DECK FACILITIES(LDF), LH/RH.14800 FCOR101900 FH1500 FCOR10900 FHGROUP 46BPOST 49431533846-01-01 822LDF FURNISHING ANDEQUIPMENTSPECIAL DETAILED INSPECTION OF FRAME SPLICES FROMFR.53.7 TO FR.53.9, BETWEEN STR.43 AND STR.44, ONLOWER DECK AFT CARGO STRUCTURE OF LDF, LH/RH.15700 FCOR102300 FH3900 FCOR25700 FHGROUP 46APOST 49431533846-01-02 822LDF FURNISHING ANDEQUIPMENTSPECIAL DETAILED INSPECTION OF FRAME SPLICES FROMFR.53.7 TO FR.53.9, BETWEEN STR.43 AND STR.44, ONLOWER DECK AFT CARGO STRUCTURE OF LDF, LH/RH.15600 FCOR107400 FH3300 FCOR22900 FHGROUP 46BPOST 49431© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 16RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533852-01-01 197 AB DETAILED INSPECTION OF THE MAIN HOLE RCT FITTINGAREA BETWEEN PUMP HOLE AND MAN HOLE BETWEENFR.53.4 AND FR.53.5.4500 FCOR34500 FH4500 FCOR34500 FHGROUP 45A533852-01-02 197 AB DETAILED INSPECTION OF THE MAIN HOLE RCT FITTINGAREA BETWEEN PUMP HOLE AND MAN HOLE BETWEENFR.53.4 AND FR.53.5.3500 FCOR28500 FH3500 FCOR28500 FHGROUP 45B533860-01-01 734 744753 754DETAILED INSPECTION OF MAIN LONGERON FLANGEBETWEEN FR.51 AND FR.53.1.12800 FCOR97800 FH4200 FCOR32700 FHGROUP 45A533860-01-02 734 744753 754DETAILED INSPECTION OF MAIN LONGERON FLANGEBETWEEN FR.51 AND FR.53.1.12600 FCOR100800 FH3400 FCOR27800 FHGROUP 45B533860-01-03 734 744753 754DETAILED INSPECTION OF MAIN LONGERON FLANGEBETWEEN FR.51 AND FR.53.1.14500 FCOR94600 FH7200 FCOR46800 FHGROUP 46A533860-01-04 734 744753 754DETAILED INSPECTION OF MAIN LONGERON FLANGEBETWEEN FR.51 AND FR.53.1.14400 FCOR99300 FH4100 FCOR28500 FHGROUP 46B533861-01-01 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OFMAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1,LH/RH.14600 FCOR95000 FH4500 FCOR29200 FHGROUP 46A533861-01-02 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OFMAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1,LH/RH.14500 FCOR99700 FH3900 FCOR27000 FHGROUP 46B533861-01-03 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OFMAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1,LH/RH.12800 FCOR98200 FH4100 FCOR31800 FHGROUP 45A533861-01-04 734 744 SPECIAL DETAILED INSPECTION OF INNER FLANGE OFMAIN LONGERON AT JUNCTION WITH FR.48 AND FR.53.1,LH/RH.12600 FCOR101200 FH6400 FCOR51300 FHGROUP 45B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 17RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533862-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF AFT CANTEDLONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.14500 FCOR94800 FH4700 FCOR30600 FHGROUP 46A533862-01-02 734 744753 754SPECIAL DETAILED INSPECTION OF AFT CANTEDLONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.14400 FCOR99200 FH4800 FCOR33200 FHGROUP 46B533862-01-03 734 744753 754SPECIAL DETAILED INSPECTION OF AFT CANTEDLONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.13700 FCOR105200 FH4000 FCOR30600 FHGROUP 45A533862-01-04 735 744753 754SPECIAL DETAILED INSPECTION OF AFT CANTEDLONGERON AT FR.53, AROUND FASTENER HOLES, LH/RH.13500 FCOR108600 FH3500 FCOR28300 FHGROUP 45B533864-01-01 734 744753 754DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAINLONGERON BETWEEN UPPER AND LOWER SHELL FROMFR.53 TO FR.53.2, LH/RH.14400 FCOR93900 FH3700 FCOR24600 FHGROUP 46A533864-01-02 734 744753 754DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAINLONGERON BETWEEN UPPER AND LOWER SHELL FROMFR.53 TO FR.53.2, LH/RH.14000 FCOR96700 FH2400 FCOR16500 FHGROUP 46B533864-01-03 734 744753 754DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAINLONGERON BETWEEN UPPER AND LOWER SHELL FROMFR.53 TO FR.53.2, LH/RH.14000 FCOR107300 FH3600 FCOR27600 FHGROUP 45A533864-01-04 735 744753 754DETAILED INSPECTION OF DOUBLER AND STRAPS ON MAINLONGERON BETWEEN UPPER AND LOWER SHELL FROMFR.53 TO FR.53.2, LH/RH.13900 FCOR111300 FH1600 FCOR12700 FHGROUP 45B533865-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF INTERNAL STRAP ONMAIN LONGERON BETWEEN UPPER AND LOWER SHELL ATFR.53.1, LH/RH.14300 FCOR98900 FH6400 FCOR44400 FHGROUP 46B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 18RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533867-01-01 734 744 DETAILED INSPECTION OF PANEL, CANTED BEAM ANDDOUBLER AT JUNCTION BETWEEN CANTED BEAM, TPROFILE AND X-DOUBLER AT FR.53.2, LH/RH.11800 FCOR76700 FH4600 FCOR30100 FHGROUP 46A533867-01-02 734 744 DETAILED INSPECTION OF PANEL, CANTED BEAM ANDDOUBLER AT JUNCTION BETWEEN CANTED BEAM, TPROFILE AND X-DOUBLER AT FR.53.2, LH/RH.11200 FCOR86000 FH4500 FCOR35000 FHGROUP 45A533868-01-01 INSULATION TO BEDISPLACED, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE, SPLICING OFSTRINGERS 12/13/14/15 AT FR.40.6, LH/RH.14100 FCOR92000 FH1900 FCOR12400 FHGROUP 46APOST 47271533868-01-02 INSULATION TO BEDISPLACED, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE, SPLICING OFSTRINGERS 12/13/14/15 AT FR.40.6, LH/RH.14000 FCOR96800 FH1800 FCOR12900 FHGROUP 46B533869-01-01 N/A SPECIAL DETAILED INSPECTION OF OVER WING EXITEXTERNAL SURROUNDING STRUCTURE, SKIN PANELS ATTWO FIRST ROWS OF DOUBLER FASTENERS, LH/RH.15500 FCOR101100 FH1900 FCOR12500 FHGROUP 46APOST 47270533869-01-02 N/A SPECIAL DETAILED INSPECTION OF OVER WING EXITEXTERNAL SURROUNDING STRUCTURE, SKIN PANELS ATTWO FIRST ROWS OF DOUBLER FASTENERS, LH/RH.15400 FCOR106300 FH1900 FCOR13100 FHGROUP 46B533872-01-01 INSULATION TO BEDISPLACED, LININGS,LAVATORY IF INSTALLEDSPECIAL DETAILED INSPECTION OF OVER WING EXITSURROUNDING STRUCTURE, LOWER STRAPS AT FR.41AAND FR.42A JUNCTION AT STRINGER 26.16400 FCOR106800 FH3500 FCOR23200 FHGROUP 46APOST 47270533873-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF SPLICE BRACKETS ATFR.53.2, AT LEVEL OF UPPER TEE/CENTRAL TEE JUNCTION,LH/RH.7800 FCOR51200 FH3900 FCOR25800 FHA340-600PRE 48487533873-01-02 734 744753 754SPECIAL DETAILED INSPECTION OF SPLICE BRACKETS ATFR.53.2 AT LEVEL OF UPPER TEE/CENTRAL TEE JUNCTION,LH/RH.10300 FCOR67200 FH3900 FCOR25800 FHGROUP 46APOST 48487533874-01-01 N/A SPECIAL DETAILED INSPECTION OF TWO MIDDLEFASTENER ROWS OF BUTTSTRAP, AT CIRCUMFERENTIALJUNCTION AT FR.40.5 FROM STR.11 TO STR.18, LH/RH.11500 FCOR75100 FH1800 FCOR12200 FHGROUP 46APOST 47270PRE 47271© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 19RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533876-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATJUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHTBETWEEN FR.42 AND FR.43 AT STR.1 LH AND STR.1 RH,AND AROUND COLLISION LIGHT CUTOUT.16000 FCOR104500 FH3600 FCOR23400 FHGROUP 46A533876-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATJUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHTBETWEEN FR.42 AND FR.43 AT STR.1 LH AND STR.1 RH,AND AROUND COLLISION LIGHT CUTOUT.15300 FCOR105400 FH3600 FCOR25100 FHGROUP 46BPre 53553533876-02-04 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATJUNCTION WITH DOUBLER OF ANTI-COLLISION LIGHTBETWEEN FR.40.4 AND FR.40.5 AND BETWEEN STR.2 ANDSTR.5, LH/RH.15200 FCOR104400 FH5300 FCOR36600 FHGROUP 46BPost 53553R533877-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF T-PROFILE ATJUNCTION WITH CANTED BEAM & PANEL AT FR.53.2,STR.38, LH/RH.10600 FCOR69400 FH5600FCOR36500 FHA340-600PRE 48487R533877-01-02 734 744753 754SPECIAL DETAILED INSPECTION OF T-PROFILE ATJUNCTION WITH CANTED BEAM & PANEL AT FR.53.2,STR.38, LH/RH.7400 FCOR56500 FH3000 FCOR23000 FHGROUP 45AR533877-01-03 734 744753 754SPECIAL DETAILED INSPECTION OF T-PROFILE ATJUNCTION WITH CANTED BEAM & PANEL AT FR.53.2,STR.38, LH/RH.9800 FCOR63700 FH5200 FCOR33900 FHGROUP 46APOST 48487533878-01-01 734 744753 754DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH YFITTING, EXTERNAL SIDE, AT STR.40/ FR.53.2, LH/RH.11100 FCOR72600 FH5900 FCOR38700 FHA340-600PRE 48487© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 20RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533878-01-02 734 744753 754DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH YFITTING, EXTERNAL SIDE, AT STR.40/ FR 53.2, LH/RH.10200 FCOR66700 FH4100 FCOR27100 FHGROUP 46APOST 48487533878-01-04 734 744753 754DETAILED INSPECTION OF DOUBLER AT JUNCTION WITH YFITTING, EXTERNAL SIDE, AT STR.40/ FR 53.2, LH/RH.11000 FCOR84300 FH3100 FCOR24000 FHGROUP 45A533879-01-01 734 744753 754SPECIAL DETAILED INSPECTION OF TEE PROFILE, ATJUNCTION BETWEEN UPPER TEE/CENTRAL TEE ANDSPLICE BRACKETS, AT FR.53.2, LH/RH.11300 FCOR73900 FH4100 FCOR26600 FHA340-600PRE 48487533879-01-02 734 744753 754SPECIAL DETAILED INSPECTION OF TEE PROFILE, ATJUNCTION BETWEEN UPPER TEE/CENTRAL TEE ANDSPLICE BRACKETS, AT FR.53.2, LH/RH.12500 FCOR81300 FH4100 FCOR26600 FHGROUP 46APOST 48487533880-01-01 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWERFITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.7700 FCOR50000 FH7700 FCOR50000 FHGROUP 46A533880-01-02 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWERFITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.7600 FCOR52700 FH7600 FCOR52700 FHGROUP 46B533880-01-03 734 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWERFITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.7300 FCOR56200 FH7300 FCOR56200 FHGROUP 45A533880-01-04 735 744 DETAILED INSPECTION OF RADIUS OF KEEL BEAM LOWERFITTING AT JUNCTION WITH Y FITTING AT FR.53.2, LH/RH.7300 FCOR58600 FH7300 FCOR58600 FHGROUP 45B533884-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE - FR.41A AT STR.16AND STR27 AND FR.42A STR27 INNER FLANGES ATJUNCTION WITH STRAPS, LH/RH.15500 FCOR101000 FH2700 FCOR17800 FHGROUP 46APOST 47270PRE 48475© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 21RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533884-02-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE - FR.41A AT STR.16INNER FLANGES AT JUNCTION WITH STRAPS, LH/RH.15500 FCOR101000 FH3700 FCOR24000 FHGROUP 46APOST 47270POST 48475533885-01-01 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE, INNER FLANGE OFBEAMS STR.14 AND STR.15A, AT JUNCTION WITH STRAPS,AT FR.41A, LH/RH.10700 FCOR69800 FH1500 FCOR9800 FHGROUP 46APOST 47270533885-01-02 INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITINTERNAL SURROUNDING STRUCTURE, INNER FLANGE OFBEAMS STR.14 AND STR.15A, AT JUNCTION WITH STRAPS,AT FR.41A, LH/RH.14600 FCOR100600 FH1500 FCOR10500 FHGROUP 46B533886-01-01 N/A DETAILED INSPECTION OF OVER WING EXIT EXTERNALSURROUNDING STRUCTURE, SKIN PANELS AT CUTOUTCORNERS, LH/RH.16200 FCOR105900 FH3600 FCOR23700 FHGROUP 46APOST 47270533886-01-02 N/A DETAILED INSPECTION OF OVER WING EXIT EXTERNALSURROUNDING STRUCTURE, SKIN PANELS AT CUTOUTCORNERS, LH/RH.15100 FCOR104100 FH3700 FCOR25400 FHGROUP 46B533889-01-01 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.40.3 TO FR.40.6 AND FROMSTR.18 TO STR.22, LH/RH.14500 FCOR94500 FH3900 FCOR25500 FHGROUP 46A533889-01-03 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.40.3 TO FR.40.6 AND FROMSTR.18 TO STR.22, LH/RH.14300 FCOR98700 FH2800 FCOR19300 FHGROUP 46B533889-02-02 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.41 TO FR.44 AND FROM STR.18TO STR.22, LH/RH.16000 FCOR122400 FH5900 FCOR45700 FHGROUP 45A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 22RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533889-02-04 SEAL DISPLACED SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.41 TO FR.44 AND FROM STR.18TO STR.22, LH/RH.16000 FCOR128300 FH3500 FCOR28300 FHGROUP 45B533892-01-01 822,FLOOR PANELS, ANDINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASKSPECIAL DETAILED INSPECTION OF THE FOOT FRAMES /UPPER LATERAL FRAMES SPLICINGS FROM FRAME 53.3 TO53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) ABOVE RCT.11600 FCOR89000 FH3000 FCOR23300 FHGROUP 45A533892-01-02 822,FLOOR PANELS, ANDINSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASKSPECIAL DETAILED INSPECTION OF THE FOOT FRAMES /UPPER LATERAL FRAMES SPLICINGS FROM FRAME 53.3 TO53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT) ABOVE RCT.11400 FCOR91900 FH3300 FCOR26700 FHGROUP 45B533893-01-01 FLOOR PANELS,INSULATION TO BEDISPLACED AS REQUIREDDETAILED INSPECTION OF RCT AT LATERAL PANEL FROMFRAME 53.2 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT)UP TO STRINGER 33, LH/RH.15300 FCOR116700 FH3900 FCOR29800 FHGROUP 45A533893-01-02 FLOOR PANELS,INSULATION TO BEDISPLACED AS REQUIREDDETAILED INSPECTION OF RCT AT LATERAL PANEL FROMFRAME 53.2 TO 53.7 (5 FRAME RCT) OR 53.9 (7 FRAME RCT)UP TO STRINGER 33, LH/RH.15200 FCOR121800 FH3300 FCOR26500 FHGROUP 45B533894-01-01 197CB 153AZ DETAILED INSPECTION OF RCT AT INTERNAL FOOT FRAME/ LATERAL FRAME SPLICING FROM FRAMES 53.3 TO 53.6 (5FRAME RCT) OR FRAMES 53.3 TO 53.8 (7 FRAME RCT).12500 FCOR95300 FH4600 FCOR35400 FHGROUP 45A533894-01-02 197CB 153AZ DETAILED INSPECTION OF RCT AT INTERNAL FOOT FRAME/ LATERAL FRAME SPLICING FROM FRAMES 53.3 TO 53.6 (5FRAME RCT) OR FRAMES 53.3 TO 53.8 (7 FRAME RCT).12000 FCOR96300 FH5000 FCOR40200 FHGROUP 45B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 23RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533897-01-01 197CB 153AZ SPECIAL DETAILED INSPECTION OF THE FRAME SPLICESAND LATERAL FRAMES FROM FR.53.3 TO FR.53.6 (ONRCT5), OR TO FR.53.8 (ON RCT7).14600 FCOR112000 FH4400 FCOR34000 FHGROUP 45A533897-01-02 197CB 153AZ SPECIAL DETAILED INSPECTION OF THE FRAME SPLICESAND LATERAL FRAMES FROM FR.53.3 TO FR.53.6 (ONRCT5), OR TO FR.53.8 (ON RCT7).15300 FCOR122500 FH4500 FCOR36300 FHGROUP 45B533898-01-01 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TOSTR22, LH/RH.8700 FCOR57100 FH1100 FCOR7600 FHGROUP 46APRE 52169533898-01-02 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.47 TO FR.53.1 AND FROM STR.18TO STR.22, LH/RH.8700 FCOR57100 FH2200 FCOR14800 FHGROUP 46APOST 52169533898-01-03 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TOSTR22, LH/RH.9400 FCOR64600 FH2600 FCOR17900 FHGROUP 46B533898-01-04 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TOSTR22, LH/RH.12400 FCOR95100 FH3100 FCOR24000 FHGROUP 45A533898-01-05 N/A SPECIAL DETAILED INSPECTION OF SKIN PANEL ANDWINDOW FRAME FROM FR.47 TO FR.53.1 FROM STR18 TOSTR22, LH/RH.14800 FCOR118500 FH2700 FCOR21800 FHGROUP 45B533899-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF WINDOW FRAME AT JUNCTIONWITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEENSTR.18 AND STR.22, INTERNAL SIDE, LH/RH.9300 FCOR60500 FH2500 FCOR16400 FHGROUP 46A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 24RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533899-01-02 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF WINDOW FRAME AT JUNCTIONWITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEENSTR.18 AND STR.22, INTERNAL SIDE, LH/RH.9000 FCOR62200 FH2400 FCOR16900 FHGROUP 46B533899-01-03 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF WINDOW FRAME AT JUNCTIONWITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEENSTR.18 AND STR.22, INTERNAL SIDE, LH/RH.10100 FCOR77600 FH2400 FCOR18700 FHGROUP 45A533899-01-04 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF WINDOW FRAME AT JUNCTIONWITH SKIN PANEL FROM FR.47 TO FR.53.1, BETWEENSTR.18 AND STR.22, INTERNAL SIDE, LH/RH.9900 FCOR79400 FH2400 FCOR19300 FHGROUP 45B533901-01-01 734 744 SPECIAL DETAILED INSPECTION OF EXTERNAL SKIN PANELAROUND ALL FASTENERS AT JUNCTION WITH CANTEDBEAM, AT FR.53.2, LH/RH.11800 FCOR81400 FH8100 FCOR55800 FHGROUP 46B533901-01-02 734 744 SPECIAL DETAILED INSPECTION OF EXTERNAL SKIN PANELAROUND ALL FASTENERS AT JUNCTION WITH CANTEDBEAM, AT FR.53.2, LH/RH.10400 FCOR83300 FH6800 FCOR54700 FHGROUP 45B533902-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITSURROUNDING STRUCTURE, AT FR.41A AND FR.42A,BETWEEN STR.23 AND STR.26, LH/RH.14500 FCOR94800 FH5300 FCOR34700 FHGROUP 46APOST 48487© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 25RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533902-01-02 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF OVER WING EXITSURROUNDING STRUCTURE, AT FR.41A AND FR.42A,BETWEEN STR.23 AND STR.26, LH/RH.16300 FCOR112600 FH4500 FCOR30900 FHGROUP 46B533903-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSSPECIAL DETAILED INSPECTION OF CIRCUMFERENTIALJUNCTION AT FR.40.5, STRINGERS AND SPLICES AROUNDFASTENER HOLES BETWEEN STR.11 AND STR.18, LH/RH.11700 FCOR76500 FH1800 FCOR12200 FHGROUP 46APOST 47270PRE 47271533904-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDGENERAL VISUAL INSPECTION OF FRAMES AT JUNCTIONWITH FLOOR CROSSBEAMS AT FR.38.1 AND FR.39, LH/RH.14700 FCOR96100 FH4200 FCOR27300 FHGROUP 46A533905-01-01 734 744 DETAILED INSPECTION OF CANTED BEAM AT JUNCTIONWITH SKIN PANEL AT FR.53.2, LH/RH.14400 FCOR99100 FH3800 FCOR26300 FHGROUP 46B533905-01-02 734 744 DETAILED INSPECTION OF CANTED BEAM AT JUNCTIONWITH SKIN PANEL AT FR.53.2, LH/RH.12800 FCOR103100 FH3500 FCOR28100 FHGROUP 45B533906-01-01 734 744753 754DETAILED INSPECTION OF LANDING GEAR BAY UPPERPRESSURE PANELS, LOWER FACE, BETWEEN FR.47 ANDFR.53.3600 FCOR23600 FH3600 FCOR23600 FHGROUP 46A533906-01-02 734 744753 754DETAILED INSPECTION OF LANDING GEAR BAY UPPERPRESSURE PANELS, LOWER FACE, BETWEEN FR.47 ANDFR.53.3500 FCOR24200 FH3500 FCOR24200 FHGROUP 46B533906-01-03 734 744753 754DETAILED INSPECTION OF LANDING GEAR BAY UPPERPRESSURE PANELS, LOWER FACE, BETWEEN FR.47 ANDFR.53.4100 FCOR31900 FH4100 FCOR31900 FHGROUP 45A533906-01-04 734 744753 754DETAILED INSPECTION OF LANDING GEAR BAY UPPERPRESSURE PANELS, LOWER FACE, BETWEEN FR.47 ANDFR.53.5600 FCOR45500 FH5600 FCOR45500 FHGROUP 45B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 26RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533907-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGE MEMBRANESAROUND FIVE FASTENER HOLES BETWEEN FR.48 ANDFR.49, AT Y-1456 AND Y+1456.7830 FCOR50900 FH2370 FCOR15400 FHGROUP 46APRE 53575PRE 57290D533907-01-02 TASK DELETED IN ISSUE 11R533907-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGE MEMBRANESAROUND FIVE FASTENER HOLES BETWEEN FR.48 ANDFR.49, AT Y-1456 AND Y+1456.9090 FCOR69300 FH2580 FCOR19600 FHGROUP 45APRE 53575PRE 57290D533907-01-04 TASK DELETED IN ISSUE 11533908-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGERS 22 AND 23 ANDSTRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.8900 FCOR58000 FH3300 FCOR21500 FHGROUP 46A533908-01-02 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGERS 22 AND 23 ANDSTRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.8700 FCOR60100 FH3200 FCOR22200 FHGROUP 46B533908-01-03 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGERS 22 AND 23 ANDSTRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.9700 FCOR74300 FH3400 FCOR26500 FHGROUP 45A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 27RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533908-01-04 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF STRINGERS 22 AND 23 ANDSTRINGER COUPLINGS, FWD AND AFT OF FR.47, LH/RH.9500 FCOR76100 FH3300 FCOR27100 FHGROUP 45B533909-01-01 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.13900 FCOR90300 FH3600 FCOR23600 FHGROUP 46A533909-01-02 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.13700 FCOR94500 FH3600 FCOR24800 FHGROUP 46B533909-01-03 N/A DETAILED INSPECTION OF EXTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.15400 FCOR123800 FH2000 FCOR16500 FHGROUP 45B533910-01-01 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF INTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.13800 FCOR90300 FH3600 FCOR23600 FHGROUP 46A533910-01-02 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF INTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.13700 FCOR94500 FH3600 FCOR24800 FHGROUP 46B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 28RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340533910-01-03 834INSULATION TO BEDISPLACED AS REQUIREDTO COMPLETE THEREQUIRED MAINTENANCETASK, LININGSDETAILED INSPECTION OF INTERNAL SKIN PANEL ATLONGITUDINAL JUNCTION AT STR.11 FROM FR.38 TO FR.54,LH/RH.15400 FCOR123800 FH2000 FCOR16500 FHGROUP 45B533911-01-01 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEAR BAYUPPER PRESSURE PANEL, LOWER SURFACE, BETWEENFR.53 AND FR.53.2.4900 FCOR32200 FH4900 FCOR32200 FHGROUP 46A533911-01-02 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEAR BAYUPPER PRESSURE PANEL, LOWER SURFACE, BETWEENFR.53 AND FR.53.2.4600 FCOR31900 FH4600 FCOR31900 FHGROUP 46B533911-01-03 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEAR BAYUPPER PRESSURE PANEL, LOWER SURFACE, BETWEENFR.53 AND FR.53.2.3300 FCOR25800 FH3300 FCOR25800 FHGROUP 45A533911-01-04 734 744753 754DETAILED INSPECTION OF CENTER LANDING GEAR BAYUPPER PRESSURE PANEL, LOWER SURFACE, BETWEENFR.53 AND FR.53.2.4200 FCOR33600 FH4200 FCOR33600 FHGROUP 45B533912-01-01 831CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATIONDETAILED INSPECTION OF STRINGERS AND SPLICESAROUND FASTENERS ON FLANGES AND WEBS, BETWEENFR.40.3 AND FR.40.6 AND BETWEEN STR.3 AND STR.4,AROUND ANTICOLLISION LIGHTS, LH/RH.16000 FCOR110000 FH3100 FCOR21800 FHGROUP 46BPOST 53553533914-01-01 834INSULATION, LININGSSPECIAL DETAILED INSPECTION OF STRINGER 12 ATJUNCTION WITH FRAME 43, LH/RH.6900 FCOR45000 FH2800 FCOR18600 FHGROUP 46A533914-01-02 834INSULATION, LININGSSPECIAL DETAILED INSPECTION OF STRINGER 12 ATJUNCTION WITH FRAME 43, LH/RH.7000 FCOR48400 FH3100 FCOR21400 FHGROUP 46B533915-01-01 N/A GENERAL VISUAL INSPECTION OF EXTERNAL SKIN PANELBETWEEN FR.53 AND FR.54, FROM STR.1 TO STR.11, LH/RH.5600 FCOR38900 FH2600 FCOR17900 FHGROUP 46BPOST 54787© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 29RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R533916-01-01 834INSULATION, LININGSCEILING PANELS,OVERHEADSTOWAGE BINS,INSULATIONDETAILED INSPECTION OF INTERNAL SKIN PANEL AROUNDCBB ANTENNAS, SUPPORT FITTINGS AND JUNCTION WITHDOUBLERS BETWEEN FR.53 AND FR.54, FROM STR.1 TOSTR.11, LH/RH.12100 FCOR83800 FH3200 FCOR22200 FHGROUP 46BPOST 54787534205-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGERCOUPLING AREAS AT FR.72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.8900 FCOR74100 FH6300 FCOR52500 FHGROUP 45AORGROUP 46A534205-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGERCOUPLING AREAS AT FR.72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.10000 FCOR88000 FH7000 FCOR61500 FHGROUP 45BORGROUP 46B534207-01-01 833/843CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR.72, FROM STR.3 TOSTR.7 AND STR.11 TO STR.13, WHERE LAP JOINTSINTERSECT WITH CIRCUMFERENTIAL SKIN SPLICE, LH/RH.8900 FCOR74100 FH6300 FCOR52500 FHGROUP 45AORGROUP 46A534207-01-02 833/843CEILING PANELS,OVERHEADSTOWAGE BINS,INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR.72, FROM STR.3 TOSTR.7 AND STR.11 TO STR.13, WHERE LAP JOINTSINTERSECT WITH CIRCUMFERENTIAL SKIN SPLICE, LH/RH.10000 FCOR88000 FH7000 FCOR61500 FHGROUP 45BORGROUP 46B534208-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE IN CIRCUMFERENTIAL SPLICE AND STRINGERCOUPLING AREAS AT FR.78 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.10200 FCOR69500 FH8000 FCOR54500 FHGROUP 45BORGROUP 46B534220-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGING BETWEEN FR.54 AND FR.73AND BETWEEN STR.18 AND STR.22 LH/RH, EXTERNALSURFACE.12700 FCOR91700 FH4300 FCOR31000 FHGROUP 45AORGROUP 46A534220-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGING BETWEEN FR.54 AND FR.73AND BETWEEN STR.18 AND STR.22 LH/RH, EXTERNALSURFACE.8000 FCOR56000 FH4300 FCOR30100 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 30RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340R534224-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR.54 AND FR.80 FROMSTR.6 TO STR.26 , LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534224-02-02.11000 FC 2200 FC A340-500ORA340-600N534224-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR.54 AND FR.80 FROM STR.6 TOSTR.26.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534224-01-02.11000 FC 6900 FC A340-500ORA340-600R534226-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR.54 AND FR.80 FROMSTR.26 LH/RH TO BOTTOM CENTER LINE, INCLUDING SKINSPLICES AND LAP JOINTS AND INCLUDING THE LOWER,UNCOVERED AREA OF SKIN AFT OF THE BELLY FAIRINGAND FORWARD OF FR.54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534226-02-02.2200 FC2200 FC A340-500ORA340-600N534226-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR.54 AND FR.80 FROM STR.26 LH/RHTO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES ANDLAP JOINTS AND INCLUDING THE LOWER, UNCOVEREDAREA OF SKIN AFT OF THE BELLY FAIRING AND FORWARDOF FR.54.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534226-01-02.6900 FC 6900 FC A340-500ORA340-600534231-01-01 833 843 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 4 (AFT PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS, LH/RH.11500 FC 7000 FC A340-500ORA340-600534232-02-01 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE LH/RH.11500 FC 7000 FC A340-500ORA340-600© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 31RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340534239-01-02 822 GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR.59A AND FR.65).3500 FC 3500 FC A340-500ORA340-600534246-01-02 823 GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGSOF BULK CARGO COMPARTMENT DOOR, AT 10 POSITIONSAT FR 67 AND FR 69.10000 FC 10000 FC A340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288534249-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR.67 AND FR.69).3500 FC 3500 FC A340-500PRE 49205PRE 49288ORA340-600PRE 49205PRE 49288534271-01-01 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/ PASSENGER/CREW DOOR) CUTOUT UPPER CORNERS, LH/RH.10700 FCOR101300 FH6500 FCOR61500 FHA340-600534272-02-01 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.10700 FCOR101300 FH6500 FCOR61500 FHA340-600534273-01-01 833 843CEILING PANELSOVERHEAD STOWAGEBINS INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR.78, FROM STR.5 TOSTR.7, WHERE LAP JOINTS INTERSECT WITHCIRCUMFERENTIAL SKIN SPLICE, LH/RH.10200 FCOR69500 FH8000 FCOR54500 FHGROUP 45BORGROUP 46B534274-01-01 834 844LINING, INSULATIONDETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,FLANGE OF LATERAL FRAMES, FR 56.1 AND 56.3A AT BEAMT1, T2, T7 AMD T8, LH/RH.7400 FC 3000 FC GROUP 46APRE 47374534275-01-01 833 843LINING, INSULATIONDETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, FLANGE OF LATERALFRAMES, FR 73A AND 75A AT BEAM T1, T2, T7 AND T8,LH/RH.7400 FC 3000 FC GROUP 46APRE 47374© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 32RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N 534277-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR 54 AND 80 FROM STR6 LH/RH TO CROWNCENTER LINE EXCLUDING AREA UNDER VERTICALSTABILIZER FAIRING, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534277-02-01.4500 FC 4500 FC A340-500ORA340-600N 534277-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR54 AND 80 FROM STR6 LH/RH TO CROWN CENTER LINEEXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING,EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534277-01-01.6900 FC 6900 FC A340-500ORA340-600535213-01-01 312AR DETAILED INSPECTION OF SKIN, INNER DOUBLER ANDEDGE BEAM AT LOWER HORIZONTAL TAILPLANE CUT-OUTAT FR.87 BETWEEN STR.26 AND STR.27, LH/RH.12000 FCOR78000 FH6500 FCOR42000 FHGROUP 46B535213-01-02 312AR DETAILED INSPECTION OF SKIN, INNER DOUBLER ANDEDGE BEAM AT LOWER HORIZONTAL TAILPLANE CUT-OUTAT FR.87 BETWEEN STR.26 AND STR.27, LH/RH.12000 FCOR66000 FH6500 FCOR35700 FHGROUP 45B545721-01-02 415AL 416AR425AL 426AR435AL 436AR445AL 446ARDETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 -F4, LH/RH.5000 FCOR32500 FH5000 FCOR32500 FHGROUP 46A545721-01-03 415AL 416AR425AL 426AR435AL 436AR445AL 446ARDETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 -F4, LH/RH.5000 FCOR34300 FH5000 FCOR30000 FHGROUP 46B545721-01-04 415AL 416AR425AL 426AR435AL 436AR445AL 446ARDETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 -F4, LH/RH.5000 FCOR38100 FH5000 FCOR30000 FHGROUP 45A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 33RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545721-01-05 415AL 416AR425AL 426AR435AL 436AR445AL 446ARDETAILED INSPECTION OF PYLON, FAN COWL FITTINGS F3 -F4, LH/RH.5000 FCOR40000 FH5000 FCOR30000 FHGROUP 45B545725-01-02 425AL 426AR427AL 428AR435AL 436AR437AL 438ARDETAILED INSPECTION OF PYLON THRUST REVERSERFITTINGS, R3- R4, LH/RH.3500 FCOR23000 FH3500 FCOR23000 FHGROUP 46A545725-01-03 425AL 426AR427AL 428AR435AL 436AR437AL 438ARDETAILED INSPECTION OF PYLON THRUST REVERSERFITTINGS, R3- R4, LH/RH.3600 FCOR24900 FH3600 FCOR24900 FHGROUP 46B545725-01-04 425AL 426AR427AL 428AR435AL 436AR437AL 438ARDETAILED INSPECTION OF PYLON THRUST REVERSERFITTINGS, R3- R4, LH/RH.3000 FCOR23400 FH3000 FCOR23400 FHGROUP 45A545725-01-05 425AL 426AR427AL 428AR435AL 436AR437AL 438ARDETAILED INSPECTION OF PYLON THRUST REVERSERFITTINGS, R3- R4, LH/RH.3200 FCOR26000 FH3200 FCOR26000 FHGROUP 45B545801-02-01 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OFLOWER ARMS AT ENGINE FORWARD MOUNT FITTING,SPIGOT HOLE LOCATION.7100 FCOR46200 FH7100 FCOR46200 FHGROUP 46A545801-02-02 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OFLOWER ARMS AT ENGINE FORWARD MOUNT FITTING,SPIGOT HOLE LOCATION.8000 FCOR55000 FH8000 FCOR55000 FHGROUP 46B545801-02-03 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OFLOWER ARMS AT ENGINE FORWARD MOUNT FITTING,SPIGOT HOLE LOCATION.6700 FCOR51000 FH6700 FCOR51000 FHGROUP 45A545801-02-04 ENGINE DETAILED INSPECTION OF PYLON PYRAMID END OFLOWER ARMS AT ENGINE FORWARD MOUNT FITTING,SPIGOT HOLE LOCATION.8000 FCOR64000 FH8000 FCOR64000 FHGROUP 45B545802-01-02 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINEATTACHMENT BEAM MATING FACE WITH THE ENGINE AFTMOUNT FITTING.5000 FCOR32500 FH5000 FCOR32500 FHGROUP 46A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 34RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545802-01-03 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINEATTACHMENT BEAM MATING FACE WITH THE ENGINE AFTMOUNT FITTING.5000 FCOR34300 FH5000 FCOR34300 FHGROUP 46B545802-01-04 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINEATTACHMENT BEAM MATING FACE WITH THE ENGINE AFTMOUNT FITTING.5000 FCOR38100 FH5000 FCOR38100 FHGROUP 45A545802-01-05 ENGINE DETAILED INSPECTION OF PYLON, AFT ENGINEATTACHMENT BEAM MATING FACE WITH THE ENGINE AFTMOUNT FITTING.5000 FCOR40000 FH5000 FCOR40000 FHGROUP 45B545804-01-01 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARSPECIAL DETAILED INSPECTION OF PYLON, ON THEPYRAMID END OF LOWER ARMS AFT RIB 1.8000 FCOR52000 FH4000 FCOR26000 FHGROUP 46A545804-01-02 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARSPECIAL DETAILED INSPECTION OF PYLON, ON THEPYRAMID END OF LOWER ARMS AFT RIB 1.8000 FCOR55000 FH4000 FCOR27500 FHGROUP 46B545804-01-03 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARSPECIAL DETAILED INSPECTION OF PYLON, ON THEPYRAMID END OF LOWER ARMS AFT RIB 1.8000 FCOR61000 FH4000 FCOR30500 FHGROUP 45A© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 35RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545804-01-04 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARSPECIAL DETAILED INSPECTION OF PYLON, ON THEPYRAMID END OF LOWER ARMS AFT RIB 1.8000 FCOR64000 FH4000 FCOR32000 FHGROUP 45B545810-01-02 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARDETAILED INSPECTION OF PYLON, ENGINE AFTATTACHMENT BEAM AT RIB 6.5000 FCOR32500 FH5000 FCOR32500 FHGROUP 46A545810-01-03 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARDETAILED INSPECTION OF PYLON, ENGINE AFTATTACHMENT BEAM AT RIB 6.5000 FCOR34300 FH5000 FCOR34300 FHGROUP 46B545810-01-04 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARDETAILED INSPECTION OF PYLON, ENGINE AFTATTACHMENT BEAM AT RIB 6.5000 FCOR38100 FH5000 FCOR38100 FHGROUP 45A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 36RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545810-01-05 415AL 416AR417AL 418AR425AL 426AR427AL 428AR435AL 436AR437AL 438AR445AL 446AR447AL 448ARDETAILED INSPECTION OF PYLON, ENGINE AFTATTACHMENT BEAM AT RIB 6.5000 FCOR40000 FH5000 FCOR40000 FHGROUP 45B545813-01-01 452CR 452GR 452EL462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLYDETAILED INSPECTION OF THE FORWARD PYLON TO WINGATTACHMENT AT RIB 8.8000 FCOR52000 FH4000 FCOR26000 FHGROUP 46A545813-01-02 452CR 452GR 452EL462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLYDETAILED INSPECTION OF THE FORWARD PYLON TO WINGATTACHMENT AT RIB 8.8000 FCOR55000 FH4000 FCOR27500 FHGROUP 46B545813-01-03 452CR 452GR 452EL462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLYDETAILED INSPECTION OF THE FORWARD PYLON TO WINGATTACHMENT AT RIB 8.8000 FCOR61000 FH4000 FCOR30500 FHGROUP 45A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 37RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545813-01-04 452CR 452GR 452EL462CR 462GR 462JL 462EL472CR 472GR 472JL 472EL482CR 482GR 482ELENGINESHACKLES DISASSEMBLYDETAILED INSPECTION OF THE FORWARD PYLON TO WINGATTACHMENT AT RIB 8.8000 FCOR64000 FH4000 FCOR32000 FHGROUP 45B545814-01-01 454AL 454AR 454BL 454BR464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BRDETAILED INSPECTION OF THE AFT PYLON TO WINGATTACHMENT AT RIB 14.8000 FCOR52000 FH4000 FCOR26000 FHGROUP 46A545814-01-02 454AL 454AR 454BL 454BR464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BRDETAILED INSPECTION OF THE AFT PYLON TO WINGATTACHMENT AT RIB 14.8000 FCOR55000 FH4000 FCOR27500 FHGROUP 46B545814-01-03 454AL 454AR 454BL 454BR464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BRDETAILED INSPECTION OF THE AFT PYLON TO WINGATTACHMENT AT RIB 14.8000 FCOR61000 FH4000 FCOR30500 FHGROUP 45A© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 38RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340545814-01-04 454AL 454AR 454BL 454BR464AR 464BL 464BR 464CL474AL 474BL 474BR 474CR484AL 484AR 484BL 484BRDETAILED INSPECTION OF THE AFT PYLON TO WINGATTACHMENT AT RIB 14.8000 FCOR64000 FH4000 FCOR32000 FHGROUP 45B545842-01-01 453CL 453CR463CL 463CR473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUT AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.6100 FCOR46500 FH6100 FCOR46500 FHGROUP 45A545842-01-02 453CL 453CR463CL 463CR473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUT AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.6000 FCOR39500 FH6000 FCOR39500 FHGROUP 46A545842-01-03 453CL 453CR463CL 463CR473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUT AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.6400 FCOR44100 FH6400 FCOR44100 FHGROUP 46B545842-01-04 453CL 453CR463CL 463CR473CL 473CR483CL 483CRDETAILED INSPECTION OF PYLON LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUT AND MATING SURFACEBETWEEN RIB 9 AND RIB 10.6300 FCOR50400 FH6300 FCOR50400 FHGROUP 45BR571801-01-01 147AZ 148AZ734 744DETAILED INSPECTION OF CENTER WING BOX, LOWERSKIN PANEL UPPER FACE AROUND HYDRAULIC HOLESBETWEEN STIFFENER 34 AND STIFFENER 35 ANDBETWEEN Y-953 AND Y-1959.13400 FCOR92100 FH2700 FCOR19000 FHGROUP 46B571802-01-01 191FB 192FB 192JB192NB 195JB 195NBSPECIAL DETAILED INSPECTION OF TEE BACKING PLATESAROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEENFR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.12600 FCOR82500 FH8500 FCOR55200 FHGROUP 46APRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 39RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571802-01-02 191FB 192FB 192JB192NB 195JB 195NBSPECIAL DETAILED INSPECTION OF TEE BACKING PLATESAROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEENFR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.11500 FCOR79600 FH5900 FCOR41100 FHGROUP 46B571802-01-03 191FB 192FB 192JB192NB 195JB 195NBSPECIAL DETAILED INSPECTION OF TEE BACKING PLATESAROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEENFR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.13500 FCOR88300 FH8300 FCOR54100 FHGROUP 46APOST 48487571802-01-04 191FB 192FB 192JB192NB 195JB 195NBSPECIAL DETAILED INSPECTION OF TEE BACKING PLATESAROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEENFR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.12900 FCOR98400 FH8000 FCOR61600 FHA340-500PRE 48487571802-01-05 191FB 192FB 192JB192NB 195JB 195NBSPECIAL DETAILED INSPECTION OF TEE BACKING PLATESAROUND FIRST ROWS OF FASTENERS AT RIB 1 BETWEENFR.40 AND FR.47, ON WING SIDE AND CWB SIDE, LH/RH.13800 FCOR105300 FH7900 FCOR60300 FHGROUP 45APOST 48487571803-01-01 CABIN FLOOR PANELS,INSULATION, LININGS,GALLEYS AND TOILETS IFFITTEDDETAILED INSPECTION OF CENTER WING BOX BEAM RADIION BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LHSIDE BETWEEN FR.46 AND FR.47.6600 FCOR43000 FH1800 FCOR11700 FHGROUP 46A571803-01-02 CABIN FLOOR PANELS,INSULATION, LININGS,GALLEYS AND TOILETS IFFITTEDDETAILED INSPECTION OF CENTER WING BOX BEAM RADIION BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LHSIDE BETWEEN FR.46 AND FR.47.6400 FCOR44100 FH1700 FCOR12100 FHGROUP 46B571803-01-03 CABIN FLOOR PANELS,INSULATION, LININGS,GALLEYS AND TOILETS IFFITTEDDETAILED INSPECTION OF CENTER WING BOX BEAM RADIION BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LHSIDE BETWEEN FR.46 AND FR.47.6000 FCOR45900 FH1700 FCOR13100 FHGROUP 45A571803-01-04 CABIN FLOOR PANELS,INSULATION, LININGS,GALLEYS AND TOILETS IFFITTEDDETAILED INSPECTION OF CENTER WING BOX BEAM RADIION BOTH SIDE OF BEAM VERTICAL WEB FROM RH TO LHSIDE BETWEEN FR.46 AND FR.47.6000 FCOR46800 FH1600 FCOR13500 FHGROUP 45B571804-01-01 191 BT192 BT,CT195 CTSPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING,FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEENSTIFFENERS 19 AND 21, LH/RH.11700 FCOR76400 FH3700 FCOR24100 FHA340-600PRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 40RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571804-01-02 191 BT192 BT,CT195 CTSPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING,FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEENSTIFFENERS 19 AND 21, LH/RH.11700 FCOR76400 FH3900 FCOR25500 FHGROUP 46APOST 48487571804-01-03 191 BT192 BT,CT195 CTSPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING,FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEENSTIFFENERS 19 AND 21, LH/RH.10100 FCOR69400 FH3400 FCOR23300 FHGROUP 46B571804-01-04 191 BT192 BT,CT195 CTSPECIAL DETAILED INSPECTION OF CRUCIFORM FITTING,FIRST ROW OF FASTENERS AT RIB 1, WING SIDE BETWEENSTIFFENERS 19 AND 21, LH/RH.12100 FCOR97300 FH4000 FCOR32400 FHGROUP 45B571808-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE", LOWER SKIN PANEL AT JUNCTION WITHL- FLANGE AROUND FASTENER HOLES BETWEEN Y1959AND RIB 1, LH/RH.9200 FCOR60200 FH4100 FCOR26800 FHGROUP 46A571808-01-02 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE", LOWER SKIN PANEL AT JUNCTION WITHL- FLANGE AROUND FASTENER HOLES BETWEEN Y1959AND RIB 1, LH/RH.13800 FCOR94900 FH3900 FCOR27000 FHGROUP 46B571808-01-03 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE" , LOWER SKIN PANEL AT JUNCTION WITHL- FLANGE AROUND FASTENERS HOLES, BETWEEN Y1959AND RIB 1, LH/RH.10300 FCOR78600 FH4000 FCOR30700 FHGROUP 45A571808-01-04 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE" , LOWER SKIN PANEL AT JUNCTION WITHL- FLANGE AROUND FASTENERS HOLES, BETWEEN Y1959AND RIB 1, LH/RH.15500 FCOR124100 FH3800 FCOR30700 FHGROUP 45B571809-01-01 147AZ 148AZ734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWERSKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959AND LOWER CORNER FITTING LH/RH.15600 FCOR93600 FH4000 FCOR24000 FHGROUP 46A571809-01-02 147AZ 148AZ734 744SPECIAL DETAILED INSPECTION OFCENTER WING BOX,FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWERSKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959AND LOWER CORNER FITTING, LH/RH.15600 FCOR107200 FH4000 FCOR27500 FHGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 41RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571809-01-03 147AZ 148AZ734 744SPECIAL DETAILED INSPECTION OFCENTER WING BOX,FRAME 40 "NODE", L- FLANGE AT JUNCTION WITH LOWERSKIN PANEL AROUND FASTENERS HOLES, BETWEEN Y1959AND LOWER CORNER FITTING, LH/RH.8000 FCOR48000 FH4000 FCOR24000 FHA340-500R571811-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTIONWITH CENTER WING BOX LOWER PANEL, LH/RH.7400 FCOR48500 FH2100 FCOR14200 FHGROUP 46AR571811-01-02 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTIONWITH CENTER WING BOX LOWER PANEL, LH/RH.7300 FCOR56200 FH2100 FCOR16300 FHGROUP 45AR571811-01-03 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTIONWITH CENTER WING BOX LOWER PANEL, LH/RH.7400 FCOR51100 FH3200 FCOR22000 FHGROUP 46BR571811-01-05 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF X-DOUBLER AT FR.40AND FR.40.1, AND Y-DOUBLER AT FR.40 AT JUNCTIONWITH CENTER WING BOX LOWER PANEL, LH/RH.14800 FCOR118500 FH3000 FCOR24000 FHGROUP 45B571812-01-01 192CB 193AB 191AB SPECIAL DETAILED INSPECTION OF CENTER WING BOX,FRAME 40 "NODE", CIRCUMFERENTIAL JUNCTION,STR.35/36 AREA, OUTSIDE LOWER SHELL.8000 FCOR48000 FH4000 FCOR24000 FHA340-500571813-01-01 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH.11100 FCOR72500 FH3000 FCOR19900 FHA340-600PRE 48487571813-01-02 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH.11300 FCOR73600 FH2900 FCOR19400 FHGROUP 46APOST 48487571813-01-04 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH.10400 FCOR79400 FH2900 FCOR22500 FHA340-500PRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 42RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571813-01-05 192CB 193AB 191AB DETAILED INSPECTION OF CENTER WING BOX, FRAME 40"NODE", Y DOUBLER AROUND FASTENER HOLES AT FR.40BETWEEN STR.39 AND STR41, EXTERNAL SIDE, LH/RH.10500 FCOR80600 FH2800 FCOR21800 FHGROUP 45APOST 48487R571815-01-01 FLOOR PANELSGALLEY OR LAVATORY IFINSTALLED734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL, AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.8730 FCOR56700 FH5150 FCOR33400 FHGROUP 46APRE 48487R571815-01-02 FLOOR PANELSGALLEY OR LAVATORY IFINSTALLED734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.7350 FCOR47700 FH3900 FCOR25300 FHGROUP 46APOST 48487R571815-01-03 FLOOR PANELSGALLEY OR LAVATORY IFINSTALLED734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL AT SYSTEM HOLES AREAS : Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.6250 FCOR43100 FH3190 FCOR21900 FHGROUP 46BPRE 55989R571815-01-04 FLOOR PANELSGALLEY OR LAVATORY IFINSTALLED734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.8800 FCOR67100 FH5150 FCOR39500 FHGROUP 45APRE 48487N571815-01-05 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLED, 734 744147AZ 148AZ.SPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.7250 FCOR55400 FH3850 FCOR29600 FHGROUP 45APOST 48487N571815-01-06 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLED, 734 744147AZ 148AZ.SPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL AT SYSTEM HOLES AREAS: Y+953 & Y+1456 AND Y1456 & Y-1959, BETWEEN STIFFENERS 22 AND 23 ANDBETWEEN STIFFENERS 17 AND 18.6610 FCOR52900 FH3550 FCOR28400 FHGROUP 45BPRE 55989D571816-01-01 TASK DELETED IN ISSUE 11D571816-01-02 TASK DELETED IN ISSUE 11© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 43RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340D571816-01-03 TASK DELETED IN ISSUE 11D571816-01-04 TASK DELETED IN ISSUE 11D571816-01-05 TASK DELETED IN ISSUE 11D571816-01-06 TASK DELETED IN ISSUE 11D571816-01-07 TASK DELETED IN ISSUE 11D571816-01-08 TASK DELETED IN ISSUE 11D571816-01-09 TASK DELETED IN ISSUE 11D571816-01-10 TASK DELETED IN ISSUE 11571817-01-01 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL, UPPER FACE AT PUMP HOLES AREA, BETWEENFR.44 AND FR.47.6300 FCOR41400 FH3600 FCOR23800 FHGROUP 46A571817-01-02 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL, UPPER FACE AT PUMP HOLES AREA, BETWEENFR.44 AND FR.47.6300 FCOR42400 FH3500 FCOR24500 FHGROUP 46B571817-01-03 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL, UPPER FACE AT PUMP HOLES AREA, BETWEENFR.44 AND FR.47.6500 FCOR49900 FH3700 FCOR28700 FHGROUP 45A571817-01-04 FLOOR PANELS, GALLEYOR LAVATORY IFINSTALLEDSPECIAL DETAILED INSPECTION OF CWB, UPPER SKINPANEL, UPPER FACE AT PUMP HOLES AREA, BETWEENFR.44 AND FR.47.6400 FCOR51300 FH3700 FCOR29800 FHGROUP 45B571818-01-01 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.10800 FCOR70300 FH4700 FCOR30700 FHGROUP 46APRE 48487571818-01-02 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.6900 FCOR45100 FH3000 FCOR19700 FHGROUP 46APOST 48487571818-01-03 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.14400 FCOR99600 FH4500 FCOR31000 FHGROUP 46B571818-01-04 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.10400 FCOR79900 FH4300 FCOR33000 FHA340-500PRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 44RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571818-01-05 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.8400 FCOR64400 FH3400 FCOR26600 FHGROUP 45APOST 48487571818-01-06 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF UPPER PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.14100 FCOR113200 FH5200 FCOR41700 FHGROUP 45B571819-01-01 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.9500 FCOR62000 FH3500 FCOR23100 FHGROUP 46APRE 48487571819-01-02 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.9500 FCOR62000 FH2300 FCOR15300 FHGROUP 46APOST 48487571819-01-03 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.9300 FCOR64000 FH2500 FCOR17500 FHGROUP 46B571819-01-04 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.10000 FCOR76700 FH3200 FCOR24600 FHA340-500PRE 48487571819-01-05 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.10000 FCOR76700 FH2400 FCOR18900 FHGROUP 45APOST 48487571819-01-06 147AZ 148AZ734 744GENERAL VISUAL INSPECTION OF LOWER SKIN PANEL ANDSTIFFENERS AT CENTER WING BOX AREA.9800 FCOR79100 FH3600 FCOR29300 FHGROUP 45B571831-02-01 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3400 FCOR22300 FH3400 FCOR22300 FHA340-600PRE 48487571831-02-02 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3000 FCOR21000 FH3000 FCOR21000 FHGROUP 46B571831-02-03 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3600 FCOR28000 FH3600 FCOR28000 FHA340-500PRE 48487571831-02-04 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3500 FCOR23300 FH3500 FCOR23300 FHGROUP 46APOST 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 45RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340571831-02-05 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3800 FCOR29300 FH3800 FCOR29300 FHGROUP 45APOST 48487571831-02-06 734 744147AZ 148AZSPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, LOWER CORNERS OF ACCESS CUTOUTS.3800 FCOR30600 FH3800 FCOR30600 FHGROUP 45B572206-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEENRIB 1 AND 12.11400 FCOR69300 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572206-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEENRIB 1 AND 12.8200 FCOR56400 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572210-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 6 AND RIB 23.10300 FCOR62600 FH5000 FCOR30700 FHA340-500PRE 48487ORA340-600PRE 48487572210-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 6 AND RIB 23.10500 FCOR63600 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572210-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 6 AND RIB 23.9300 FCOR63900 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572211-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO CENTER SPARBETWEEN RIB 6 AND RIB 9.13200 FCOR80200 FH7400 FCOR45100 FHA340-500PRE 48487ORA340-600PRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 46RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572211-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO CENTER SPARBETWEEN RIB 6 AND RIB 9.11800 FCOR71900 FH5400 FCOR33100 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572211-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO CENTER SPARBETWEEN RIB 6 AND RIB 9.10000 FCOR68700 FH3500 FCOR24200 FHGROUP 45BORGROUP 46B572212-01-01 541AB 541AZ 541CZ 542AB542BZ 641AB 641AZ 641CZ642AB 642BZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 BETWEEN RIB 4 AND RIB 8.11600 FCOR70700 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572212-01-02 541AB 541AZ 541CZ 542AB542BZ 641AB 641AZ 641CZ642AB 642BZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 BETWEEN RIB 4 AND RIB 8.9600 FCOR66000 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572213-01-01 542BB 542CB 542DB 542EB542FB 542GB 642BB 642CB642DB 642EB 642FB 642GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 26 BETWEEN RIB 7 AND RIB 15.10800 FCOR65800 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572213-01-02 542BB 542CB 542DB 542EB542FB 542GB 642BB 642CB642DB 642EB 642FB 642GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 26 BETWEEN RIB 7 AND RIB 15.12100 FCOR83400 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572214-01-01 541AB 541AZ 541CZ 542AB542BZ 641AB 641AZ 641CZ642AB 642BZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 4 AND RIB8.11700 FCOR71200 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572214-01-02 541AB 541AZ 541CZ 542AB542BZ 641AB 641AZ 641CZ642AB 642BZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 4 AND RIB8.9600 FCOR66300 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 47RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572215-01-01 542BB 542CB 542DB 542EB542FB 542GB 642BB 642CB642DB 642EB 642FB 642GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 26 BETWEEN RIB 7 AND RIB15.11000 FCOR67100 FH6500 FCOR39400 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572215-01-02 542BB 542CB 542DB 542EB542FB 542GB 642BB 642CB642DB 642EB 642FB 642GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 26 BETWEEN RIB 7 AND RIB15.12400 FCOR85600 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572236-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3AND RIB 7.7900 FCOR48300 FH7900 FCOR48300 FHA340-500PRE 48487ORA340-600PRE 48487572236-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3AND RIB 7.8600 FCOR52500 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572236-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 3AND RIB 7.8000 FCOR55200 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572239-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIBBAY 3-4 AND RIB BAY 11-13.10800 FCOR65400 FH8000 FCOR48000 FHA340-500PRE 48487ORA340-600PRE 48487572239-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIBBAY 3-4 AND RIB BAY 11-13.9100 FCOR55100 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572239-01-03 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT REAR SPAR STRINGER RUNOUTS RIBBAY 3-4 AND RIB BAY 11-13.9300 FCOR64300 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 48RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572241-02-01 573/673 BB, FB, DEPLOYFLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER ANDLOWER ATTACHMENT ANGLES.10300 FCOR62400 FH8000 FCOR48000 FHA340-500PRE 48487ORA340-600PRE 48487572241-02-02 573/673 BB, FB, DEPLOYFLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE BETWEEN RIB 1 AND RIB 12 INCLUDING UPPER ANDLOWER ATTACHMENT ANGLES.11100 FCOR67500 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572244-01-02 541AB 641AB DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE UPPER AND LOWER ROOT JOINTFITTINGS.13200 FCOR90700 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572246-01-01 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB5.9700 FCOR59100 FH7700 FCOR47000 FHA340-500PRE 48487ORA340-600PRE 48487572246-01-02 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB5.10600 FCOR64700 FH7800 FCOR47800 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572246-01-03 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR AFT FACE AT SYSTEM HOLE BETWEEN RIB 3 AND RIB5.9400 FCOR64700 FH7200 FCOR49500 FHGROUP 45BORGROUP 46B572247-01-01 573FB 673FBDEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WING REARSPAR FORWARD FACE JOINT PLATE AT RIB 9.12300 FCOR85100 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572264-01-03 522EB 622EB DETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE JOINT PLATE AT RIB 12.14000 FCOR96500 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 49RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572265-01-01 542BB 542CB 542CZ 542DZ642BB 642CB 642CZ 642DZDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 11 INCLUDING TOP ANDBOTTOM FLANGES.12000 FCOR73100 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572265-01-02 542BB 542CB 542CZ 542DZ642BB 642CB 642CZ 642DZDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 11 INCLUDING TOP ANDBOTTOM FLANGES.10700 FCOR74000 FH5000 FCOR34900 FHGROUP 45BORGROUP 46B572276-02-01 542CB 542DB 542DZ542EZ 642CB 642DB642DZ 642EZDETAILED INSPECTION OF OUTER WING RIB 10 FORWARD,RIB 10A AND PYLON DIAPHRAGM.11800 FCOR81100 FH6200 FCOR42800 FHGROUP 45BORGROUP 46B572277-02-01 542AB 542AZ 542BB542BZ 542CB 542CZ542DB 542DZ 542EB542EZ 642AB 642AZ642BB 642BZ 642CB642CZ 642DB 642DZ642EB 642EZDETAILED INSPECTION OF OUTER WING RIBS 10 AFT, 11AND 12, FORWARD AND AFT OF CENTER SPAR, AT SKINATTACHMENTS (INCLUDING CLEATS), SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.7800 FCOR54200 FH4700 FCOR32300 FHGROUP 45BORGROUP 46B572278-01-01 542AB 642AB SPECIAL DETAILED INSPECTION OF OUTER WING RIB 7 AFTAT TOP AND BOTTOM CASTELLATIONS FOR STRINGERS.11100 FCOR67500 FH3600 FCOR22300 FHGROUP 45AORGROUP 46A572278-01-02 542AB 642AB SPECIAL DETAILED INSPECTION OF OUTER WING RIB 7 AFTAT TOP AND BOTTOM CASTELLATIONS FOR STRINGERS.9100 FCOR62600 FH3500 FCOR24200 FHGROUP 45BORGROUP 46B572281-01-02 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.10300 FCOR62900 FH4100 FCOR25000 FHA340-500PRE 48487ORA340-600PRE 48487572286-01-01 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPARUPPER AND LOWER ROOT JOINT FITTINGS IN RIB BAY 1-2.11700 FCOR71200 FH5300 FCOR32100 FHA340-500PRE 48487ORA340-600PRE 48487572286-01-02 541/641 AB, AZ DETAILED INSPECTION OF OUTER WING CENTER SPARUPPER AND LOWER ROOT JOINT FITTINGS IN RIB BAY 1-2.13700 FCOR94700 FH12500 FCOR86100 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 50RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572287-01-01 542/642 DB DETAILED INSPECTION OF OUTER WING CENTER SPAR TOUPPER AND LOWER STRINGER JOINTS IN RIB BAY 11-12.7600 FCOR46400 FH6600 FCOR40300 FHA340-500PRE 48487ORA340-600PRE 48487572287-01-02 542/642 DB DETAILED INSPECTION OF OUTER WING CENTER SPAR TOUPPER AND LOWER STRINGER JOINTS IN RIB BAY 11-12.7900 FCOR47900 FH5600 FCOR34400 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572287-01-03 542/642 DB SPECIAL DETAILED INSPECTION OF OUTER WING CENTERSPAR TO UPPER AND LOWER STRINGER JOINTS IN RIB BAY11-12.7700 FCOR53000 FH1900 FCOR13400 FHGROUP 45BORGROUP 46BR572288-01-01 542AB 542BB 542BZ 542CB542CZ 542DZ 642AB 642BB642BZ 642CB 642CZ 642DZDETAILED INSPECTION OF OUTER WING CENTRE SPARBETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACESINCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES ANDCONDUIT HOLES.9200 FCOR55800 FH3000 FCOR18700 FHA340-500PRE 48487ORA340-600PRE 48487R572288-01-02 542AB 542BB 542BZ 542CB542CZ 542DZ 642AB 642BB642BZ 642CB 642CZ 642DZDETAILED INSPECTION OF OUTER WING CENTRE SPARBETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACESINCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES ANDCONDUIT HOLES.11900 FCOR72200 FH3300 FCOR20300 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572288-01-03 542AB 542BB 542BZ 542CB542CZ 542DZ 642AB 642BB642BZ 642CB 642CZ 642DZDETAILED INSPECTION OF OUTER WING CENTRE SPARBETWEEN RIB 6 AND RIB 11 FORWARD AND AFT FACESINCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES ANDCONDUIT HOLES.12600 FCOR86900 FH3500 FCOR24400 FHGROUP 45BORGROUP 46B572289-01-01 541AB 541AZ 541BB 541BZ541CZ 641AB 641AZ 641BB641BZ 641CZDETAILED INSPECTION OF OUTER WING CENTRE SPARBETWEEN RIB 2 AND RIB 6 FORWARD AND AFT FACESINCLUDING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN HOLES, VENT HOLES ANDCONDUIT HOLES.10600 FCOR73200 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 51RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572307-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACKCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLESAFT OF FRONT SPAR AND FORWARD OF REAR SPARBETWEEN RIBS 12 AND 41.9000 FCOR55000 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572307-01-04 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT DRAIN HOLES FOR SLAT TRACKCANS, FUEL JETTISON HOLE, MLI HOLES AND DRAIN HOLESAFT OF FRONT SPAR AND FORWARD OF REAR SPARBETWEEN RIBS 12 AND 41.8800 FCOR60800 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572313-01-02 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURE IN RIBBAY 12-13.13800 FCOR83800 FH5500 FCOR33300 FHGROUP 45APOST 48487POST 51484ORGROUP 46APOST 48487POST 51484572313-01-04 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURE IN RIBBAY 12-13.11600 FCOR80300 FH4600 FCOR31600 FHGROUP 45BORGROUP 46B572314-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT FUEL JETTISON HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEENRIBS 17 AND 18.8500 FCOR51600 FH5700 FCOR34900 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572314-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT FUEL JETTISON HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEENRIBS 17 AND 18.10500 FCOR72300 FH5900 FCOR40700 FHGROUP 45BORGROUP 46B572315-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 23 AND RIB 36.9400 FCOR57500 FH3000 FCOR18300 FHGROUP 45APOST 48487ORGROUP 46APOST 48487© AIRBUS SAS 2009. 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CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 52RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572315-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 23 AND RIB 36.11200 FCOR77300 FH7600 FCOR52300 FHGROUP 45BORGROUP 46B572316-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT FRONT SPAR STRINGERRUNOUTS, STR 7 (RIB BAY 14-15), STR 8 (RIB BAY 17-18)AND STR 9 (RIB BAY 19-20).10400 FCOR63400 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572316-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT FRONT SPAR STRINGERRUNOUTS, STR 7 (RIB BAY 14-15), STR 8 (RIB BAY 17-18)AND STR 9 (RIB BAY 19-20).9800 FCOR68000 FH7600 FCOR52800 FHGROUP 45BORGROUP 46B572317-01-01 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 642DB 642EB 642FB642GB 642HB 642JB 642KB642LB 642MBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.10300 FCOR62900 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572317-01-02 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 642DB 642EB 642FB642GB 642HB 642JB 642KB642LB 642MBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 AND STRINGER 18 BETWEEN RIB 11 & RIB 20.11200 FCOR77300 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572318-01-01 543QB 543RB 543SB 543TB543UB 643QB 643RB 643SB643TB 643UBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 BETWEEN RIB 25 & RIB 30.10100 FCOR61200 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572318-01-02 543QB 543RB 543SB 543TB543UB 643QB 643RB 643SB643TB 643UBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 BETWEEN RIB 25 & RIB 30.9000 FCOR62500 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 53RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572319-01-01 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 642DB 642EB 642FB642GB 642HB 642JB 642KB642LB 642MBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 18BETWEEN RIB 11 & RIB 20.10300 FCOR62900 FH6500 FCOR39400 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572319-01-02 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 642DB 642EB 642FB642GB 642HB 642JB 642KB642LB 642MBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 AND STRINGER 18BETWEEN RIB 11 & RIB 20.11200 FCOR77300 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572320-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT FRONT SPAR STRINGERRUNOUTS, STR 12 (RIB BAY 27-28), STR 13 (RIB BAY 29-30)AND STR 14 (RIB BAY 32-33).8100 FCOR49500 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572320-01-02 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT FRONT SPAR STRINGERRUNOUTS, STR 12 (RIB BAY 27-28), STR 13 (RIB BAY 29-30)AND STR 14 (RIB BAY 32-33).10600 FCOR73100 FH7600 FCOR52800 FHGROUP 45BORGROUP 46B572321-01-01 543CB 543DB 543EB 543FB543GB 543QB 543RB 543SB543TB 543UB 643CB 643DB643EB 643FB 643GB 643QB643RB 643SB 643TB 643UBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 25 & RIB30.10100 FCOR61700 FH7600 FCOR46600 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572321-01-02 543CB 543DB 543EB 543FB543GB 543QB 543RB 543SB543TB 543UB 643CB 643DB643EB 643FB 643GB 643QB643RB 643SB 643TB 643UBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 25 & RIB30.10500 FCOR72700 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 54RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572322-01-01 PYLON FAIRINGSFLAP TRACK FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO STRINGERS,RIBSAND REAR SPAR BETWEEN RIB 12 AND RIB 27.11600 FCOR70400 FH3500 FCOR21500 FHA340-500PRE 48487ORA340-600PRE 48487572322-01-02 PYLON FAIRINGSFLAP TRACK FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO STRINGERS,RIBSAND REAR SPAR BETWEEN RIB 12 AND RIB 27.12700 FCOR77100 FH3700 FCOR23000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572323-01-01 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 542NB 542PB 542QB542SB 542SB 642DB 642EB642FB 642GB 642HB 642JB642KB 642LB 642MB 642NB642PB 642QB 642SB 642SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS, STRINGER JOINTS AND BUTTSTRAPSBETWEEN RIB 11 AND RIB 23 EXCLUDING STRINGERS 13,18AND 26.11600 FCOR70500 FH8000 FCOR48000 FHA340-500PRE 48487ORA340-600PRE 48487572323-01-02 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 542NB 542PB 542QB542SB 542SB 642DB 642EB642FB 642GB 642HB 642JB642KB 642LB 642MB 642NB642PB 642QB 642SB 642SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS, STRINGER JOINTS AND BUTTSTRAPSBETWEEN RIB 11 AND RIB 23 EXCLUDING STRINGERS 13,18AND 26.10100 FCOR61200 FH5300 FCOR32300 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572335-01-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT FRONT SPAR STRINGER RUNOUTS,RIB BAY 14-15.13400 FCOR81600 FH4500 FCOR27200 FHGROUP 45APOST 48487ORGROUP 46APOST 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 55RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572336-01-01 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINLOWER SURFACE STRINGER JOINTS, RIB BAY 12-13,STRINGER 20.13300 FCOR80500 FH8000 FCOR48000 FHA340-500PRE 48487ORA340-600PRE 48487572336-01-02 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINLOWER SURFACE STRINGER JOINTS, RIB BAY 12-13,STRINGER 20.8400 FCOR50900 FH8000 FCOR48000 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572336-01-03 542EB 642EB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINLOWER SURFACE STRINGER JOINTS, RIB BAY 12-13,STRINGER 20.10600 FCOR72900 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572337-01-01 542HB 642HB SPECIAL DETAILED INSPECTION OF OUTER WING TOP SKINLOWER SURFACE STRINGER JOINTS, RIB BAY 15-16,STRINGER 28.13200 FCOR80000 FH5400 FCOR33100 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572338-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPERSURFACE ABOVE FRONT SPAR BETWEEN RIB 11 AND RIB22.10600 FCOR64600 FH3600 FCOR22100 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572340-01-01 542EB 542FB 542GB 542HB542JB 542KB 542LB 542MB542NB 542PB 542QB 542RB542SB 642EB 642FB 642GB642HB 642JB 642KB 642LB642MB 642NB 642PB 642QB642RB 642SBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS AND BUTTSTRAPS BETWEEN RIBS 12 AND 23AND STRINGER JOINTS 12,13,14 AT RIB BAY 22-23.11400 FCOR69200 FH6800 FCOR41400 FHGROUP 45APOST 48487ORGROUP 46APOST 48487572362-01-02 523/623 DB DETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 26.11200 FCOR77400 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 56RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572367-01-01 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 542NB 542PB 542QB542SB 542SB 543AB 543BB543CB 543DB 543EB 543FB543GB 543HB 543JB 543KB543LB 543MB 543NB 543PB543QB 543RB 543SB 543TB543UV 543VB 642DB 642EB642FB 642GB 642HB 642JB642KB 642LB 642MB 642NB642PB 642QB 642SB 642SB643AB 643BB 643CB 643DB643EB 643FB 643GB 643HB643JB 643KB 643LB 643MB643NB 643PB 643QB 643RB643SB 643TB 643UV 643VBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 11 AND RIB 35 INCLUDING TOP ANDBOTTOM FLANGES.9900 FCOR60000 FH4700 FCOR28700 FHGROUP 45APOST 48487ORGROUP 46APOST 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 57RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572367-01-02 542DB 542EB 542FB 542GB542HB 542JB 542KB 542LB542MB 542NB 542PB 542QB542SB 542SB 543AB 543BB543CB 543DB 543EB 543FB543GB 543HB 543JB 543KB543LB 543MB 543NB 543PB543QB 543RB 543SB 543TB543UV 543VB 642DB 642EB642FB 642GB 642HB 642JB642KB 642LB 642MB 642NB642PB 642QB 642SB 642SB643AB 643BB 643CB 643DB643EB 643FB 643GB 643HB643JB 643KB 643LB 643MB643NB 643PB 643QB 643RB643SB 643TB 643UV 643VBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 11 AND RIB 35 INCLUDING TOP ANDBOTTOM FLANGES.8900 FCOR61400 FH2700 FCOR18700 FHGROUP 45BORGROUP 46B572372-02-01 543BB 543CB 543PB543QB 643BB 643CB643PB 643QBOUTBOARD PYLONFAIRINGSVENT PIPES DISPLACEDFROM RIB 23 OUTBOARDDETAILED INSPECTION OF OUTER WING RIBS, RIB 25INCLUDING INTERNAL PYLON ATTACHMENT BRACKET.6500 FCOR45200 FH7000 FCOR48700 FHGROUP 45BORGROUP 46B572373-02-01 542/642 EB, FB, KB, LB, QB,SB 543/643 AB, NBDETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGERCUTOUTS AND FORWARD FLAP TRACK BRACKETS.9200 FCOR56300 FH3400 FCOR21100 FHA340-500PRE 48487ORA340-600PRE 48487© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 58RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340572373-02-02 542/642 EB, FB, KB, LB, QB,SB 543/643 AB, NBDETAILED INSPECTION OF OUTER WING RIBS, RIB 13, 18AND 23 AT SKIN ATTACHMENTS AND REGION OF STRINGERCUTOUTS AND FORWARD FLAP TRACK BRACKETS.12300 FCOR84800 FH7000 FCOR48700 FHGROUP 45BORGROUP 46B572655-01-02 573BB 573FB 673BB673FBDETAILED INSPECTION OF OUTER WING TRAILING EDGERIBS 5A AND 5B INCLUDING BACKING ANGLES AND FLAPTRACK 2 AFT PICK UP (INCLUDING BOX BRACKET,INTERFACE PLATE AND THRUST PADS).12400 FC 4800 FC GROUP 45AORGROUP 46A572656-02-01 532/632/533/633/534/634 SB DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK-UP, ASSEMBLY.8200 FC 8000 FC A340-500PRE 48487ORA340-600PRE 48487572656-02-02 532/632/533/633/534/634 SB DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK-UP, ASSEMBLY.7000 FC 7000 FC GROUP 45APOST 48487ORGROUP 46APOST 48487572659-01-01 523AB 523BB 523AT 523CT623AB 623BB 623AT 623CTSPECIAL DETAILED INSPECTION OF OUTER WING OUTERPYLON INBOARD AND OUTBOARD FORWARD ATTACHMENTFITTINGS.8000 FCOR48000 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B572666-01-01 533VT 533WB 534VT 534WB633VT 633WB 634VT 634WBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 4AND 5 FORWARD PICK-UP FITTING LUGS.8300 FC 5500 FC A340-500PRE 48487ORA340-600PRE 48487572666-01-02 533VT 533WB 534VT 534WB633VT 633WB 634VT 634WBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 4AND 5 FORWARD PICK-UP FITTING LUGS.8300 FC 7400 FC GROUP 45APOST 48487ORGROUP 46APOST 48487572666-01-03 533VT 533WB 534VT 534WB633VT 633WB 634VT 634WBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 4AND 5 FORWARD PICK-UP FITTING LUGS.8000 FC 4400 FC GROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 59RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340574158-02-01 521/621 AB DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAINATTACHMENTS TO FRONT SPAR AND FUSELAGE.6900 FCOR42200 FH4000 FCOR24600 FHA340-500PRE 48487ORA340-600PRE 48487574158-02-02 521/621 AB DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE FAIRING SUPPORT INBOARD OF RAMP RIB, MAINATTACHMENTS TO FRONT SPAR AND FUSELAGE.11600 FCOR70800 FH4900 FCOR30200 FHGROUP 45APOST 48487ORGROUP 46APOST 48487574170-01-01 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 23 AND RIB 26.12200 FCOR74100 FH2600 FCOR16000 FHA340-500PRE 48487ORA340-600PRE 48487574170-01-02 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 23 AND RIB 26.9400 FCOR57100 FH1800 FCOR11100 FHGROUP 45APOST 48487ORGROUP 46APOST 48487574170-01-03 454AL 454AR 484AL 484AR DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 23 AND RIB 26.10500 FCOR72700 FH2500 FCOR17300 FHGROUP 45BORGROUP 46B574171-01-01 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS ATSLAT TRACKS 7-9 AND SLAT TRACK 14.13600 FCOR82900 FH1000 FCOR6100 FHGROUP 45APOST 48487ORGROUP 46APOST 48487574172-01-01 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS ATSLAT TRACKS 12 & 138000 FCOR48000 FH1000 FCOR6400 FHGROUP 45APOST 48487ORGROUP 46APOST 48487574172-01-02 SLATS FULLY EXTENDED DETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE D-NOSE LOWER SKIN SLAT TRACK CUTOUTS ATSLAT TRACKS 12 & 138100 FCOR55700 FH1000 FCOR7100 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 60RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340N574353-01-01 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACKLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.9100 FCOR69200 FH2000 FCOR15200 FHGROUP 45AN574353-01-02 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACKLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.9400 FCOR61100 FH2300 FCOR14900 FHGROUP 46AN574353-01-03 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACKLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.8400 FCOR67200 FH2000 FCOR16000 FHGROUP 45BN574353-01-04 SLATS FULLY EXTENDED GENERAL VISUAL INSPECTION OF SLAT 1, TRACKS 1 TO 4ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACKLUGS, BOLTS, LINKS AND LINK PLATE, LH/RH.8800 FCOR60300 FH2200 FCOR15000 FHGROUP 46B575071-02-01 FLAPS EXTENDED734 744DETAILED INSPECTION OF FLAP TRACK BEAM NO 1,ROLLER TRACKS.12000 FC 8300 FC A340-500ORA340-600575074-01-02 FLAPS EXTENDED734 744DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOXSUPPORT, FORK ASSEMBLY, DRIVE STRUT AND CARRIAGE.12000 FC 8300 FC GROUP 45APRE 48487ORGROUP 46APRE 48487ORGROUP 46BORGROUP 45B575074-01-03 FLAPS EXTENDED734 744DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOXSUPPORT, FORK ASSEMBLY, DRIVE STRUT AND CARRIAGE.12000 FC 6500 FC GROUP 45APOST 48487ORGROUP 46APOST 48487575077-01-01 FLAPS EXTENDED734 744DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4AND 5, ROLLER TRACK.10800 FC 7600 FC GROUP 45AORGROUP 46A575077-01-02 FLAPS EXTENDED734 744DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4AND 5, ROLLER TRACK.10800 FC 7000 FC GROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 61RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575079-01-02 FLAPS EXTENDED, AFTFLAP TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5,DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITHTRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORTLINK AND TRAVELING BEAM AT TRACK NO 4.10800 FC 7600 FC GROUP 45AORGROUP 46A575079-01-03 FLAPS EXTENDED, AFTFLAP TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5,DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITHTRACKSIDE ATTACHMENT FITTINGS AND AFT SUPPORTLINK AND TRAVELING BEAM AT TRACK NO 4.10800 FC 7000 FC GROUP 45BORGROUP 46B575087-01-02 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575087-02-02.12000 FC 5000 FC A340-500PRE 48487ORA340-600PRE 48487575087-01-03 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575087-02-03.12000 FC 4700 FC A340-500POST 48487ORA340-600POST 48487575087-02-02 FWD FLAP TRACKFAIRINGSSPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMSNO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575087-01-02.12000 FC 5000 FC A340-500PRE 48487ORA340-600PRE 48487575087-02-03 FWD FLAP TRACKFAIRINGSSPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMSNO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575087-01-03.12000 FC 4700 FC A340-500POST 48487ORA340-600POST 48487575112-02-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREA COVEREDBY FLAP TRACK 2 FAIRING.13600 FCOR94100 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 62RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575114-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 9 AND RIB 12.10100 FCOR61500 FH2200 FCOR13400 FHA340-500PRE 48487ORA340-600PRE 48487575114-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 9 AND RIB 12.9100 FCOR55100 FH1900 FCOR11800 FHGROUP 45APOST48487ORGROUP 46APOST48487575114-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGETOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEENRIB 9 AND RIB 12.9400 FCOR65100 FH5300 FCOR37000 FHGROUP 45BORGROUP 46B575122-01-02 575AB 675AB DETAILED INSPECTION OF OUTER WING TRAILING EDGEINNER AILERON HINGES 1-3 AND THE TOP AND BOTTOMSKIN OVERHANGS UPPER AND LOWER SURFACES ATTHESE LOCATIONS.11400 FCOR69600 FH2500 FCOR15400 FHGROUP 45APOST 51830ORGROUP 46APOST 51830575123-01-02 575CB 675CB DETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTER AILERON HINGES 1-3 AND THE TOP AND BOTTOMSKIN OVERHANGS UPPER AND LOWER SURFACES ATTHESE LOCATIONS.6300 FCOR38200 FH6300 FCOR38200 FHGROUP 45APOST 51830ORGROUP 46APOST 51830575125-01-01 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGEINNER BOTTOM SKIN LOWER SURFACE AFT OF REAR SPARFROM RIB 9 TO RIB 12.10500 FCOR72800 FH8000 FCOR48000 FHGROUP 45BORGROUP 46B575126-01-02 575/675 BB DETAILED INSPECTION OF OUTER WING TRAILING EDGEINNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS ANDTHE TOP AND BOTTOM SKINS UPPER AND LOWERSURFACES AT ATTACHMENTS TO THE POSTS.8100 FCOR49300 FH4500 FCOR27400 FHA340-500PRE 48487PRE 51830ORA340-600PRE 48487PRE 51830© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 63RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340575126-01-03 575/675 BB DETAILED INSPECTION OF OUTER WING TRAILING EDGEINNER AILERON HINGES 4 AND 5, THEIR HINGEPOSTS ANDTHE TOP AND BOTTOM SKINS UPPER AND LOWERSURFACES AT ATTACHMENTS TO THE POSTS.6600 FCOR40100 FH3600 FCOR22300 FHGROUP 45APOST 51830ORGROUP 46APOST 51830575451-01-02 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD FLAP,EXTERNAL SURFACE OF UPPER AND LOWER SKIN.3000 FC 3000 FC A340-500ORA340-600575452-01-01 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKINAND DOUBLER IN CUT-OUT AREA FOR ATTACHMENTFITTINGS TRACK NO. 2.12000 FC 8600 FC A340-500ORA340-600575453-01-02 734 744581/681 ABPLUGSDETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 1 AND TRUNNION,EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575453-02-2.12000 FC 5700 FC A340-500ORA340-600575453-02-02 734 744581/681 AB, PLUGS, SPEEDTAPESSPECIAL DETAILED INSPECTION OF INBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 1 ANDTRUNNION, INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575453-01-02.12000 FC 5700 FC A340-500ORA340-600711351-01-01 415AL 416AR 425AL 426AR435AL 436AR 445AL 446ARDISASSEMBLY ONE BYONE OF THE HINGE BOLTIS REQUIRED.DETAILED INSPECTION OF FAN COWL, FITTINGS ANDSURROUNDING STRUCTURE (15 CM AROUND FITTINGS).4000 FC 4000 FC A340-500ORA340-600711352-01-01 415AL 416AR425AL 426AR435AL 436AR445AL 446ARDETAILED INSPECTION OF FAN COWL LATCH FITTINGS ANDSURROUNDING STRUCTURE (15 CM AROUND FITTINGS).4000 FC 4000 FC A340-500ORA340-600© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 64RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340712152-01-01 415AL 416AR 417AL 418AR425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448ARDETAILED INSPECTION OF TRENT 500-ENGINE FORWARDMOUNT REAR TRUNNION CLEARANCE HOLE.NOTE: THE INSPECTION IS FOR LOSS OF CLEARANCEBETWEEN THE REAR TRUNNION AND VERTICAL FAILSAFELOAD LINK ASSEMBLY.4000 FCOR27500 FH4000 FCOR27500 FHA340-500ORA340-600712153-01-01 415AL 416AR 417AL 418AR425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448ARENGINE REMOVAL ANDENGINE MOUNTDISASSEMBLYSPECIAL DETAILED INSPECTION OF TRENT 500-ENGINEFORWARD MOUNT THRUST TRUNNION.8000 FCOR55000 FH8000 FCOR55000 FHA340-500ORA340-600712252-01-01 415AL 416AR 417AL 418AR425AL 426AR 427AL 428AR435AL 436AR 437AL 438AR445AL 446AR 447AL 448ARFAILSAFE PIN RETAININGBOLT & WASHERTORQUE LINK PINRETAINING BOLTS &WASHERDETAILED INSPECTION OF TRENT 500-ENGINE REARMOUNT FAILSAFE PIN ,TORQUE LINK PIN.NOTE : INSPECTION OF THE FAILSAFE PIN IS FORFREEDOM OF MOVEMENT. INSPECTION OF THE TORQUELINK PIN IS FOR DAMAGE OF THE PIN AND RETAININGBOLTS.2400 FCOR16700 FH2400 FCOR16700 FHA340-500ORA340-600© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 65RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340783251-01-02 417EL 418ER427EL 428ER437EL 438ER447EL 448ERDISASSEMBLY ONE BYONE OF HINGE BOLTS ISREQUIRED.DETAILED INSPECTION OF THRUST REVERSER HINGELUGS AND SURROUNDING STRUCTURE (15 CM AROUNDHINGE LUGS).4000 FC 4000 FC A340-500ORA340-600R783252-01-01 415AL 416AR417AL 417FL418AR 425AL426AR 427AL427FL 428AR435AL 436AR437AL 437FL438AR 445AL446AR 447AL447FL 448ARDETAILED INSPECTION OF THRUST REVERSER 6 O'CLOCKBEAM LATCH ASSEMBLY (ON 2 HALVES) ANDSURROUNDING STRUCTURE (15 CM AROUND LATCHFITTINGS).4000 FC 4000 FC A340-500ORA340-600783253-01-01 414AL 414AR415AL 416AR417AL 417FL418AR 424AL424AR 425AL426AR 427AL427FL 428AR434AL 434AR435AL 436AR437AL 437FL438AR 444AL444AR 445AL446AR 447AL447FL 448ARDETAILED INSPECTION OF THRUST REVERSER AFT CORECOWL LATCH ASSEMBLY (ON 2 HALVES) ANDSURROUNDING STRUCTURE (15 CM AROUND LATCHFITTING).4000 FC 4000 FC A340-500ORA340-600© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 66RevcodeTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATIONS SECTIONA340783254-01-02 415AL 416AR417CL 417DL417EL 418CR418DR 418ER425AL 426AR427CL 427DL427EL 428CR428DR 428ER435AL 436AR437CL 437DL437EL 438CR438DR 438ER445AL 446AR447CL 447DL447EL 448CR448DR 448ERDISCONNECTION ONE BYONE OF THE ACTUATORFROM THE T/R COWL ISREQUIRED.DETAILED INSPECTION OF THRUST REVERSER FORWARDFRAME AND TRANSCOWL ACTUATOR FITTINGS AND ITSATTACHMENTS (6 PLACES ON EACH HALF).4000 FC 4000 FC A340-500ORA340-600783255-01-01 415/425/435/445 AL416/426/436/446 AR417/427/437/447 FL417/427/437/447 AL418/428/438/448 ARDETAILED INSPECTION OF THRUST REVERSER J-RING (VBLADE).4000 FC 4000 FC A340-500ORA340-600© AIRBUS SAS 2009. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.Issue 11: February 2009 Section 2.2 - List of Airworthiness Limitation ItemsEASA APPROVEDPage 67

# 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 t he 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 comi ng 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 ex tend 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 t he 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 Desc ription updated.

R 571811-01-01 Descri ption simplified

R 571811-01-02 Descri ption simplified

R 571811-01-03 Descri ption simplified

R 571811-01-05 Descri ption 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, inspectabi lity, 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.