AIRBUS 

Customer Services Directorate 

A330 Airworthiness Limitation Items

A330 

Airworthiness Limitation Items 

© AIRBUS SAS 2010. All rights reserved. Confidential and proprietary document. 

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

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

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

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

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

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

for which it is supplied.

AI/SE-M4/95A.0089/97 

28 May 2010 

Issue 17
AIRWORTHINESS LIMITATION ITEMS 

TABLE OF CONTENTS

SUBJECT SECTION

ISSUE: 28 MAY 2010 PAGE: 1-TOC 

©AIRBUS SAS 2010. All rights reserved. 

A330 

RECORD OF REVISIONS ROR 

 INTRODUCTION 1 

 GENERAL 1-1 

 Airworthiness Limitations 1-1- A 

 RULES FOR COMPLIANCE DEMONSTRATION 1-2 

 General 1-2- A 

 Conditions for DT ALI inspection 1-2- B 

 Reporting 1-2- C 

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

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

 LIMIT OF VALIDITY (LOV) 1-3 

 APPLICABILITY 1-4 

General 1-4- A 

 Weight Variant (WV) applicability 1-4- B 

 Applicability System 1-4-C 

 EXPLANATION OF SECTION 2 TABLE FORMAT 1-5 

 AIRWORTHINESS LIMITATIONS 2 

 SUMMARY OF CHANGES APPENDIX A 

 

 ABBREVIATIONS APPENDIX B

 TERMS AND DEFINITIONS APPENDIX C
AIRWORTHINESS LIMITATION ITEMS 

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 1-ROR 

EASA APPROVED 

©AIRBUS SAS 2010. All rights reserved. 

A330 

Issue Date Reason for revision Approved 

by EASA 

1 22 Aug 97 Section 2 of CMR documents originally identified 

‘Structural Inspections’ These are not CMRs. New 

document created. 

Target date for inclusion of these requirements in 

MRB report extended from 1998 to 1999.

2 31 Mar 98 Applicability extended to include A330-202. 

Document retitled ‘Airworthiness Limitation Items’.

It was originally called ‘Structural Inspection 

Requirements’. 

Text of Section 1 modified to refer to A330-200 

and to add a new paragraph to justify 

acceptability of 1999 target date. 

3 23 Jun 98 Applicability extended to include A330-223.

4 02 Dec 98 Applicability extended to include A330-243.

5 15 Apr 99 Applicability extended to include A330-323.

6 02 Sep 99 Applicability extended to include A330-343.

7 16 Oct 01 Applicability extended to include A330-203. 

Text of Section 1 modified to revise target dates 

for publication of ALIs.

8 31 Oct 01 Document completely revised to introduce ALIs 

following completion of the full scale fatigue test 

and teardown analysis.

9 15 Oct 02 Applicability extended to include A330-201. WV 

022 added for A330-200. WVs 013, 014, 024 & 

025 added for A330-300. Reference to Zonal 

Program deleted from paragraph 1.5. 

10 20 Jun 03 Requirements added for A330-300 WVs 050 & 

052 in new WV GROUP 33E. New DSG added 

for GROUP 33E. To provide compatibility with 

MRBR and MPD, task numbering changed to 9 

digits and applicability amended. 

11 01 Sep 03 Requirements of WV GROUP 33E for GE 

engines (A330-300 WV 051) included. 

Tasks that were deleted in Issue 10 reintroduced.

12 01 Nov 03 Requirements of WV GROUP 32E for GE, PW 

and RR engines (A330-200 WV 050, 051, 052) 

included. 

Requirements of WV GROUP 33E for RR 
AIRWORTHINESS LIMITATION ITEMS 

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 2-ROR 

EASA APPROVED 

©AIRBUS SAS 2010. All rights reserved. 

A330 

Issue Date Reason for revision Approved 

by EASA 

engines (A330-300 WV 050, 052) included. 

Requirements for enhanced modifications 

embodied on non-fully enhanced aircraft 

included.

13 01 Mar 04 Applicability extended to include A330-302 and 

A330-303.

14 10 Oct 05 Task requirements for WV Group 33D (A330-300 

WV022) included. 

Task applicabilities changed due to impact of 

product improvement mods for A330 WV000 up 

to WV030 series. 

New numbering rules (ALI task previously with 9 

digits replaced by 10 Digit number system) 

included in section 2. 

WV053, 054, 055 added for Group 32E. 

WV027 added for Group 32A. 

WV026, 027 added for Group 33C. 

WV053 added for Group 33E. 

Confidentiality statement added.

Approved by 

EASA 

under reference 

EASA.A.C.01277 

on 17 January 2006 

15 26 Mar 07 WV 056 added for Group 32E. 

Task applicabilities changed due to impact of 

modifications. 

GE requirements updated due to new calculation. 

Approved by 

EASA 

under reference 

EASA.A.C.07222 

on 9 July 2007 

16 13 Jun 08 New compliance time requirements introduced in 

the Record Of Revisions. 

Introduction reworded with : 

New Limits Of Validity (LOV) 

New information concerning Rules for 

Compliance Demonstration (Alternative 

inspections, Multiple WV configuration...) 

Task requirements updated due to: 

Intermediate Service Goal exercise 

Fleet survey results 

Modifications/In-service experience 

Approved by 

EASA 

under reference 

EASA.A.C.10414 

on 4 Nov 2008 

17 28 MAY 2010 Task requirements for A330-200F added. 

Task applicabilities changed due to impact of 

modifications. 

Approved by 

EASA 

under reference 

10031148 

on 29 July 2010 

 
AIRWORTHINESS LIMITATION ITEMS 

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 3-ROR 

EASA APPROVED 

©AIRBUS SAS 2010. All rights reserved. 

A330 

COMPLIANCE TIME:

1. From the 29th of July 2011, it is mandatory to comply with the airworthiness limitations as 

defined in the A330 ALI Document revision 17. 

2. From the 29th of July 2010 to 28th of July 2011, 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 16 

or, 

- The ALI Document at issue 17. 

3. From the 29th of July 2010 to 28th of July 2011, for the following task/applicabilities limitations, 

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

- Table 1 

Or 

- The ALI document at issue 17: 

TABLE 1 

Task 

reference 

Adapted Threshold 

(whichever occurs first, from aircraft first 

flight) Applicability 

FH FC 

545140-01-03/ 58010 7760 MSN 524 

545140-02-03 57690 7760 MSN 542 

 58320 7760 MSN 533 

 57250 7760 MSN 549 

 58070 7760 MSN 552 

 57460 7760 MSN 578 

 58690 7760 MSN 588 

 58120 7760 MSN 591 

 24870 8290 MSN 640 

 55700 7760 MSN 663 

 57710 7760 MSN 674 

 24870 8290 MSN 676 

 57870 7760 MSN 690 
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INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 1 

©AIRBUS SAS 2010. All rights reserved. 

A330

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 00G050A3301/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 occuring 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 A330 MRB Report is an acceptable means of compliance. 

The Structure Section (Section D) of the A330 MRB report provides opportunities for timely 

detection of accidental damage and is an acceptable means of compliance for accidental 

damage. 

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). 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 2 

©AIRBUS SAS 2010. All rights reserved. 

A330

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 

performed. 

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 have to be evaluated and repaired in accordance with the AIRBUS Structural 

Repair Manual SRM or other documentation acceptable to the relevant Airworthiness 

Authority. 
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INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 3 

©AIRBUS SAS 2010. All rights reserved. 

A330

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 repairs, the DT ALI maintenance requirements may have to be 

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

that are given in the relevant documents (SRM or specific Repair design Approval Sheet) 

must be applied. 

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

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

1-2-C Reporting

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

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

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

− DT ALI maintenance requirement reference, 

− Aircraft Manufacturer Serial Number (MSN) affected, 

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

the finding, 

− Identification of the affected structure, 

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

− Circumstance of detection and inspection method used. 

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

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

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

Compliance (AMOC). 

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

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. 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 4 

©AIRBUS SAS 2010. All rights reserved. 

A330

1-3 LIMIT OF VALIDITY (LOV)

Aircraft series LOV 

 Flight Hours Flight Cycles 

A330-200 series excl. WV050’s and above or 060000 40000 

100000 33000 

A330-200 series WV050’s and above 100000 33000 

A330-200F 100000 33000 

A330-300 series excl. WV050’s and above or 060000 40000 

100000 33000 

A330-300 series WV050’s and above 100000 33000 

Note: When different LOVs are indicated for a given aircraft series, no combination is allowed. 

Example: A330-200 series excl. WV050’s and above : 

These aircraft shall be operated within the envelope of: 

40000 FC and 60000 FH (initial LOV) OR 33000 FC and 100000FH. 

Values from each pair of associated parameters must not be mixed. 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 5 

©AIRBUS SAS 2010. All rights reserved. 

A330

1-4 APPLICABILITY 

1-4-A General

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

Aircraft series Aircraft models WV

A330-200 

A330-201 020, 023, 024, 050, 052, 055, 056, 059, 060

A330-202 020, 021, 022, 023, 050, 052, 053, 055, 

056, 059, 060 

A330-203 020, 022, 023, 026, 050, 051, 052, 054, 

055,056, 059, 060 

A330-223 020, 021, 022, 023, 050, 052, 055, 056, 

059, 060 

A330-243 020, 021, 022, 023, 024, 025, 026, 027, 

050, 052, 055, 056, 059, 060 

A330-200F 

A330-223F 000, 001 

A330-243F 000, 001 

A330-300 

A330-301 000, 001, 002, 003, 004, 010, 051 

A330-302 050, 052, 053 

A330-303 050, 052 

A330-321 000, 002, 003, 004, 010, 011, 012, 013 

A330-322 000, 002, 003, 004, 010, 011, 012, 013 

A330-323 020, 022, 025, 050, 052 

A330-341 000, 002, 003, 004, 010, 011, 012, 013, 014

A330-342 000, 002, 003, 004, 010, 011, 012, 013, 

014, 022, 052 

A330-343 020, 022, 024, 050, 052
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 6 

©AIRBUS SAS 2010. All rights reserved. 

A330

1-4-B Weight Variant (WV) applicability

A/C Series Weight Variants WV Group 

A330-200 

020, 021, 022, 023, 024, 025, 026, 027 Group 32A 

050, 051, 052, 053, 054, 055, 056, 059, 060 Group 32E 

A330-200F 000, 001 - 

A330-300 

000, 001, 002, 003, 004 Group 33A 

010, 011, 012, 013, 014 Group 33B 

020, 024, 025, 026, 027 Group 33C 

022 Group 33D 

050, 051, 052, 053 Group 33E 

Interpretation: Group XYZ 

− X: Aircraft Type 3 for A330 

− Y: Series (2 for -200, 3 for -300) 

− 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 table provides limitations depending on the aircraft weight variants within 

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

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. 

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 embodiement of the referenced Service Bulletins in 

order to determine the relevant weight variant for the affected Manufacturer Serial Number 

(MSN). 

For aircraft having mutliple WV configurations possibility, the limits of the WV of the highest 

MTOW have to be applied. 

 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 7 

©AIRBUS SAS 2010. All rights reserved. 

A330

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 

ALL All A330 aircraft. 

A330-xxx -xxx series aircraft. 

A330-200 A330-200 Pax aircraft 

A330-200F A330-200 Freighter aircraft 

PRE nnnnn All A330 PRE MOD nnnnn. 

i.e. A330 that do not have MOD nnnnn embodied. 

POST nnnnn All A330 POST MOD nnnnn. 

i.e. A330 that do have MOD nnnnn embodied. 

POST nnnnn 

Sxxxxx 

All A330 POST MOD nnnnn (at least with Mod Proposal Sxxxxx embodied). 

POST nnnnn 

POST mmmmm 

All A330 POST MOD nnnnn and POST MOD mmmmm. 

i.e. A330 that do have MOD nnnnn and MOD mmmmm embodied. 

A330-200 

OR 

A330-300 

PRE nnnnn 

All A330-200, 

Or, 

All A330-300 that do not have MOD nnnnn embodied. 

A330-200 

POST nnnnn 

OR 

POST mmmm 

All A330-200 that do have MOD nnnnn embodied, 

Or, 

All A330-200 that do have MOD mmmm embodied. 

A330-200 

POST nnnnn 

OR 

A330-300 

POST nnnnn 

PRE mmmmm 

All A330-200 that do have MOD nnnnn embodied, 

Or, 

All A330-300 that do have MOD nnnnn embodied and do not have MOD mmmmm 

embodied. 

GE All A330 equipped with GE CF6-80 E1 engines. 

PW All A330 equipped with PW 4000 engines. 

RR All A330 equipped with RR Trent 700 engines. 

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 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 8 

©AIRBUS SAS 2010. All rights reserved. 

A330

1-5 EXPLANATION OF SECTION 2 TABLE FORMAT

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

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. 532114-01-03. 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. 532114. 

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. 
AIRWORTHINESS LIMITATION ITEMS 

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 9 

©AIRBUS SAS 2010. All rights reserved. 

A330

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 structutral 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. 
2 AIRWORTHINESS LIMITATIONS

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

DOOR 1 (FORWARD PASSENGER/CREW DOOR).

1

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

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8

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

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8

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

DOOR 2 (MID PASSENGER/CREW DOOR).

1

AIRWORTHINESS LIMITATION SECTION

A330 

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

DOOR 2 (MID PASSENGER/CREW DOOR).

6

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

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.

8

A330 

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

DOOR 4 (AFT PASSENGER/CREW DOOR).

1

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

DOOR 4 (AFT PASSENGER/CREW DOOR).

6

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

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

8

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).

1

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

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).

6

N 523104-01-02 132AR 132BR 132CR 

132DR 132ER 132FR 132GR 132HR 132JR132KR 132LR

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT DOOR HINGE ASSEMBLIES AT FR 20B TO FR25 (10 PLACES). 

1

R 523106-01-01 821CR

DOOR LOCKING HANDLE UNLOCKED

DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT , DOOR FRAME C20B BETWEEN BEAM 3 AND 4.

1

N 523204-01-02 152AR 152BR 152CR 

152DR 152ER 152FR 152GR 152HR 152JR152KR 152LR

DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR HINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES) 

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

524101-01-02 N/A DETAILED INSPECTION OF AVIONICS COMPARTMENT LOWER 

ACCESS DOOR SKIN, EXTERNAL SURFACE.

1

524103-01-02 811

DOOR FLOOR PANEL

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, AVIONICS COMPARTMENT LOWER ACCESS DOOR CROSS MEMBERS.

3

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

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

8

R 528203-01-02 713 714 DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARD 

DOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON 

9

, (, , ) 

FUSELAGE, LH/RH. 

N 528206-01-01 713 714 715 716 DETAILED INSPECTION OF NOSE LANDING GEAR DOORS, 

HINGES (NO 1, NO 2, NO 3, NO 4, NO5) INCLUDING FITTINGS ON FUSELAGE, LH/RH.

1

531106-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 

AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.

2

531106-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 

AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.

3

N 531106-01-06 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR.9 

AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 531108-01-01 LINING

NOTE 1

SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINT AT FRAME 18 BETWEEN STRINGER 3 AND STRINGER 7, BUTT JOINT AND REAR PANEL, LH.

1

N 531109-01-01 LINING

NOTE 1

 SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINT AT FRAME 18 BETWEEN STRINGER 11 AND STRINGER 13, BUTT JOINT AND REAR PANEL, RH . 

2

R 531110-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10 

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

1

N 531110-02-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 10 

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

1

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

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

9

,

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

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

8

R 531118-01-01 121AL 121EL

713 714

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

3

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

STRUCTURE, NOSE LANDING GEAR WELL PANELS.

1

531124-01-03 713 714 DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER 

RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH.

2

531124-01-04 713 714 DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER 

RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH.

2

531124-01-05 713 714 DETAILED INSPECTION OF NLG BAY SIDE PANEL TOP INNER 

RADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFT PANEL, LH/RH.

2

531125-01-03 811 821

AVIONICS BAY FLOORPANELS

SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531125-01-04 811 821

AVIONICS BAY FLOORPANELS

SPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH.

2

N 531125-02-01 811 821

AVIONICS BAY FLOORPANELS

DETAILED INSPECTION OF FRAME 17 ATTACHMENT TO BOTTOM SKIN FROM STRINGER 46 TO 51, LH/RH.

1

531129-02-02 713 714 715

716BOLTSNLG ACTUATORSDISCONNECTED

SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING.

2

531130-01-02 NOTE 1 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL 

STRUCTURE, FRAME 16A AT CABIN FLOOR LEVEL, LH/RH.

2

531131-01-02 NOTE 1 DETAILED INSPECTION OF FUSELAGE INTERNAL 

STRUCTURE, FRAME 16A, JOINT AREA BETWEEN STRINGERS 28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 531131-02-02.

1

531131-02-02 NOTE 1 SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL 

STRUCTURE, FRAME 16A, JOINT AREA BETWEEN STRINGERS 28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 531131-01-02.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531132-01-02 NOTE 1 DETAILED INSPECTION OF FUSELAGE INTERNAL 

STRUCTURE, FRAME 14 JOINT BETWEEN STRINGERS 28 AND 30 LEVEL, LH/RH.

3

531133-01-03 NOTE 1

AIR DUCTS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ON FRAME 12A AT STRINGER 26 LEVEL, LH/RH.

2

531134-01-01 AVIONICS COMPT DOOR

OPENED

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.

3

531134-01-02 AVIONICS COMPT DOOR

OPENED

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.

2

531134-01-03 AVIONICS COMPT DOOR

OPENED

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO 16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47, LH/RH.

2

531135-01-02 N/A SPECIAL DETAILED INSPECTION OF REAR LOWER CORNER 

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

4

531136-01-02 CEILING PANELS

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 12 AND 13 DOUBLER AREA AT CROWN CENTRELINE.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531138-01-02 RADOME OPENED

INSULATION PANELS

DETAILED INSPECTION OF FORWARD PRESSURE BULKHEAD FORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50 ABOVE COCKPIT FLOOR LEVEL.

3

531139-01-02 811

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACE VERTICAL BEAMS AND UPPER SHEET AT Y=-330, Y=0 AND Y=330, ABOVE COCKPIT FLOOR LEVEL.

3

531140-01-01 831

LININGNOTE 1GALLEYS AND TOILETS IF INSTALLED

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

1

531141-01-02 LINING

NOTE 1

DETAILED INSPECTION OF LATERAL FRAME 11, SPLICE ABOVE COCKPIT FLOOR LEVEL ATTACHMENT, INTERNAL STRUCTURE, LH/RH.

1

531142-01-02 CEILING

NOTE 1

DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-02-02.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531142-02-02 CEILING

NOTE 1

SPECIAL DETAILED INSPECTION OF FRAME 10 UPPER CURVED MEMBER BETWEEN CROWN CENTRELINE AND UPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNAL STRUCTURE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-01-02.

3

531143-01-02 NOTE 1

AIR DUCTSVACUUM PIPES

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

1

531144-01-02 NOTE 1

LININGTOILET

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

1

N 531145-01-01 LINING

NOTE 1

SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINT AT FRAME19 BETWEEN STRINGER 45 AND STRINGER 47, BUTT JOINT AND REAR PANEL, RH.

2

531146-01-01 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LATERAL AND AFT WINDOW FRAMES JUNCTION WITH FRAME 7 UPPER MEMBER, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 531148-01-01 LINING

NOTE 1

SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINT AT FRAME18 BETWEEN STRINGER 30 AND STRINGER 32, BUTT JOINT AND REAR PANEL, LH.

2

531149-01-01 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, ANGLE GUSSET ABOVE FRONT WINDSHIELD PANELS, INCLUDING TOP 3 NUTS ON CENTRE POST.

3

531154-01-02 LININGS

SLIDING WINDOWSOPENEDNOTE 1

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

1

R 531154-01-03 LININGS

SLIDING WINDOWS OPENEDNOTE 1

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

3

N 531155-01-01 LINING

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 14C, FROM STRINGER 9 TO STRINGER 12, LH/RH.

1

531157-01-02 LINING

NOTE 1

DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPER KEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL, INTERNAL STRUCTURE, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531158-01-01 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, JUNCTION AREA BETWEEN AFT WINDOW FRAME AND FRAMES 8 AND 9 UPPER MEMBERS, LH/RH.

3

N 531160-01-01 811 821

AVIONICS BAY FLOORPANELS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RADIUS OF LUGS ON UPPER CORNER OF PORTAL FRAME 15A, LH/RH.

9

531161-01-02 LINING

NOTE 1

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

1

N 531163-01-01 713 714

NLG

SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR MAIN ATTACHEMENT BEARING BORE, LH/RH.

1

N 531164-01-01 713 714 SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR 

BAY LATERAL PANELS, JUNCTION TO LOWER FRAME 17 FITTING, LH/RH.

7

N 531169-02-01 125AL 125BL 125CL

126BR 126CR 713 714

DETAILED INSPECTION OF NOSE FUSELAGE LOWER SKIN AND FAIRING SUBSTRUCTURE, AREA COVERED BY NOSE FAIRING BETWEEN FR10 AND FR17 INCLUDING NLG BAY LATERAL PANEL EXTERNAL SURFACE, FLAT PANEL, FR16A AND FORWARD FACE OF LOWER FR17 FITTING, LH/RH.

1

531175-01-03 LINING

NOTE 1

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

2

N 531177-01-01 125AL 125BL 125CL

126BR 126CR 713 714

SPECIAL DETAILED INSPECTION OF LONGITUDINAL JUNCTION CENTRAL AND LATERAL PANELS AT STRINGER 46, EXTERNAL SURFACE BETWEEN FR11 TO FR12A, LH/RH.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 531178-01-01 125AL 125BL 125CL

126BR 126CR 713 714

DETAILED INSPECTION OF Y750 AFT FITTING, TOP RADIUS, LH/RH.

2

N 531179-01-01 125AL 125BL 125CL

126BR 126CR 713 714

SPECIAL DETAILED INSPECTION OF LOWER FRAME 17 FITTING AT Y750 FITTING JUNCTION, LH/RH.

1

531183-01-01 TOILETS, LINING, 

INSULATION TO BE DISPLACED, FASTENERS TO BE REMOVED

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH.

3

531183-01-02 TOILETS, LINING, 

INSULATION TO BE DISPLACED, FASTENERS TO BE REMOVED

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWS FORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH.

2

N 531184-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP 

2

,

JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A AND FROM FR.14 TO FR.16A, LH/RH.

531185-01-02 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PASSENGER / CREW DOOR CUTOUT 

AFT UPPER CORNER, JUNCTION OF INTERNAL PLATE ON FR. 17, BETWEEN STR.12 AND 13, LH/RH.

2

531186-01-02 TOILETS & CRR

LININGSNOTE 1TITANIUM RIVETS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531186-01-03 TOILETS & CRR

LININGSNOTE 1TITANIUM RIVETS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OF FORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD, LH/RH.

2

531188-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 3

CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STGR.9 FWD LEVEL, LH/RH.

531188-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OF FRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWS AT STGR.9 FWD LEVEL, LH/RH.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

531189-01-02 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT, FORWARD UPPER LONGERON AT STRINGER 12 LEVEL, BETWEEN FR. 13A AND FR.13B, LH/RH.

2

R 531192-01-03 LINING

NOTE 1

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

2

R 531194-01-03 LINING

NOTE 1

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

2

,

531198-01-02 LINING

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE BELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANEL BETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH.

2

R 532101-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-02

2

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

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TO BOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRING LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-02

6

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

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

2

12

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

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

2

12

532114-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

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

28

532114-01-05 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

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

28

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

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

3

R 532117-01-03 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 STR 26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-02-03

2

N 532117-02-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 STR 26, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-03

2

532124-02-04 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE 

UNDERNEATH SCUFF PLATE, LH/RH.

29

532124-02-05 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE 

UNDERNEATH SCUFF PLATE, LH/RH.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532124-02-06 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE 

UNDERNEATH SCUFF PLATE, LH/RH.

28

532124-02-07 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE 

UNDERNEATH SCUFF PLATE, LH/RH.

28

532124-02-08 832 842

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE 

UNDERNEATH SCUFF PLATE, LH/RH.

28

532124-02-09 832 842 SPECIAL DETAILED INSPECTION OF DOOR 2 (MID 2

SCUFF PLATE

(

PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH SCUFF PLATE, LH/RH.

8

532124-02-10 832 842

SCUFF PLATE

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

2

14

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

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

29

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

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

27

532125-01-06 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532125-01-07 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

28

532125-01-08 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

28

532125-01-09 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

28

532125-01-10 832 842 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

2

14

532126-01-01 832 842

DOOR FRAME LINING

DETAILED INSPECTION OF DOOR 2, COVER PLATE OF TORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND 

1

INSULATION

,

STR 13, LH/RH. 85

532127-01-01 832 842

DOOR FRAME LININGNOTE 1

DETAILED INSPECTION OF DOOR NO 2, FR 33, BETWEEN STR 13 AND STR 15, LH/RH.

16

R 532128-01-01 832 842 GENERAL VISUAL INSPECTION OF DOOR NO 2 (MID 

PASSENGER/CREW DOOR) STOP FITTINS ON FR33 AND FR 35A, LH/RH.

1

532129-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2

532129-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532130-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROM STR 18 TO STR 22, LH/RH.

2

532130-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROM STR 18 TO STR 22, LH/RH.

29

532130-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AND VISIBLE PORTION OF WINDOW FORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROM 

2

15

,

STR 18 TO STR 22, LH/RH.

R 532138-01-01 131AG 821

DRAINMAST

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

2

532139-01-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AT CLOSED DRAIN MAST CUT-OUT BETWEEN FR 28 AND FR 29, FROM STR 46 TO STR 47, RH.

2

R 532143-01-02 ANTENNA DETAILED INSPECTION OF SKIN AROUND GPS ANTENNAS 

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

2

R 532144-01-02 832 842

CEILING PANELSNOTE 1

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

2

R 532146-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

R 532147-01-02 821

CARGO COMPARTMENTFLOOR PANELSLININGSNOTE 1

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

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 532148-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

R 532149-01-02 832 842

CEILING AND SIDE WALL PANELSOVERHEAD STOWAGE BINSINSULATION

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

2

532150-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

3

532150-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

2

532150-01-04 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

3

532151-01-01 N/A SPECIAL DETAILED INSPECTION OF EXTERNAL SKIN OF 

LONGITUDINAL LAP JOINT AT STR 22, BETWEEN FR 37.1 AND FR 38.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532153-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW 

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

1

532153-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOW 

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

1

10

532154-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE AT SPOT LIGHT CUT-OUT, BETWEEN- FR 27 AND FR 28 AND BETWEEN- FR 30 AND FR 31,

2

, 

- FROM STR 24 TO STR 26, LH/RH 

532155-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND DOUBLER AT 

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

2

532156-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532156-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

2

532156-01-04 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

3

532157-01-02 832 842

SIDEWALL LINING

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

3

INSULATION

, ,

LH/RH. 

532158-01-02 833 843

CEILING PANELSINSULATION

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

3

532158-01-03 833 843

CEILING PANELSINSULATION

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

3

532164-01-01 821

CEILING PANELS

SPECIAL DETAILED INSPECTION OF FWD FUSELAGE, CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR 22 AND FR 23.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

532165-01-02 831 841

CEILING PANELSLININGINSULATION

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

3

532165-01-03 831 841

CEILING PANELSLININGINSULATION

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

3

N 532166-01-03 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO CROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-03

4

N 532166-02-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TO CROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532117-01-03

6

N 532182-01-01 835

LINING NOTE1

SPECIAL DETAILED INSPECTION OF FRAME AND FRAME COUPLING FROM FR 20 TO FR 26/28 AT STR 21 RH

1

N 532183-01-01 835

LINING NOTE1

SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AND CIRCUMFERENTIAL SPLICE AT FR 31 BETWEEN STR 5 AND CROWN CENTER LINE, LH/RH.

1

533005-01-02 191AB 191AT 191BB

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

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

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533009-01-01 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-01

39

533009-01-02 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 

LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-02

2

14

533009-01-03 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-03

39

533009-01-04 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 

LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-04

39

533009-02-01 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 

LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-01

39

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533009-02-02 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-02

2

14

533009-02-03 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, 

LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-03

39

533009-02-04 251JC 251VW 252JC

252VWOVERHEAD STOWAGEBINSNOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEEN STRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-04

39

533010-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH.

39

533010-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH.

2

14

533010-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH.

39

533010-01-04 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH.

39

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 533012-01-01 261CC 262CC

OVERHEAD STOWAGEBINSNOTE 1RIVETS

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO 5, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-01

27

R 533012-02-01 261CC 262CC

OVERHEAD STOWAGEBINSNOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4 TO 5, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-01

27

533013-01-02 FLOOR PANELS

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANEL STIFFENER 

2

,

JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH.

11

533013-01-03 FLOOR PANELS

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH.

27

533013-01-04 FLOOR PANELS

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, CANTED PRESSURE PANEL STIFFENER JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 AND Y=2361, LH/RH.

27

533014-01-01 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR 

BAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF FRAME 47 DATUM, LH/RH.

27

533014-01-02 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR 

BAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFT OF FRAME 47 DATUM, LH/RH.

2

14

533016-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN CENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH.

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533016-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWN CENTERLINE TO STR 3 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH.

3

10

533018-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH.

2

13

533018-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH.

28

533018-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

CIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWN CENTERLINE TO STR 4 AND FROM STR 5 TO STR 11, EXTERNAL SURFACE, LH/RH.

39

,

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

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

1

533104-01-03 ANTICOLLISION LIGHT: 

LENS 7LVADF: LENSES 2RP1 & SEAL AND 2RP2 & SEAL

DETAILED INSPECTION OF FUSELAGE SKIN 50 MM AROUND:- UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 AND FR.43- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEEN FR.48 AND FR.49 AND BETWEEN FR.52 & FR.53, BETWEEN STRINGER 1 LH AND STRINGER 1 RH.

39

533105-01-02 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

13

533106-01-02 N/A DETAILED INSPECTION OF FUSELAGE EXTERNAL 

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533107-01-03 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

14

533107-01-04 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

16

533107-01-05 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

14

533107-01-06 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

28

,

533107-01-07 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

2

11

533107-01-08 LINING

NOTE 1AIR CONDITIONINGDUCTS

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

14

533109-01-01 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

LONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME 38 TO 53.3, AT STRINGER 13 FROM FRAME 38 TO 47 AND AT STRINGER 22 FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVET ROWS FORWARD AND AFT FRAME 45 LEVEL, LH/RH.

3

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

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

13

533113-01-05 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

13

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533113-01-06 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

9

4

533113-01-07 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

13

533113-01-08 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

15

533113-01-09 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

13

N 533113-01-10 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOW STRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.

1

533114-01-03 251XW 252XW

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTION WITH STABILIZERS STRINGER 20 TO 23, LH/RH.

26

533114-01-04 251XW 252XW

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTION WITH STABILIZERS STRINGER 20 TO 23, LH/RH.

15

533114-01-06 251XW 252XW

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTION WITH STABILIZERS STRINGER 20 TO 23, LH/RH.

18

533115-01-04 251XW 252XW

NOTE 1

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

14

533115-01-05 251XW 252XW

NOTE 1

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

13

533115-01-06 251XW 252XW

NOTE 1

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

13

533115-01-07 251XW 252XW

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 

9

23, LH/RH. 4

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533115-01-08 251XW 252XW

NOTE 1

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

15

N 533115-01-09 251XW 252XW

NOTE 1

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

1

533124-01-02 734 744 DETAILED INSPECTION OF BELLY FAIRING STRUCTURE AT 

CLG DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION, LH/RH.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA.

3

R 533125-01-01 734 744 GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR 

53.2 PRESSURE BULKHEAD INCLUDING THE ATTACHMENT AREA OF THE CLG TRUNNION FITTINGS.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA.

1

533126-01-03 734 744 GENERAL VISUAL INSPECTION OF AREA AROUND CLG AND 

MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA.

4

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533126-01-05 734 744 GENERAL VISUAL INSPECTION OF AREA AROUND CLG AND 

MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA.

4

1

533126-01-06 734 744 GENERAL VISUAL INSPECTION OF AREA AROUND CLG AND 

MLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTED TO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGE STRUCTURAL COMMONALITY WITH THE A340 IN THIS AREA.

3

533127-03-01 FAIRING PANELS BETWEEN 

FR.39.1 AND FR.47

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

4

1

533127-03-02 FAIRING PANELS BETWEEN 

FR.39.1 AND FR.47

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

4

2

533127-03-03 FAIRING PANELS BETWEEN 

FR.39.1 AND FR.47

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

3

N 533127-03-04 FAIRING PANELS BETWEEN 

FR.39.1 AND FR.47

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

1

533137-01-01 251FG 251MG 252FG

252MG

DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM FUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER AT Y=2565, LH/RH.

3

533137-01-02 251FG 251MG 252FG

252MG

DETAILED INSPECTION OF HORIZONTAL PRESSURE PANEL AND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52 FROM FUSELAGE SKIN PANEL TO FIRST HORIZONTAL STIFFENER AT Y=2565, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533138-01-02 FLOOR PANELS

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y=1959, AT FR48 LEVEL LH/RH.

26

533145-01-03 197AT 197HB 198AT

198HB

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

2

533145-01-04 197AT 197HB 198AT

198HB

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

2

533154-01-04 CABIN FLOOR PANELS

GALLEYS

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, RIVET ROWS AT SHEAR PANELS AND 

1

TOILETS

,

LONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1, LH/RH.

533154-01-05 CABIN FLOOR PANELS

GALLEYSTOILETS

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

2

533154-01-06 CABIN FLOOR PANELS

GALLEYSTOILETS

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

2

533155-01-01 251FG 252FG

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH.

3

17

533155-01-02 251FG 252FG

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533155-01-03 251FG 252FG

NOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, 

LH/RH

3

11

533156-01-01 822

LININGNOTE 1LD-MCR IF INSTALLEDPOST 46678: LDL TOILETS AND FURNISHINGS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH.

3

10

533162-01-02 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR 

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

14

533164-01-03 734 744 DETAILED INSPECTION OF FUSELAGE INTERNAL 

STRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OF 

3

,

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

15

533164-01-04 734 744 DETAILED INSPECTION OF FUSELAGE INTERNAL 

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

2

14

533164-01-06 734 744 DETAILED INSPECTION OF FUSELAGE INTERNAL 

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

28

533164-01-07 734 744 DETAILED INSPECTION OF FUSELAGE INTERNAL 

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

3

10

N 533164-01-08 734 744 DETAILED INSPECTION OF FUSELAGE INTERNAL 

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

2

533165-01-02 251MG 251SG 252MG

252SGNOTE 1GALLEYS & TOILETS IFINSTALLED

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

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533179-01-02 251MG 251SG 252MG

252SGNOTE 1

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

27

533180-01-03 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE 

AND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

29

533180-01-04 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE 

AND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

27

533180-01-05 N/A DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE 24

AND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)

9

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

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

29

533181-01-04 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

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

27

533181-01-05 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

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

29

533181-01-06 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533181-01-07 N/A SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THE 

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

16

N 533187-01-01 CABIN FLOOR PANELS

GALLEYS & TOILETS IFINSTALLED

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.

2

11

N 533187-01-02 CABIN FLOOR PANELS

GALLEYS & TOILETS IFINSTALLED

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.

27

N 533187-01-03 CABIN FLOOR PANELS

GALLEYS & TOILETS IFINSTALLED

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.

26

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

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) AT FR 53.5 

1

( ) 

AND 53.7 A, LH/RH. 

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

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

3

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

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

28

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

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

14

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

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

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533194-01-07 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

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

27

533194-01-08 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

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

29

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

DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT 

2

( )

UPPER CORNERS. 90

533194-01-11 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

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

1

10

533194-01-12 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN AT 

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

29

533195-02-04 834 844

SCUFF PLATE

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

28

533195-02-05 834 844

SCUFF PLATE

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

14

533195-02-06 834 844

SCUFF PLATE

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

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

533195-02-07 834 844

SCUFF PLATE

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

27

533195-02-08 834 844

SCUFF PLATE

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

29

533195-02-09 834 844

SCUFF PLATE

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, 

2

( ) ,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. 90

533195-02-11 834 844

SCUFF PLATE

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

1

10

533195-02-12 834 844

SCUFF PLATE

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

29

N 533196-01-01 734 744 SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR 

BAY, CATENARIES SKINS AT JUNCTION WITH GANTRIES Y1456, OUTSIDE BOARD, AND Y1959, INSIDE BOARD, BETWEEN FR48 AND FR49 LH/RH.

1

534102-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

29

534102-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

29

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534102-01-05 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

12

534104-01-04 833 843

CEILING PANELSOVERHEAD STOWAGEBINS, INSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS 4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22, LH/RH.

15

534104-01-05 833 843

CEILING PANELSOVERHEAD STOWAGE

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS 4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22, 

29

BINS, INSULATION

, ,

LH/RH.

534104-01-06 833 843

CEILING PANELSOVERHEAD STOWAGEBINS, INSULATION

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS 4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22, LH/RH.

2

12

534105-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

10

534105-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534105-01-05 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

10

534105-01-06 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

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

2

13

534107-01-02 833 843

CEILING PANELSOVERHEAD STOWAGEBINS, INSULATION

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

16

534107-01-03 833 843

CEILING PANELSOVERHEAD STOWAGEBINSINSULATION

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

2

10

534107-01-04 833 843

CEILING PANELSOVERHEAD STOWAGEBINSINSULATION

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

2

13

534120-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

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

2

534120-01-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534120-01-04 N/A DETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLE 

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

18

R 534124-01-02 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEEN 

FR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK534124-02-02

2

N 534124-02-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN FR 54 

AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDING AREA UNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE.

2

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK534124-01-02

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

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

2

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

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

6

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

2

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

2

10

534131-01-04 833 843 SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFT 

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.

2

15

534132-02-01 833 843 SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT 2

SCUFF PLATE

(

PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE LH/RH.

534132-02-02 833 843

SCUFF PLATE

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

2

10

534132-02-03 833 843

SCUFF PLATE

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

2

15

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

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

1

534136-01-02 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN OF AFT 

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

29

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534137-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN OF AFT CARGO 

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

29

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

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

2

12

R 534139-01-04 822 GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL 

3

, 

FRAMES (FR 59A AND 65) AS FAR AS VISIBLE. 

R 534140-02-02 822 GENERAL VISUAL INSPECTION OF LOCK FITTINGS OF AFT 

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

7

534143-01-02 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

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

2

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

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

28

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

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

2

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534144-01-02 823

SCUFF PLATE

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

2

534144-01-03 823

SCUFF PLATE

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

28

534144-01-04 823

SCUFF PLATE

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

2

12

R 534146-01-02 823 GENERAL VISUAL INSPECTION OF BULK CARGO 1

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

534148-01-02 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA 

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

28

534148-01-03 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA 

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

28

534148-01-04 ANTENNA DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA 

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

2

12

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

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

3

R 534150-01-02 823

LININGSNOTE 1

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

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 534150-01-03 823

LININGSNOTE 1

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

28

534151-01-01 833 843

DOOR FRAME LINING

DETAILED INSPECTION OF WEB OF FUSELAGE DOOR FRAME 73A, FROM CABIN FLOOR TO STRINGER 11, LH/RH 

2

534152-01-01 833 843

SIDEWALL LININGSNOTE 1

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE FROM FR 60 TO FR 66 AND FROM STR 18 TO STR 23 RH IN FRAME COUPLING AREA.

2

534153-01-01 162ZW 823

NOTE 1

DETAILED INSPECTION OF WEB OF FR 73A BELOW CABIN FLOOR, BETWEEN STR 26 AND 26X LH/RH.

2

, 

R 534154-01-02 833 843

LININGINSULATION

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

2

R 534155-01-02 833 843

LININGINSULATION

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

2

534156-01-02 822

LININGCARGO FLOOR PANELSINSULATION

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

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

534164-01-01 822

CEILING PANELS

SPECIAL DETAILED INSPECTION OF AFT FUSELAGE, CARGO DOOR ACTUATOR SUPPORT BEAM BETWEEN FR 61 AND FR 62.

2

534165-01-01 162ZW 823

NOTE 1

DETAILED INSPECTION OF WEB OF FR 75A, BELOW CABIN FLOOR, BETWEEN STR 26 AND STR 26X, LH/RH.

2

534166-01-02 ANTENNA SPECIAL DETAILED INSPECTION OF SKIN AROUND VHF2 

ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 56 

2

, 

TO STR 57, RH. 

534166-01-03 ANTENNA SPECIAL DETAILED INSPECTION OF SKIN AROUND VHF2 

ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 51 

2

TO STR 52, LH. 

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 534177-01-03 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TO CROWN CENTER LINE, EXLUDING AREA UNDER VERTICAL STABILIZER FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-03

4

N 534177-02-03 N/A DETAILED INSPECTION OF FUSELAGE SKIN EXTERNAL 

SURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TO CROWN CENTER LINE, EXLUDING AREA UNDER VERTICAL STABILIZER FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-03

6

N 534182-01-01 835

LINING 

SPECIAL DETAILED INSPECTION OF FRAME AND FRAME COUPLING FROM FR 60 TO FR 64 BETWEEN STR 20X AND STR 

1

NOTE1 23, RH. 3

N 534184-01-01 821

LININGNOTE1

DETAILED INSPECTION OF FRAME AND FRAME COUPLING AT FR 67, STR 33 RH AND FR 69, STR 33 RH.

26

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

FACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26 LH/RH AND CROWN CENTER LINE.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

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

3

N 545103-02-04 ENGINE SPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OF 

ARMS AT ENGINE FORWARD MOUNT FITTING.

1

545104-02-03 415AL 416AR 425AL

426AR 453AZ 463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMID ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)

15

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545104-02-04 415AL 415BL 416AR

416BR 425AL 425BL426AR 426BR 453AZ463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMID ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)

15

545104-02-05 415AL 416AR 425AL

426AR 453AZ 463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMID ATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.

15

(2 FASTENER LOCATIONS/PYLON) 

545104-02-12 415AL 416AR 425AL

426AR 453AZ 463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)

19

545104-02-13 415AL 415BL 416AR

416BR 425AL 425BL426AR 426BR 453AZ463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)

19

545104-02-14 415AL 416AR 425AL

426AR 453AZ 463AZ

SPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMS BETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)

19

N 545108-04-19 415AL 416AR 425AL 426AR 

415BL 416BR 425BL 426BR

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1.

7

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 545108-04-20 415AL 416AR 425AL 426AR DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE 

FORWARD MOUNT FITTING TO RIB 1.

7

545111-02-01 ENGINE

AFT ENGINE MOUNT DISASSEMBLED

SPECIAL DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT UPPER BEAM AT RIB 9C.

9

9

545138-01-06 N/A DETAILED INSPECTION OF PYLON LATERAL PANELS, AREA 

OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BEETWEEN RIB 10 AND RIB 11.

3

15

545138-01-07 N/A DETAILED INSPECTION OF PYLON LATERAL PANELS, AREA 

OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-03.

15

545138-01-09 N/A DETAILED INSPECTION OF PYLON LATERAL PANELS, AREA 

OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-05.

27

545138-01-10 N/A DETAILED INSPECTION OF PYLON LATERAL PANELS, AREA 

OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-06.

2

10

545138-01-12 N/A DETAILED INSPECTION OF PYLON LATERAL PANELS, AREA 

OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-12 

18

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545138-02-03 N/A SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, 

AREA OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-07.

15

545138-02-05 N/A SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, 

AREA OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-09.

27

545138-02-06 N/A SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, 

AREA OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-10.

2

10

545138-02-12 N/A SPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS, 

AREA OF FASTENERS SECURING SUPPORT TO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-12

18

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 545140-01-01 N/A DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA 

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (4750 FC OR 14250 FH)

13

R 545140-01-02 N/A DETAILED INSPECTION OF PYLON, LATE , RAL PANELS, AREA 1

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (3770 FC OR 11310 FH)

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 545140-01-03 N/A DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA 

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (3060 FC OR 9180 FH)

8

2

R 545140-01-06 N/A 545140 01 06 N/A DETAILED DETAILED INSPECTION INSPECTION OF PYLON OF PYLON,LATERAL PANELS LATERAL PANELS,AREA 1

AREA 

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-06.

THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (4560 FC OR 22800 FH)

1

5

R 545140-01-07 N/A DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA 

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (3620 FC OR 18090 FH)

15

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 545140-01-08 N/A DETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA 

OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (2930 FC OR 14680 FH)

7

3

R 545140-02-01 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-01

13

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-01. 

THIS ALI TASK SUPERSEDES THE AOT A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (7600 FC OR 22800 FH)

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 545140-02-02 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (7100 FC OR 21310 FH)

13

R 545140-02-03 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL , 8

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (5630 FC OR 16900 FH)

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 545140-02-06 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (7290 FC OR 36450 FH)

15

R 545140-02-07 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-07

15

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-07. 

THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (6810 FC OR 34080 FH)

R 545140-02-08 N/A SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (5400 FC OR 27030 FH)

7

3

N 545140-02-09 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

13

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 545140-02-10 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

13

N 545140-02-11 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

8

2

N 545140-02-12 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

15

N 545140-02-13 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL , 1

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

5

N 545140-02-14 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

7

3

N 545140-02-15 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

7

N 545140-02-16 FASTENERS SPECIAL DETAILED INSPECTION OF PYLON, LATERAL 

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545142-02-01 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

9

2

545142-02-02 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

8

2

545142-02-05 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545142-02-06 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

13

545142-02-07 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

16

545142-02-08 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

15

545142-02-09 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 

9

4

AND RIB 14. 

545142-02-10 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

7

3

N 545142-02-11 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

13

N 545142-02-12 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS MATING SURFACE AND INTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13 AND RIB 14.

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545143-02-04 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-01.

26

545143-02-09 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-04.

28

545143-02-10 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-05.

2

12

545143-02-13 453CL 453CR 463CL

463CR

DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-13

2

10

545143-03-01 453CL 453CR 463CL

463CR

SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-04.

26

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545143-03-04 453CL 453CR 463CL

463CR

SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-09.

28

545143-03-05 453CL 453CR 463CL

463CR

SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-10.

2

12

545143-03-13 453CL 453CR 463CL

463CR

SPECIAL DETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATING SURFACE BETWEEN RIB 10 AND RIB 11.

2

10

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-13

545146-03-01 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES : - HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-01.

26

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545146-03-02 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-02.

14

545146-03-03 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION

28

- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-03.

545146-03-04 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-04.

26

545146-03-05 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-05.

2

13

545146-03-06 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-06.

19

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545146-03-07 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES : - HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-07

19

545146-03-08 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-08

17

545146-04-01 452AL 453BL 453BR

462AL 463BL 463BR

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.

2

PRE-COOLERRODS, AIR DUCT

,

NOTES : - INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-01.

6

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545146-04-02 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-02.

14

545146-04-03 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE

28

- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-03.

545146-04-04 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-04.

26

545146-04-05 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-05.

2

13

545146-04-06 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-06.

19

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545146-04-07 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES : - INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-07

19

545146-04-08 452AL 453BL 453BR

462AL 463BL 463BRPRE-COOLERRODS, AIR DUCT

SPECIAL DETAILED INSPECTION OF PYLON, LOWER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-08

17

545150-02-01 452AL 462AL

PRE-COOLER

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

2

RODSAIR DUCT

,

8

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545150-02-02 452AL 462AL

PRE-COOLERRODSAIR DUCT

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

26

545150-02-06 452AL 462AL

PRE-COOLERRODSAIR DUCT

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

39

545150-02-07 452AL 462AL DETAILED INSPECTION OF PYLON, UPPER SPAR AND 3

PRE-COOLERRODSAIR DUCT

,

LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. 

15

545150-02-10 452AL 462AL

PRE-COOLERRODSAIR DUCT

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

2

13

545150-02-11 452AL 462AL

PRE-COOLERRODSAIR DUCT

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

2

11

N 545150-02-13 452AL 462AL

PRE-COOLERRODSAIR DUCT

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545166-02-05 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

3

10

545166-02-06 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

26

545166-02-08 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

26

545166-02-09 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

3

15

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545166-02-10 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

19

545166-02-13 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

3

15

545166-02-14 454BL 454BR 464BL

464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTINGS AT RIB 12.

19

545168-02-05 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON).

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545168-02-06 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON).

26

545168-02-08 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON).

26

545168-02-09 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON).

3

( ) 

15

545168-02-10 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON).

19

545168-02-13 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)

3

15

545168-02-14 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON)

19

N 545168-02-15 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON)

1

N 545168-02-16 452CL 452CR 462CL 462CR 

454BL 454BR 464BL 464BR

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON)

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545174-02-03 PRE 43271:

454DL 454DR 454FL 454FR 464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR 464KL 464KR 464ML 464MR

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A.

3

11

545174-02-06 PRE 43271:

454DL 454DR 454FL 454FR 464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR 

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A.

3

11

464KL 464KR 464ML 464MR 

545174-02-07 PRE 43271:

454DL 454DR 454FL 454FR 464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR 464KL 464KR 464ML 464MR

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A

3

15

545174-02-09 PRE 43271:

454DL 454DR 454FL 454FR 464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR 464KL 464KR 464ML 464MR

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A

3

15

N 545174-02-10 454KL 454KR 454ML 454MR 

464KL 464KR 464ML 464MR

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A

1

N 545174-02-11 454KL 454KR 454ML 454MR 

464KL 464KR 464ML 464MR

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

545180-04-04 ENGINE

LINKSSLEEVESAFT SECONDARYSTRUCTURE

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON).

15

545180-04-05 ENGINE

LINKSSLEEVESAFT SECONDARYSTRUCTURE

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON).

15

545180-04-06 ENGINE

LINKSSLEEVESAFT SECONDARY

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON).

18

STRUCTURE

545180-04-07 ENGINE

LINKSSLEEVESAFT SECONDARYSTRUCTURE

SPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON)

15

N

545180-04-09 ENGINE

LINKSSLEEVESAFT SECONDARYSTRUCTURE

SPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON)

1

N 545180-04-10 ENGINE

LINKSSLEEVESAFT SECONDARYSTRUCTURE

SPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON)

1

N 551008-01-04 312AR

313AL

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

551016-01-02 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZER 

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

39

N 551024-01-04 331 / 341BT, AT 

333 / 343AT, AB

GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER LATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3 AND 4.

15

571102-01-01 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

17

571102-01-02 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

2

10

571102-01-03 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

15

571102-01-04 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571102-01-05 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

27

571102-01-06 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

2

11

571102-01-07 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

27

571102-01-08 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

27

N 571102-01-09 821

NOTE 1LININGAIR CONDITIONING DUCTS

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

1

571103-01-03 191HB 192HB 821

NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-03.

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571103-01-04 191HB 192HB 821

NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-04.

17

571103-01-05 191HB 192HB 821

NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-05

14

R 571103-01-06 191HB 192HB 821

NOTE 1

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF 

1

LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)

,

FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-06.

4

571103-02-03 821

NOTE 1LININGAIR CONDITIONING DUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-03

14

571103-02-04 821

NOTE 1LININGAIR CONDITIONING DUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-04.

17

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571103-02-05 821

NOTE 1LININGAIR CONDITIONING DUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-05

14

R 571103-02-06 821

NOTE 1LININGAIR CONDITIONING DUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-06.

14

571104-01-01 191KB 192PB

FASTENER TO BE REMOVED

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF 

2

821131CX 131DX 132CX 132DX 

,

FASTENER BETWEEN STR 38 AND STR 39, LH/RH. 84

571104-01-02 191KB 192PB

FASTENER TO BE REMOVED821131CX 131DX 132CX 132DX 

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

14

571104-01-03 191KB 192PB

FASTENER TO BE REMOVED821131CX 131DX 132CX 132DX 

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

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571104-01-04 191KB 192PB

FASTENER TO BE REMOVED821131CX 131DX 132CX 132DX 

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

19

571104-01-05 191KB 192PB

FASTENER TO BE REMOVED821131CX 131DX 132CX 132DX 

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

26

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

LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN 

3

,

STRINGERS 20 & 21, LH/RH. 15

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

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

3

11

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

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

28

571107-01-05 191QB 192QB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

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

3

15

571108-01-04 147AZ 148AZ 734

744

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

4

12

571108-01-05 147AZ 148AZ 734

744

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

3

11

571108-01-06 147AZ 148AZ 734

744

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

3

17

571108-01-07 147AZ 148AZ 734

744

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

3

11

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571110-01-01 821

NOTE 1LININGAIR CONDITIONING DUCTS

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 40 FRONT FITTING FLANGE REINFORCING STRAP, 4 FASTENER HOLES AT STR. 38 LEVEL, LH/RH.

27

571114-01-05 147AZ 148AZ 734

744

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

39

571114-01-06 147AZ 148AZ 734

744

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

2

11

571114-01-07 147AZ 148AZ 734 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 2

744 INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 

AND 28.

7

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

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

3

15

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

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

3

11

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

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

28

571116-01-05 193DB SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

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

3

15

571118-01-06 FAIRING PANELS BETWEEN 

FR.44 AND FR.47

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

3

15

571118-01-07 FAIRING PANELS BETWEEN 

FR.44 AND FR.47

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571118-01-08 FAIRING PANELS BETWEEN 

FR.44 AND FR.47

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

3

11

571118-01-09 FAIRING PANELS BETWEEN 

FR.44 AND FR.4

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

3

15

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

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

3

11

N 571123-01-01 CABIN FLOOR PANELS

NOTE 1

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

28

N 571123-01-02 CABIN FLOOR PANELS

NOTE 1

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

27

N 571123-01-03 CABIN FLOOR PANELS

NOTE 1

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

19

571125-01-03 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 

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

28

571125-01-04 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 

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

2

10

571125-01-05 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 

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

27

571126-01-03 734 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR 

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

39

571126-01-04 734 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR 

SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE 

2

LOWER CORNER. 12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571126-01-05 734 SPECIAL DETAILED INSPECTION OF CENT WING BOX, REAR 

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

28

571129-01-04 147AZ 148AZ 734

744

DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES).

39

571130-01-03 147AZ 148AZ 734

744

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2 PLACES).

39

571144-01-01 191HB 191QB 192HB

192QB

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, LOWER SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACH SIDE OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25 TO 29 FOR INBOARD RIVET ROW, AND AT STR.11, STR.14, STR.18 TO 20 AND STR.23 TO 28 FOR OUTBOARD RIVET ROW, LH/RH.

3

11

571145-01-01 147AZ 148AZ 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX 3

SEALANT TO BE REMOVED INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD 

FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.

9

571145-01-03 147AZ 148AZ 734 744

SEALANT TO BE REMOVED

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.

3

15

571145-01-04 147AZ 148AZ 734 744

SEALANT TO BE REMOVED

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 

STR.21 AND STR.25 TO 29, LH/RH.

39

571145-01-05 147AZ 148AZ 734 744

SEALANT TO BE REMOVED

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.

2

13

571145-01-06 147AZ 148AZ 734 744

SEALANT TO BE REMOVED

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 

STR.21 AND STR.25 TO 29, LH/RH.

3

10

N 571145-01-07 147AZ 148AZ 734 744

SEALANT TO BE REMOVED

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARD FLANGE, FASTENERS IN RADIUS AREA AT STR.16, STR.20, 

STR.21 AND STR.25 TO 29, LH/RH.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571146-02-04 191QB 192QB

191HB 192HB

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

39

571146-02-05 191QB 192QB

191HB 192HB

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

2

13

571146-02-06 191QB 192QB

191HB 192HB

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

39

571146-02-07 191QB 192QB

191HB 192HB

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

2

13

,

571146-02-08 191QB 192QB

191HB 192HB

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

39

N 571146-02-09 191QB 192QB

191HB 192HB

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

3

571152-01-02 147AZ 148AZ 734

744

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

26

571153-01-01 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

26

571153-01-02 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

19

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571153-01-03 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

13

571153-01-04 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

15

571153-01-05 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

15

, 

571153-01-06 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

17

N 571153-01-07 147AZ 148AZ 

734 744SEALANT TO BE REMOVED

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

1

571159-01-03 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

PORTAL BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).

27

571159-01-04 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

PORTAL BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).

2

13

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

571159-01-05 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WING BOX 

PORTAL BEAMS AT CONNECTION WITH FRONT SPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).

28

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

TWO FASTENERS HOLES IN CONNECTION OF KEEL BEAM FITTING TO CWB BOTTOM PANEL AT STR.1 LEVEL, LH/RH.

13

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

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

13

N 571164-01-01 191HB 192HB DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, KEEL BEAM FITTING ANGLE AND DOUBLER AT FR 40, LH/RH.

1

571165-01-03 734 744 SPECIAL DETAILED INSPECTION OF CENTER WING BOX REAR 

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

13

572001-02-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON REINFORCING.

2

12

572001-02-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON REINFORCING.

39

572001-02-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREA COVERED BY PYLON FAIRING AND PYLON REINFORCING.

28

572003-01-04 454BL 454BR 454CL

454CR 464BL 464BR464CL 464CR

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE

2

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572003-01-06 454BL 454BR 454CL

454CR 464BL 464BR464CL 464CR

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE

39

572003-01-07 454BL 454BR 454CL

454CR 464BL 464BR464CL 464CR

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE VISIBLE PORTION OF PYLON REINFORCING PLATE

28

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

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

17

572004-02-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

3

10

572004-02-04 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

15

572004-02-05 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

15

572005-01-08 541BB 541CB 641BB

641CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR SPAR.

3

11

572005-01-09 541CB 641CB SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAIN LANDING GEAR REINFORCING PLATE INCLUDING ATTACHMENT TO REAR SPAR.

3

11

572006-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.

15

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572006-01-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.

13

572006-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.

13

572006-02-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.

15

572007-01-04 454GL 454GR 464GL

464GR 531AB 631AB

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

17

572007-01-05 454GL 454GR 464GL

464GR 531AB 631AB

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

3

10

572007-01-06 454GL 454GR 464GL

464GR 531AB 631AB

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

15

572007-01-08 454GL 454GR 464GL

464GR 531AB 631AB

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

15

572008-01-04 531AB 631AB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE FORWARD OF REAR SPAR IN AREA COVERED BY FLAP TRACK 2 FAIRING.

3

11

572010-02-04 541AB 541BB 541CB

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

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

3

16

572010-02-06 541AB 541BB 541CB

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

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

3

11

572010-02-07 541AB 541BB 541CB

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

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

3

11

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572012-02-01 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

2

11

572012-02-02 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

28

572012-02-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

28

572012-02-04 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 2

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

7

572013-03-01 454BL 454BR 454CL

454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HR

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

3

14

572013-03-02 454BL 454BR 454CL

454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HR

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

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572013-03-03 454BL 454BR 454CL

454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HR

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

3

10

572013-03-04 454BL 454BR 454CL

454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HR

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

39

572014-02-02 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

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

3

11

572015-02-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

2

11

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

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

39

572015-02-03 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

39

572015-02-04 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

27

572016-02-04 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

2

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

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

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

28

572016-02-06 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

27

572016-02-07 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

27

N 572016-02-12 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

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

28

572018-01-05 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

2

12

641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

572018-01-06 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

28

572018-01-07 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

3

11

572018-01-08 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572018-01-09 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

2

10

572018-01-10 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

3

14

572018-01-11 541AB 541AZ 541BB

541BZ 541CB 541CZ

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING 

2

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

,

STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

8

572018-01-12 541AB 541AZ 541BB

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

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 & 20.

28

572019-01-05 541EB 541FB 541GB

641EB 641FB 641GB

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

 2

12

572019-01-06 541EB 541FB 541GB

641EB 641FB 641GB

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

28

572019-01-07 541EB 541FB 541GB

641EB 641FB 641GB

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

38

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572019-01-08 541EB 541FB 541GB

641EB 641FB 641GB

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

38

572019-01-09 541EB 541FB 541GB

641EB 641FB 641GB

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

2

12

572019-01-10 541EB 541FB 541GB

641EB 641FB 641GB

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

2

12

572019-01-11 541EB 541FB 541GB

641EB 641FB 641GB

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

28

572019-01-12 541EB 541FB 541GB

641EB 641FB 641GB

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

28

572021-03-02 454FL 454FR 454GL

454GR 464FL 464FR464GL 464GR 531AB631AB

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

3

11

D 572022-01-04 TASK DELETED IN ISSUE 17D 572022-01-05 TASK DELETED IN ISSUE 17D 572022-01-06 TASK DELETED IN ISSUE 17D 572022-01-07 TASK DELETED IN ISSUE 17

572023-02-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 

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

2

12

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

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572023-02-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 

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

28

572023-02-06 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN AT 

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

28

572027-01-5 541AB 541AZ 541BB

541BZ 541CB 541CZ541DB 541DZ 541EZ

541FZ 641AB 641AZ

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

3

16

541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ

572027-01-06 541AB 541AZ 541BB

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

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN 

RIB 1 AND RIB 9.

3

11

572027-01-10 541AB 541AZ 541BB

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

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

3

11

572029-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

18

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

SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1 

AND RIB 12

26

AND RIB 12. 6

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572029-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

25

572029-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

15

572030-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

29

572030-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

14

572030-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

15

572030-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

26

572030-01-08 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

26

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

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

3

14

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

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

14

572032-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

27

572032-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

28

572032-01-08 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 

2

AND RIB 7. 8

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572032-01-09 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

2

10

572032-01-10 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

2

10

572032-01-11 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

27

572033-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

17

572033-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

28

572033-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 38

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

11

572033-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

10

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

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

17

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

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

14

572034-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

15

572034-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

14

AND 13.

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572035-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

16

572035-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

14

572035-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

14

572035-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

13

572036-01-04 541AB 541AZ 541BZ

641AB 641AZ 641BZ

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

2

10

572036-01-05 541AB 541AZ 541BZ DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER 2

641AB 641AZ 641BZ CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REAR 

SPARS.

7

572036-01-06 541AB 541AZ 541BZ

641AB 641AZ 641BZ

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

26

572036-01-07 541AB 541AZ 541BZ

641AB 641AZ 641BZ

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

26

R 572039-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

15

572039-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

10

572039-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

11

572039-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

10

R 572040-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

2

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572040-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

38

572040-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

3

10

572040-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

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

39

572043-01-04 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 9.

3

14

572043-01-05 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 9.

27

572043-01-06 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 33

FACE SPAR JOINT PLATE AT RIB 9. 

10

572043-01-07 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 9.

29

572046-01-04 541AB 541BB 541CB

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

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

2

10

572046-01-05 541AB 541BB 541CB

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

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

15

572046-01-06 541AB 541BB 541CB

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

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

16

572046-01-07 541AB 541BB 541CB

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

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

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572046-01-08 541AB 541BB 541CB

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

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

28

572046-01-09 541AB 541BB 541CB

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

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

2

13

572046-01-10 541AB 541BB 541CB

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

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

2

13

572046-01-11 541AB 541BB 541CB

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

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

26

572046-01-12 541AB 541BB 541CB

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

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

27

N 572046-01-13 541AB 541BB 541CB

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

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

26

572047-01-03 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

18

572047-01-04 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572047-01-05 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

16

572047-01-06 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

39

572047-01-07 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZ

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET 

3

10

SEALANT REMOVAL ASPER NTM.

)

BETWEEN RIB 1 AND RIB 7.

R 572047-01-08 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

2

16

R 572047-01-09 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

2

15

572047-01-10 541AB 541BB 541BZ

541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.

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

15

R 572048-01-01 541DB 541EB 

641DB 641EB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.

3

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 572048-01-02 541DB 541EB 

641DB 641EB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.

27

R 572048-01-03 541DB 541EB 

641DB 641EB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.

3

10

R 572048-01-04 541DB 541EB 

641DB 641EB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.

29

R 572049-01-04 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.

3

14

572049-01-05 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.

27

R 572049-01-06 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 33

UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. 

10

572049-01-07 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.

29

572050-01-04 573DB 673DB

DEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

29

572050-01-05 573DB 673DB

DEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

15

572050-01-06 573DB 673DB

DEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

28

572050-01-07 573DB 673DB

DEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

27

572050-01-08 573DB 673DB

DEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.

27

572051-01-05 DEPLOY FLAPS

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.

17

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572051-01-06 DEPLOY FLAPS

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.

3

10

572051-01-07 DEPLOY FLAPS

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.

15

572051-01-08 DEPLOY FLAPS

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.

15

572051-01-09 DEPLOY FLAPS

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.

15

572052-03-01 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

29

572052-03-02 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

15

572052-03-04 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

28

572052-03-05 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

27

572052-03-06 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572052-03-07 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

27

572052-03-08 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

2

11

572052-03-09 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

2

11

N 572052-03-10 541BB 541CB 641BB

641CBSEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE.

28

572054-01-05 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

29

572054-01-06 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

14

572054-01-08 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

28

572054-01-09 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

28

572054-01-10 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

2

14

572054-01-11 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572054-01-12 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

2

14

572054-01-13 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

39

572054-01-14 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

15

N 572054-01-15 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.

28

572063-01-05 541AB 541BB 541CB

541DB 541EB 541FB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 

3

641AB 641BB 641CB641DB 641EB 641FB

12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

15

572063-01-06 541AB 541BB 541CB

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

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

28

572063-01-07 541AB 541BB 541CB

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

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

3

12

572063-01-08 541AB 541BB 541CB

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

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

3

11

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572063-01-10 541AB 541BB 541CB

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

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

3

19

572063-01-11 541AB 541BB 541CB

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

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND 12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OF FORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIB BAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.

3

11

572064-01-05 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

2

11

572064-01-06 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 13

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

4

572064-01-07 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

39

572064-01-08 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

39

572064-01-09 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

2

15

572064-01-10 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

2

15

572064-01-11 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

16

572064-01-12 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES.

27

N 572064-01-13 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 

FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND 

2

BOTTOM FLANGES. 7

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572065-01-04 522DB 522EB 622DB

622EB

DETAILED INSPECTION OF OUTER WING FRONT SPAR FORWARD FACE AND SPAR JOINT PLATE AT RIB 12.

3

10

572066-01-05 N/A SPECIAL DETAILED INSPECTION OF OUTER WING FRONT 

SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12.

3

10

572067-01-05 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

3

10

R 572067-01-06 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

26

N 572067-01-15 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 6 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

26

572068-01-05 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

9

2

572068-01-06 541CB 541DB 541EZ

541FZ 641CB 641DB641EZ 641FZ

DETAILED INSPECTION OF OUTER WING RIB 7 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

15

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572069-01-04 541DB 541FZ 641DB

641FZ

DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

3

17

572069-01-05 541DB 541FZ 641DB

641FZ

DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

28

572069-01-06 541DB 541FZ 641DB

641FZ

DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

28

572069-01-08 541DB 541FZ 641DB DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9 34

641FZ FORWARD AND AFT OF CENTER SPAR AT SKIN 

ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

9

R 572069-01-11 541DB 541FZ 641DB

641FZ

DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

3

12

R 572069-01-12 541DB 541FZ 641DB

641FZ

DETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

3

19

572071-01-06 541AB 541AZ 541BB

541BZ 541CZ 541DZ541EZ 641AB 641AZ641BB 641BZ 641CZ641DZ 641EZ

DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING.

39

572071-01-07 541AB 541AZ 541BB

541BZ 541CZ 541DZ541EZ 641AB 641AZ641BB 641BZ 641CZ641DZ 641EZ

DETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND 5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS, ACCESS CUTOUT SURROUNDS AND AREA OF MANHOLE BOLTING.

39

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572073-01-05 541FB 541GB 641FB

641GB

DETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB 11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OF STRINGER CUTOUTS AND ACCESS CUTOUT SURROUNDS.

39

572081-01-05 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. 

29

572081-01-06 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

15

572081-01-07 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

26

572081-01-08 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

27

572081-01-10 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

26

572081-01-14 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

3

20

N 572081-01-15 541AB 541AZ 641AB

641AZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.

39

572082-01-05 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

2

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572082-01-06 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

29

572082-01-07 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

29

572082-01-08 541AB 541AZ 541BB

541CB 541DB 541DZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES 

2

541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

8

R 572082-01-09 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

28

R 572082-01-10 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

2

14

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572082-01-11 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

2

14

572082-01-12 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

15

572082-01-13 541AB 541AZ 541BB

541CB 541DB 541DZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES 

2

541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

6

N 572082-01-14 541AB 541AZ 541BB

541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZ

DETAILED INSPECTION OF OUTER WING CENTER SPAR BETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES COMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREA AROUND ACCESS HOLES, DRAIN AND VENT HOLES AND CONDUIT HOLES.

15

572084-01-01 541AB 641AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.

38

572084-01-03 541AB 641AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 

AND AT STR. 23 TO 28 LH/RH.

2

10

572084-01-04 541AB 641AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 

27

AND AT STR. 23 TO 28 LH/RH.

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572084-01-05 541AB 641AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.

2

10

572084-01-06 541AB 641AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR. 14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.

29

N 572084-01-07 541 AB, 641 AB,

SEALANT REMOVAL AS PER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING BOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTING OUTBOARD FLANGE IN RADIUS AREA AT STR.11, STR.14, STR.18 TO 20 AND AT STR.23 TO 28, LH/RH.

2

572090-01-01 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.

2

12

NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-01

572090-01-03 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-03

39

572090-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-02-04

28

R 572090-02-01 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-01

2

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572090-02-03 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-03

39

572090-02-04 N/A SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572090-01-04

28

572093-01-06 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME 

2

13

AS TASK 572093-02-06.

572093-01-07 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-07

3

11

572093-01-09 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-09.

38

572093-01-10 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-10.

38

572093-01-13 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-13

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572093-01-14 541FB 641FB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT 

OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-02-14

3

14

572093-02-06 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-06.

2

13

572093-02-07 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-07

3

11

572093-02-09 541FB 641FB SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM 3

SEALANT REMOVAL AS PER NTM

SKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-09.

9

572093-02-10 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-10.

38

572093-02-13 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-14

3

10

572093-02-14 541FB 641FB

SEALANT REMOVAL AS PER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572093-01-13

3

14

572094-01-05 541EB 541FB 541GB

641EB 641FB 641GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 AND RIB 12.

3

16

572094-01-06 541EB 541FB 541GB

641EB 641FB 641GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN 

3

RIB 9 AND RIB 12. 9

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572094-01-10 541EB 541FB 541GB

641EB 641FB 641GB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 9 AND RIB 12.

3

11

572095-01-05 541BB 541CB 641BB

641CB.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

2

12

572095-01-06 541BB 541CB 641BB

641CB.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

28

572095-01-07 541BB 541CB 641BB

641CB.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

28

572095-01-08 541BB 541CB 641BB

641CB.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.

28

572101-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 32

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

14

572101-01-06 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

3

10

572101-01-07 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

39

572104-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND RIB 39.

3

14

572104-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND RIB 39.

39

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572104-01-06 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND RIB 39.

3

10

572104-01-07 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREAS COVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS AT RIB 27 AND RIB 39.

39

572108-02-04 532AB 533AB 534AB

541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND 

ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 

27.

3

16

632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

572108-02-06 532AB 533AB 534AB

541GB 541HB 541JB541KB 541MB 541NB541PB 541QB 541RB541SB 542AB 542BB542CB 542DB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND 

ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 

27.

3

11

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572108-02-07 532AB 533AB 534AB

541GB 541HB 541JB541KB 541MB 541NB541PB 541QB 541RB541SB 542AB 542BB542CB 542DB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER MATING SURFACES AROUND 

ACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND 

27.

3

11

572109-02-05 542EB 542FB 542GB

542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.

39

642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB

572110-01-04 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

2

10

572110-01-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

26

572110-01-06 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

27

572110-01-07 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

26

572111-01-04 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

2

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572111-01-05 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

26

572111-01-06 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

27

572111-01-07 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5.

26

572116-02-02 N/A GENERAL VISUAL INSPECTION OF OUTER WING BOTTOM 

SKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 13 AND STRINGER 20 BETWEEN RIB 12 AND RIB 27 EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 4 

3

11

,

& 5.

572117-01-05 532AB 532CB 533AB

533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBFAIRING ATTMT BRACKET.

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13 AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.

3

11

N 572119-02-10 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT DRAIN HOLES FOR SLAT CANS, MLI HOLES AND DRAIN HOLES AFT OF FRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIBS 12 AND 23.

28

572121-01-04 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

29

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572121-01-05 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

26

572121-01-06 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

3

10

572121-01-07 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

26

572121-01-08 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

2

13

572121-01-09 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDING STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 AND 20.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572122-01-04 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY 26-28 AND STRINGERS 15 & 18.

29

572122-01-05 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY 26-28 AND STRINGERS 15 & 18.

26

650BB 650CB 650DB650EB 650FB

572122-01-06 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY 26-28 AND STRINGERS 15 & 18.

27

572122-01-07 542AB 542BB 542CB

542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY 26-28 AND STRINGERS 15 & 18.

26

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572125-01-06 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-04.

2

12

572125-01-07 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-05.

3

10

572125-01-08 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.

39

NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-06.

572125-01-09 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-07.

28

572125-02-04 542DB 542EB 642DB

642EBSEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-06.

2

12

572125-02-05 542DB 542EB 642DB

642EBSEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-07.

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572125-02-06 542DB 542EB 642DB

642EBSEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-08.

39

572125-02-07 542DB 542EB 642DB

642EBSEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-09.

28

572129-01-03 541SB 641SB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME 

26

AS TASK 572129-02-03. 

572129-02-03 541SB 641SB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-01-03.

26

572130-01-03 542AB 642AB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-02-03.

26

572130-02-03 542AB 642AB

SEALANT REMOVAL ASPER NTM

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572130-01-03.

26

R 572131-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

2

13

572131-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

39

572131-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR 

3

BETWEEN RIB 12 AND RIB 27. 10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572131-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR BETWEEN RIB 12 AND RIB 27.

39

572133-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

3

15

572133-01-05 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

3

10

572133-01-07 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN UPPER 

SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR.

3

11

572138-01-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN JOINT AREA.

39

572138-01-07 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 34

UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN JOINT AREA.

10

572138-01-09 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN JOINT AREA.

3

14

572138-01-10 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKIN JOINT AREA.

3

11

572139-01-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

39

572139-01-07 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

3

10

572139-01-09 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

3

14

572139-01-10 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.

3

11

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572140-01-04 541EB 541FB 541GB

541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.

3

16

572140-01-05 541EB 541FB 541GB

541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.

3

10

641NB 641PB 641QB641RB 641SB

N 572140-01-10 541EB 541FB 541GB

541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDING BUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.

39

572141-01-04 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24.

3

16

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572141-01-05 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24.

39

572141-01-08 542AB 542BB 542CB

542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDING BUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUT IN RIB BAY 23-24.

3

11

550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB

572144-01-05 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

39

572144-01-07 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

3

10

572144-01-09 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

3

14

572144-01-10 542EB 642EB DETAILED INSPECTION OF OUTER WING TOP SKIN LOWER 

SURFACE AT CHORDWISE JOINT AT RIB 27.

3

11

572148-01-04 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

2

12

572148-01-05 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572148-01-06 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

39

572148-01-07 542DB 542EB 642DB

642EB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.

28

572153-01-04 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 27.

3

14

572153-01-05 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 27.

27

572153-01-06 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 27.

3

10

572153-01-08 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 28

FACE SPAR JOINT PLATE AT RIB 27. 

9

R 572153-01-12 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR AFT 

FACE SPAR JOINT PLATE AT RIB 27.

3

21

572154-01-04 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

2

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572154-01-05 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

29

R 572154-01-06 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

28

542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

R 572154-01-07 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 572154-01-08 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

2

14

572154-01-09 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

2

14

542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

572154-01-10 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

29

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572154-01-11 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

39

N 572154-01-13 541FB 541GB 541HB

541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDING TOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING AT RIB 27.

39

542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB

572158-01-05 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23.

3

16

572158-01-06 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23.

39

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572158-01-10 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23.

3

11

572159-01-04 542AB 542BB 542CB

642AB 642BB 642CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26.

3

16

572159-01-05 542AB 542BB 542CB

642AB 642BB 642CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 26.

39

572159-01-09 542AB 542BB 542CB

642AB 642BB 642CB

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 BETWEEN RIB 23 AND RIB 

3

26. 11

572162-01-05 523CB 623CB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

FORWARD FACE SPAR JOINT PLATE AT RIB 27.

3

10

572164-01-05 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

2

12

572164-01-06 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572164-01-07 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

29

572164-01-09 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

29

641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

572164-01-11 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

3

17

572164-01-12 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES.

3

10

D 572166-01-05 TASK DELETED IN ISSUE 17

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572180-01-04 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

29

572180-01-05 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

26

572180-01-06 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

27

572180-01-07 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

27

572180-01-08 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572180-01-09 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

29

572180-01-10 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

29

572180-01-11 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

26

N 572180-01-12 541GB 541HB 541JB

541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.

28

572181-01-04 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

29

572181-01-05 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

26

572181-01-06 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

2

7

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572181-01-07 542AB 542BB 542CB

642AB 642BB 642CB

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.

26

572184-01-04 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-04.

29

572184-01-05 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-05.

26

572184-01-06 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.

27

NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-06.

572184-01-07 541QB 641QB DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-02-07.

26

572184-02-04 541QB 641QB

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-04.

29

572184-02-05 541QB 641QB

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-05.

26

572184-02-06 541QB 641QB

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-06.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

572184-02-07 541QB 641QB

SEALANT REMOVAL ASPER NTM.

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572184-01-07.

26

572185-01-01 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL 

REFUELLING APERTURE IN RIB BAY 22-23

3

16

572185-01-02 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL 

REFUELLING APERTURE IN RIB BAY 22-23

4

12

572185-01-03 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL 

REFUELLING APERTURE IN RIB BAY 22-23.

39

572185-01-04 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN MANUAL 

REFUELLING APERTURE IN RIB BAY 22-23.

2

11

572606-01-03 532CB 533CB 534CB

632CB 633CB 634CB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY.

1

N 572606-01-07 532CB 533CB 534CB

632CB 633CB 634CB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY.

26

N 572607-01-06 531AB 531CB 532AB

532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CB

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.

26

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

573001-01-05 535AZ 535BZ 635AZ

635BZ

DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.

2

11

573001-01-07 535AZ 535BZ 635AZ

635BZ

DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.

39

573001-01-08 535AZ 535BZ 635AZ

635BZ

DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.

29

573001-01-10 535AZ 535BZ 635AZ

635BZ

DETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT AND REAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.

29

573002-01-05 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER 

SURFACE AND BOTTOM SKIN LOWER SURFACE.

2

11

573002-01-07 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER 

SURFACE AND BOTTOM SKIN LOWER SURFACE.

39

573002-01-08 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER 

SURFACE AND BOTTOM SKIN LOWER SURFACE.

29

573002-01-09 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN UPPER 

SURFACE AND BOTTOM SKIN LOWER SURFACE.

29

573003-02-04 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

3

14

573003-02-05 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

3

11

573003-02-06 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 573003-02-07 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

16

R 573003-02-08 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

19

573003-02-09 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

2

16

573003-02-10 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

3

10

N 573003-02-12 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLET 

FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).

14

574106-01-04 521BB 521CB 521DB DETAILED INSPECTION OF OUTER WING FIXED LEADING 2

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

12

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574106-01-05 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

28

622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

574106-01-06 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

28

623FB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574106-01-08 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

28

622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

574106-01-11 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

3

19

623FB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574106-01-12 521BB 521CB 521DB

521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16.

3

12

622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB

R 574107-02-04 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522KB 522LB522MB 522NB 522PB522QB 522RB 522SB523CB 523DB 523EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

3

17

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574107-02-05 521FB 521GB 521HB

521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522KB 522LB522MB 522NB 522PB522QB 522RB 522SB523CB 523DB 523EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB

SPECIAL DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACK RIB 12.

3

10

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-01 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

17

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-02 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

15

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-03 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

26

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-04 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

26

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-05 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

1

10

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-06 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

1

10

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-07 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

16

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574109-02-08 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

16

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 574109-02-09 521AB 521BB 521CB

521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622AB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDING CLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWN RIBS.

15

622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PB

R 574114-03-01 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.

2

12

574114-03-02 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.

3

11

574114-03-03 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.

39

574114-03-04 N/A DETAILED INSPECTION OF OUTER WING FIXED LEADING 

EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.

28

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

574115-02-01 522AB 522BB 522CB

622AB 622BB 622CB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11.

17

574115-02-02 522AB 522BB 522CB

622AB 622BB 622CB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11.

15

574115-02-03 522AB 522BB 522CB

622AB 622BB 622CB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11.

15

574115-02-05 522AB 522BB 522CB

622AB 622BB 622CB

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARD OF FRONT SPAR BETWEEN RIBS 9 AND 11.

15

R 575011-01-04 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

3

15

575011-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 16

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

4

R 575011-01-06 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

3

11

575011-01-07 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

38

575011-01-08 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

38

575011-01-09 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

2

11

575011-01-10 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

2

11

R 575011-01-11 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14.

3

10

N 575011-01-12 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 

SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 

2

AND RIB 14. 85

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575012-01-10 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

3

10

575012-01-11 N/A DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.

3

13

575016-01-04 531AB 631AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING.

3

16

575016-01-06 531AB 631AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING.

3

11

575016-01-08 531AB 631AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING.

3

11

575017-01-04 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR RIB 6.

3

16

575017-01-06 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR RIB 6.

3

11

575017-01-07 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT, INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUST OUTBOARD OF GEAR RIB 6.

3

11

575018-01-03 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

2

10

575018-01-04 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

26

575018-01-05 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

2

7

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575018-01-06 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

28

R 575018-01-07 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

26

R 575018-01-08 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

1

10

575018-01-09 147AT 148AT 191CT

192CTDEPLOY FLAPS

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

2

11

575018-01-10 147AT 148AT 191CT

192CT

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX.

2

DEPLOY FLAPS 7

575022-01-01 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

15

575022-01-02 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

14

575022-01-03 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575022-01-04 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

17

575022-01-05 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

14

575022-01-06 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO 

1

, 

REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

4

575022-01-07 575AB 575BB 675AB

675BB

DETAILED INSPECTION OF OUTER WING TRAILING EDGE INBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST AND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

14

575023-01-07 575CB 575DB 675CB 675DB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

OUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENT TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOST TO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.

3

13

575025-01-04 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

3

15

575025-01-05 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

27

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575025-01-06 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

3

11

575025-01-07 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

38

575025-01-08 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

29

575025-01-09 532AB 632AB DETAILED INSPECTION OF OUTER WING TRAILING EDGE 

BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROM RIB 8 TO RIB 12.

3

10

575051-01-01 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS.

1

575051-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS.

1

575053-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO 1, DRIVE LINK, DRIVE LEVER, DRIVE STRUT AND CARRIAGE.

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575054-01-01 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOX SUPPORT, FORK ASSY, DRIVE STRUT AND CARRIAGE.

1

575054-01-02 734 744

FLAPS EXTENDED

DETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOX SUPPORT, FORK ASSY, DRIVE STRUT AND CARRIAGE.

1

, , 

575055-01-02 734 744 DETAILED INSPECTION OF FLAP TRACK NO 1, ATTACHMENTS 

TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.

1

575055-01-03 734 744 DETAILED INSPECTION OF FLAP TRACK NO 1, ATTACHMENTS 

TO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDING SUPPORT STRUTS WITH ATTACHMENT FITTING.

1

R

575057-01-02 FLAPS EXTENDED

AFT TRACK FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 5, UPPER FLANGES RADII.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R

575059-01-02 FLAPS EXTENDED

AFT FLAP TRACKFAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO 2, 3, 4 AND 5, DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDE 

ATTACHMENT FITTINGS AND AFT SUPPORT LINK AND TRAVELLING BEAM AT TRACK NO 4.

2

575061-01-02 FLAPS EXTENDED

FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, CARRIAGE ASSEMBLIES.

2

575061-01-03 FLAPS EXTENDED

FAIRINGS

DETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5, CARRIAGE ASSEMBLIES.

2

R 575063-01-01 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND 

5 LOWER FLANGES, STRAP AND ANGLES.

2

575067-01-02 FWD FLAP TRACK

FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-02-02.

2

575067-01-03 FWD FLAP TRACK

FAIRINGS

DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-02-03.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575067-02-02 FWD FLAP TRACK

FAIRINGSFAIL SAFE BOLT

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-01-02.

2

575067-02-03 FWD FLAP TRACK

FAIRINGSFAIL SAFE BOLT

SPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575067-01-03.

2

575069-01-02 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 

5, AFT ATTACHMENT SPIGOTS.

2

, 

575069-01-03 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND 

5, AFT ATTACHMENT SPIGOTS.

2

R 575401-01-02 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNAL 

SURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TASK TO 575401-02-01.

3

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575401-02-01 FLAPS EXTENDED DETAILED INSPECTION OF INBOARD FLAP, EXTERNAL 

SURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TASK TO 575401-01-02.

5

R 575402-01-01 FLAPS EXTENDED SPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN AND 

DOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT 

1

TRACK 2, LH/RH. 

575403-01-02 581AB 681AB 734

744

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-02-02.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575403-01-03 581AB 681AB 734

744

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-02-03.

2

575403-02-02 581AB 681AB 734

744

SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-01-02.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

575403-02-03 581AB 681AB 734

744

SPECIAL DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION, INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575403-01-03.

2

575405-01-02 531AT 531CB 631AT

631CBFLAPS EXTENDED

DETAILED INSPECTION OF INBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 2 AND EXTERNAL DRIVE STRUT BRACKET, CARRIAGE ATTACHMENT BRACKET AND GUIDE ARM ATTACHMENT BRACKET.

2

R 575503-01-02 532AT 532CB 632AT

632CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3, AND EXTERNAL DRIVE STRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575503-02-02.

2

R 575503-02-02 532AT 532CB 632AT

632CBFLAPS EXTENDEDSPEED TAPE

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 3.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575503-01-02.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 575505-01-02 533AT 533CB 633AT

633CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 4, AND EXTERNAL FWD SUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575505-02-02.

2

R 575505-02-02 533AT 533CB 633AT

633CBFLAPS EXTENDEDSPEED TAPE

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 4.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575505-01-02.

2

R 575507-01-02 534AT 534CB 634AT

634CBFLAPS EXTENDED

DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 5, AND EXTERNAL DRIVE STRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACH FITTING.

2

NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575507-02-02.

R 575507-02-02 534AT 534CB 634AT

634CBFLAPS EXTENDEDSPEED TAPE

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL SUPPORT FITTING AT TRACK NO 5.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575507-01-02.

2

R 575509-01-02 FLAPS EXTENDED

RUBBER SEAL

DETAILED INSPECTION OF OUTBOARD FLAP, INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET, EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575509-02-02.

2

R 575509-02-02 FLAPS EXTENDED

RUBBER SEALSPEED TAPE

SPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INNER END RIB INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT BRACKET, INTERNALNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 575509-01-02.

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

N 576105-01-01 FAIRING

PANEL

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1.

13

N 576108-01-01 FAIRING

PANEL

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.

19

R 576114-02-01 JACK FAIRINGS SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER 

FLANGE OF OUTER JACK FITTING.

2

8

N 576115-01-01 FAIRING

PANEL

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGERADIUS AT LUG SIDE OF HINGE1.

26

N 576117-01-01 FAIRING

PANEL

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACK FITTING.

1

3

N 576118-01-01 FAIRING

PANEL

SPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.

15

R 577003-01-02 SPOILERS DEPLOYED

FLAP DEPLOYED

DETAILED INSPECTION OF SPOILER NO 1, HINGE AND ACTUATOR ATTACHMENT FITTINGS (6 PLACES).

1

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

711141-01-02 415AL 416AR 425AL

426AR

GENERAL VISUAL INSPECTION OF INLET COWL ATTACHMENT (A1 FLANGE).

8

R 711200-01-02 415AL 416AR 425AL

426AR

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

8

R 711246-01-02 415AL 416AR 425AL

426AR

GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

8

R 711301-02-02 415AL 415BL 416AR

416BR 425AL 425BL426AR 426BR

GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

8

R 711302-02-02 415AL 415BL 416AR

416BR 425AL 425BL426AR 426BR

GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

8

711341-02-02 415AL 416AR 425AL

426AR

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

8

711343-02-01 415AL 416AR 425AL

426AR

GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

8

711345-02-01 414AL 414AR 424AL

424AR

GENERAL VISUAL INSPECTION OF CORE COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

8

711347-01-01 414AL 414AR 424AL

424AR

GENERAL VISUAL INSPECTION OF CORE COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

8

712102-01-01 417AL 418AR 427AL

428AR

DETAILED INSPECTION OF CF6-80E1 FORWARD ENGINE MOUNT EXCLUDING THE PLATFORM.

4

1

712103-01-01 ENGINE

FORWARD ENGINE MOUNTDISASSEMBLED

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT PLATFORM.

6

6

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

712103-01-02 ENGINE

FORWARD ENGINE MOUNTDISASSEMBLED

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT PLATFORM.

6

6

712104-01-01 417AL 418AR 427AL

428AR

DETAILED INSPECTION OF FORWARD ENGINE MOUNT REAR TRUNNION CLEARANCE HOLE.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH.

27

712105-01-01 ENGINE

FWD ENGINE MOUNTDISASSEMBLED

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT THRUST TRUNNION.

8

2

712106-01-01 ENGINE

FORWARD ENGINE MOUNT

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT.

8

DISASSEMBLED 2

712202-01-01 414AL 414AR 424AL

424AR

DETAILED INSPECTION OF AFT ENGINE MOUNT EXCLUDING THE UPPER BEAM.

8

5

712204-01-01 417AL 418AR 427AL

428AR

DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFE LINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH.

4

1

712204-02-01 417AL 418AR 427AL

428ARENGINEENGINE MOUNT

DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFE LINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH.

8

2

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

AIRWORTHINESS LIMITATION SECTION

A330 

R 783200-01-02 417DL 417EL 418DR

418ER 427DL 427EL428DR 428ER

GENERAL VISUAL INSPECTION OF THRUST RESERVER HINGES, SLEEVES, PINS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS).

2

783201-03-01 415BL 416BR 417AL GENERAL VISUAL INSPECTION OF THRUST REVERSER 8

418AR 425BL 426BR427AL 428AR

HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE ATTACHMENTS).

R 783201-04-01 415BL 416BR 417AL

418AR 425BL 426BR427AL 428AR

GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE ATTACHMENTS).

8

783202-01-02 415BL 416BR 417AL

418AR 425BL 426BR427AL 428ARLATCH ACCESS DOOR

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS).

8

R 783202-02-02 415BL 416BR 417AL

418AR 425BL 426BR427AL 428ARLATCH ACCESS DOOR

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS).

8

R 783245-02-01 418HR 418JR 428HR

428JR

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS).

8

ISSUE: 28 May 2010© AIRBUS SAS 2010. ALL RIGHTS RESERVED.

ALI SECTION 2

EASA APPROVED
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-1

©AIRBUS SAS 2010. All rights reserved. 

A330 

1 SUMMARY OF CHANGES

Section 2 AIRWORTHINESS LIMITATIONS:

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

R 521103-01-02 Applicability updated to exclude A330-200F 

R 521201-01-02 Applicability updated to exclude A330-200F 

R 521301-01-02 Applicability updated to exclude A330-200F 

R 522201-01-02 Applicability updated to exclude A330-200F 

N 523104-01-02 New task created 

R 523106-01-01 Applicability updated to exclude A330-200F 

N 523204-01-02 New task created 

R 528203-01-02 Applicability updated to exclude A330-200F 

N 528206-01-01 New task created to cover A330-200F 

N 531106-01-06 New task created to cover A330-200F 

N 531108-01-01 New task created to cover A330-200F 

N 531109-01-01 New task created to cover A330-200F 

R 531110-02-02 Applicability updated to exclude A330-200F 

N 531110-02-03 New task created to cover A330-200F 

R 531112-02-01 Applicability updated to exclude A330-200F 

N 531112-02-02 New task created to cover A330-200F 

R 531118-01-01 Applicability updated to exclude A330-200F 

R 531120-01-02 Applicability updated to exclude A330-200F 

N 531125-02-01 New task created to cover A330-200F 

N 531145-01-01 New task created to cover A330-200F 

N 531148-01-01 New task created to cover A330-200F 

R 531154-01-03 Applicability extended to A330-200F 

N 531155-01-01 New task created to cover A330-200F 

N 531160-01-01 New task created to cover A330-200F 

N 531163-01-01 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-2

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

N 531164-01-01 New task created to cover A330-200F 

N 531169-02-01 New task created to cover A330-200F 

N 531177-01-01 New task created to cover A330-200F 

N 531178-01-01 New task created to cover A330-200F 

N 531179-01-01 New task created to cover A330-200F 

N 531184-01-03 New task created 

R 531192-01-03 Threshold updated 

R 531194-01-03 Threshold updated 

R 532101-01-02 Threshold/Interval updated 

 Applicability updated to exclude A330-200F 

N 532101-02-02 New task created as an alternative to 532101-01-02 

R 532115-01-02 Applicability updated to exclude A330-200F 

R 532117-01-03 Interval updated 

 Applicability updated to exclude A330-200F 

N 532117-02-03 New task created as an alternative to 532117-01-03 

R 532128-01-01 Applicability updated to exclude A330-200F 

R 532138-01-01 Applicability updated to exclude A330-200F 

R 532143-01-02 Applicability updated to exclude A330-200F 

R 532144-01-02 Applicability updated to exclude A330-200F 

R 532146-01-02 Applicability updated to exclude A330-200F 

R 532147-01-02 Applicability updated to exclude A330-200F 

R 532148-01-02 Applicability updated to exclude A330-200F 

R 532149-01-02 Applicability updated to exclude A330-200F 

N 532166-01-03 New task created 

N 532166-02-03 New task created 

N 532182-01-01 New task created to cover A330-200F 

N 532183-01-01 New task created to cover A330-200F 

R 533012-01-01 Description updated to remove the information on the 

number of fasteners 

R 533012-02-01 Description updated to remove the information on the 

number of fasteners 

N 533113-01-10 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-3

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

N 533115-01-09 New task created to cover A330-200F 

R 533125-01-01 Applicability updated to exclude A330-200F 

N 533127-03-04 New task created to cover A330-200F 

N 533164-01-08 New task created to cover A330-200F 

N 533187-01-01 New task created 

N 533187-01-02 New task created 

N 533187-01-03 New task created 

R 533192-01-01 Applicability updated to exclude A330-200F 

R 533193-01-01 Applicability updated to exclude A330-200F 

N 533196-01-01 New task created to cover A330-200F 

R 534124-01-02 Interval reduced 

 Applicability updated to exclude A330-200F 

N 534124-02-02 New task created as an alternative to 534124-01-02 

R 534126-01-02 Threshold/Interval updated 

 Applicability updated to exclude A330-200F 

N 534126-02-02 New task created as an alternative to 534126-01-02 

R 534135-01-01 Applicability updated to exclude A330-200F 

R 534139-01-04 Applicability updated to exclude A330-200F 

R 534140-02-02 Applicability updated to exclude A330-200F 

R 534146-01-02 Applicability updated to exclude A330-200F 

R 534149-01-02 Applicability updated to exclude A330-200F 

R 534150-01-02 Applicability updated to exclude A330-200F 

N 534150-01-03 New task created to cover A330-200F 

R 534154-01-02 Applicability updated to exclude A330-200F 

R 534155-01-02 Applicability updated to exclude A330-200F 

N 534177-01-03 New task created 

N 534177-02-03 New task created 

N 534182-01-01 New task created to cover A330-200F 

N 534184-01-01 New task created to cover A330-200F 

N 545103-02-04 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-4

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

N 545108-04-19 New task created to cover A330-200F 

N 545108-04-20 New task created to cover A330-200F 

R 545140-01-01 Description note updated 

 Applicability extended 

R 545140-01-02 Description note updated 

 Applicability extended 

R 545140-01-03 Description note updated 

 Applicability extended 

R 545140-01-06 Description note updated 

 Applicability extended 

R 545140-01-07 Description note updated 

 Applicability extended 

R 545140-01-08 Description note updated 

 Applicability extended 

R 545140-02-01 Description note updated 

 Applicability extended 

R 545140-02-02 Description note updated 

 Applicability extended 

R 545140-02-03 Description note updated 

 Applicability extended 

R 545140-02-06 Description note updated 

 Applicability extended 

R 545140-02-07 Description note updated 

 Applicability extended 

R 545140-02-08 Description note updated 

 Applicability extended 

N 545140-02-09 New task created 

N 545140-02-10 New task created 

N 545140-02-11 New task created 

N 545140-02-12 New task created 

N 545140-02-13 New task created 

N 545140-02-14 New task created 

N 545140-02-15 New task created to cover A330-200F 

N 545140-02-16 New task created to cover A330-200F 

N 545142-02-11 New task created to cover A330-200F 

N 545142-02-12 New task created to cover A330-200F 

N 545150-02-13 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-5

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

N 545168-02-15 New task created to cover A330-200F 

N 545168-02-16 New task created to cover A330-200F 

N 545174-02-10 New task created to cover A330-200F 

N 545174-02-11 New task created to cover A330-200F 

N 545180-04-09 New task created to cover A330-200F 

N 545180-04-10 New task created to cover A330-200F 

N 551008-01-04 New task created to cover A330-200F 

N 551024-01-04 New task created to cover A330-200F 

N 571102-01-09 New task created to cover A330-200F 

R 571103-01-06 Description updated to correct the note. 

R 571103-02-06 Description updated to correct the note. 

N 571123-01-01 New task created 

N 571123-01-02 New task created 

N 571123-01-03 New task created 

N 571145-01-07 New task created to cover A330-200F 

N 571146-02-09 New task created to cover A330-200F 

N 571153-01-07 New task created to cover A330-200F 

R 571162-01-01 Description updated 

Threshold and Intervals updated 

Applicability updated 

N 571164-01-01 New task created to cover A330-200F 

N 572016-02-12 New task created to cover A330-200F 

D 572022-01-04 Task deleted as it is not applicable to A330 

D 572022-01-05 Task deleted as it is not applicable to A330 

D 572022-01-06 Task deleted as it is not applicable to A330 

D 572022-01-07 Task deleted as it is not applicable to A330 

R 572032-01-04 FH Interval figure updated 

R 572039-01-04 FH Interval figure updated 

R 572040-01-04 FH Interval figure updated 

N 572046-01-13 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-6

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

R 572047-01-08 FH Interval figure updated 

R 572047-01-09 FH Interval figure updated 

R 572048-01-01 Inspection level updated 

R 572048-01-02 Inspection level updated 

R 572048-01-03 Inspection level updated 

R 572048-01-04 Inspection level updated 

R 572049-01-04 FH Interval figure updated 

R 572049-01-06 FH Interval figure updated 

N 572052-03-10 New task created to cover A330-200F 

N 572054-01-15 New task created to cover A330-200F 

N 572064-01-13 New task created to cover A330-200F 

R 572067-01-06 Threshold updated 

Applicability corrected 

N 572067-01-15 New task created 

R 572069-01-11 FH Interval figure updated 

R 572069-01-12 FH Interval figure updated 

N 572081-01-15 New task created to cover A330-200F 

R 572082-01-09 Interval updated 

R 572082-01-10 Interval updated 

N 572082-01-14 New task created to cover A330-200F 

N 572084-01-07 New task created to cover A330-200F 

R 572090-02-01 FH Interval figure updated 

N 572119-02-10 New task created to cover A330-200F 

R 572131-01-04 FH Threshold and Interval figures updated 

N 572140-01-10 New task created to cover A330-200F 

R 572153-01-12 FH Interval figure updated 

R 572154-01-06 FH Interval figure updated 

R 572154-01-07 Interval updated 

R 572154-01-08 Interval updated 

N 572154-01-13 New task created to cover A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-7

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

D 572166-01-05 Task deleted 

N 572180-01-12 New task created to cover A330-200F 

N 572606-01-07 New task created to cover A330-200F 

N 572607-01-06 New task created to cover A330-200F 

R 573003-02-07 Interval updated 

R 573003-02-08 Interval updated 

N 573003-02-12 New task created to cover A330-200F 

R 574107-02-04 FH Interval figure updated 

N 574109-02-09 New task created to cover A330-200F 

R 574114-03-01 FH Interval figure updated 

R 575011-01-04 FH Interval figure updated 

R 575011-01-06 FH Interval figure updated 

R 575011-01-11 FH Interval figure updated 

N 575011-01-12 New task created to cover A330-200F 

R 575018-01-07 Interval updated 

R 575018-01-08 Interval updated 

R 575057-01-02 Applicability updated to exclude A330-200F 

R 575059-01-02 Applicability updated to exclude A330-200F 

R 575063-01-01 Applicability updated to exclude A330-200F 

R 575401-01-02 Applicability updated to exclude A330-200F 

R 575402-01-01 Applicability updated to exclude A330-200F 

R 575503-01-02 Applicability updated to exclude A330-200F 

R 575503-02-02 Applicability updated to exclude A330-200F 

R 575505-01-02 Applicability updated to exclude A330-200F 

R 575505-02-02 Applicability updated to exclude A330-200F 

R 575507-01-02 Applicability updated to exclude A330-200F 

R 575507-02-02 Applicability updated to exclude A330-200F 

R 575509-01-02 Applicability updated to exclude A330-200F 

R 575509-02-02 Applicability updated to exclude A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA-8

©AIRBUS SAS 2010. All rights reserved. 

A330 

REV 

CODE TASK REFERENCE SUMMARY OF CHANGES 

N 576105-01-01 New task created 

N 576108-01-01 New task created 

R 576114-02-01 Applicability updated to exclude A330-200F 

N 576115-01-01 New task created 

N 576117-01-01 New task created 

N 576118-01-01 New task created 

R 577003-01-02 Applicability updated to exclude A330-200F 

R 711200-01-02 Applicability updated to exclude A330-200F 

R 711246-01-02 Applicability updated to exclude A330-200F 

R 711301-02-02 Applicability updated to exclude A330-200F 

R 711302-02-02 Applicability updated to exclude A330-200F 

R 783200-01-02 Applicability updated to exclude A330-200F 

R 783201-04-01 Applicability updated to exclude A330-200F 

R 783202-02-02 Applicability updated to exclude A330-200F 

R 783245-02-01 Applicability updated to exclude A330-200F 
AIRWORTHINESS LIMITATION ITEMS 

APPENDIX B - ABBREVIATIONS

ISSUE: 28 MAY 2010 PAGE: APXB -1 

©AIRBUS SAS 2010. All rights reserved. 

A330 

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: 28 MAY 2010 PAGE: APXC -1 

©AIRBUS SAS 2010. All rights reserved. 

A330 

TERM DEFINITION 

AIRCRAFT 

STRUCTURE 

Consists of all load-carrying members including wings, fuselage, empennage, 

engine mountings, landing gear, flight control surfaces, and related points of 

attachment. The actuating portions of items such as landing gear, flight controls, 

doors, etc. are treated as systems components. Attachment of the actuators to 

the airframe are treated as structure. 

CALENDAR TIME 

(Cal) 

In Years (Ye), in Months (Mo), etc... must be counted from the date of initial 

entry into service, unless otherwise stated. Storage, maintenance, etc... do not 

freeze calendar time accumulation. 

CONTINUED 

AIRWORTHINESS 

Is the process of ensuring that the level of airworthiness guaranteed by TC is 

maintained for each individual aircraft at the time of its entry into service and 

during all its service life. 

DAMAGE 

TOLERANCE 

CONCEPT 

The damage-tolerance evaluation of structure is intended to ensure that should 

serious fatigue, corrosion, or accidental damage occur within the operational life 

of the aeroplane, the remaining structure can withstand reasonable loads without 

failure or excessive structural deformation until the damage is detected. 

Damage-tolerance design is required, unless it entails such complications that an 

effective damage-tolerant structure cannot be achieved within the limitations of 

geometry, inspectability, or good design practice. Under these circumstances, a 

design that complies with the fatigue evaluation (safe life) requirements is used. 

DAMAGETOLERANT 

AIRWORTHINESS 

LIMITATION ITEMS 

(DT ALI) 

They are all those parts of the structure whose failure could result in catastrophic 

failure of the airplane and that are designed to fatigue and damage-tolerance 

concept. 

DESIGN SERVICE 

GOAL Is a reference figure selected for the design and certification of the aircraft. 

EXTENDED 

SERVICE GOAL Is an extension of the DSG. 

FLIGHT CYCLE (FC) A complete take-off and landing sequence 

FLIGHT HOUR (FH) The accumulated time intervals between ‘wheels-off’ and ‘wheels-on’. 

INTERVAL The maximum period expressed in usage parameters between the completion of 

a task and its next due accomplishment. 

LIMIT OF VALIDITY 

(LOV) Is a limitation to the validity of the Airworthiness Limitation Sections 

THRESHOLD 

The maximum period of time expressed in usage parameters between the first 

flight of the aircraft, and the frist due completion of the task. 

Subsequent accomplishment deadlines are obtained by adding the repeat 

interval and its multiples to the threshold. 

TOUCH AND GO A ‘Touch and go’ is a landing in which an aircraft touches the runway and does 

not come to a full stop prior to commencing an additional flight.