Customer Services Directorate 

A330 Airworthiness Limitation Items

A330 

Airworthiness Limitation Items 

© AIRBUS SAS 2012. 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 

23 March 2012 

Issue 19 
A330 Airworthiness Limitation Items

TABLE OF CONTENTS

SUBJECT SECTION

ISSUE: 23 MAR 2012 PAGE: 1-TOC 

©AIRBUS SAS 2012. All rights reserved. 

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
A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 1-ROR 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved. 

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.
A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 2-ROR 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved. 

Issue Date Reason for revision Approved 

by EASA 

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 

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 
A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 3-ROR 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved. 

Issue Date Reason for revision Approved 

by EASA 

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 

18 1st AUG 2011 Task requirements updated due to: 

Fleet survey results 

New approach added with 2 sets of figures for the 

tasks sensitive to the range 

Section 2.2 is created for tasks FH optimized 

Modifications/In-service experience 

Weight variants added 

Approved by 

EASA 

under reference 

10038005 

on 11 January 2012 

19 23 MAR 2012 Correction of errors from Rev 18 

Weight Variant 062 added for Group 32E 

Weight Variant 055 added for Group 33E 

Approved by 

EASA 

under reference 

10040023 

on 08 June 2012 

 
A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 4-ROR 

EASA APPROVED 

AIRBUS SAS 2012. All rights reserved. 

COMPLIANCE TIME:

The compliance time defined in issue 18 for specific tasks mentioned in table 1 remains valid as there

was no threshold nor interval updated between issue 18 and 19.

1. From the 12 January 2014, it is mandatory to comply with the airworthiness limitations as 

defined in the A330 ALI Document revision 19. 

2. From the 11 January 2012 to 11 January 2014, 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 17 

or,

- The ALI Document at issue 19.

3. For the following tasks, it is mandatory to comply with the airworthiness limitations defined in 

table 1 through the following instructions: 

- As per issue 18:

This means that no compliance time is granted. 

Issue 18 is to be applied from 11 January 2012.

- As per issue 17 for 1 year: 

This means that issue 17 can be applied until 11 January 2013 

After this date, issue 18 shall be applied. 

- As per Para 2: 

This means that there is no specific instruction. 

 The conditions defined in paragraph 2 above, apply. 

 TABLE 1 

TASK REFERENCE THRESHOLD INTERVAL 

532124-02-08 As per Issue 18 As per Para 2 

533021-01-01 As per Issue 17 for 1 year As per Para 2 

533021-01-02 As per Issue 17 for 1 year As per Para 2 

533021-01-03 As per Issue 17 for 1 year As per Para 2 

533151-01-01 As per Issue 17 for 1 year As per Para 2 

533151-01-02 As per Issue 17 for 1 year As per Para 2 

533151-01-03 As per Issue 17 for 1 year As per Para 2 

523104-01-02 As per Para 2 As per Issue 17 for 1 year 

531130-01-02 As per Para 2 As per Issue 17 for 1 year 
A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 5-ROR 

EASA APPROVED 

AIRBUS SAS 2012. All rights reserved. 

TABLE 1 

TASK REFERENCE THRESHOLD INTERVAL 

532127-01-01 As per Para 2 As per Issue 17 for 1 year 

532130-01-02 As per Para 2 As per Issue 17 for 1 year 

532155-01-02 As per Para 2 As per Issue 17 for 1 year 

534104-01-08 As per Para 2 As per Issue 17 for 1 year 

534140-02-02 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-01 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-03 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-09 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-11 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-12 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545108-03-14 As per Issue 17 for 1 year As per Issue 17 for 1 year 

545142-02-01 As per Para 2 As per Issue 17 for 1 year 

545142-02-02 As per Para 2 As per Issue 17 for 1 year 

545142-02-05 As per Para 2 As per Issue 17 for 1 year 

545142-02-06 As per Para 2 As per Issue 17 for 1 year 

545142-02-07 As per Para 2 As per Issue 17 for 1 year 

545142-02-08 As per Para 2 As per Issue 17 for 1 year 

545142-02-09 As per Para 2 As per Issue 17 for 1 year 

545142-02-10 As per Para 2 As per Issue 17 for 1 year 

574115-02-01 As per Para 2 As per Issue 17 for 1 year 

574115-02-03 As per Para 2 As per Issue 17 for 1 year 

574115-02-05 As per Para 2 As per Issue 17 for 1 year 
A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 6 

©AIRBUS SAS 2012. All rights reserved. 

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). 
A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 7 

©AIRBUS SAS 2012. All rights reserved. 

1-1-B Section 2-1:

The section 2-1 contains airworthiness limitations arising from fatigue and damage tolerance 

that could be sensitive to the range or not. 

The fatigue tasks sensitive to range are FC optimized and are defined with the following note in 

the description column: 

NOTE: The thresholds/intervals of this maintenance requirement are FC optimized. 

For these tasks, an alternative set of FH optimized requirements is stated in Section 2-2. 

The two sets of figures are applicable to any aircraft defined in the Applicability column. One 

set is FC optimized, providing that the associated FH limit is not exceeded.The other set is FH 

optimized, providing that the associated FC limit is not exceeded. Both sets of data are 

approved and the operator can select whichever set of data is most appropriate. 

1-1-C Section 2-2:

The section 2-2 contains only airworthiness limitations arising from fatigue and damage 

tolerance that are sensitive to the range. 

They are FH optimized and are defined with the following note in the description column: 

NOTE: The thresholds/intervals of this maintenance requirement are FH optimized. 

For these tasks, the alternative set of FC optimized requirements is stated in Section 2-1. 

1-2 RULES FOR COMPLIANCE DEMONSTRATION

1-2-A General

The airworthiness limitations contained in section 2 allow operation up to the Limit of Validity 

(LOV) in FC or FH whichever occurs first. 

The relevant LOV values are stated in paragraph 1-3. 

The LOV reflects the limit of validity of the engineering data that supports the structural 

maintenance program.

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. 
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INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 8 

©AIRBUS SAS 2012. All rights reserved. 

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. 

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, 
A330 Airworthiness Limitation Items

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©AIRBUS SAS 2012. All rights reserved. 

− 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. 

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. 
A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 10 

©AIRBUS SAS 2012. All rights reserved. 

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. 

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, 052,054, 055, 056, 057, 

058, 059, 060, 061, 062 

A330-202 020, 021, 022, 023, 050, 052, 053, 054, 

055, 056, 057, 058, 059, 060, 061, 062 

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

055,056, 057, 058, 059, 060, 061, 062 

A330-223 020, 021, 022, 023, 050, 052, 054, 055, 

056, 057, 058, 059, 060, 062 

A330-243

020, 021, 022, 023, 024, 025, 026, 027, 

050, 052, 054, 055, 056, 057, 058, 059, 

060, 061, 062 

A330-200F 

A330-223F 000, 001, 002 

A330-243F 000, 001, 002 

A330-300 

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

A330-302 050, 052, 053, 054, 055 

A330-303 050, 052, 054, 055 

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, 054, 055 

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

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

014, 022, 052, 054, 055 

A330-343 020, 022, 024, 050, 052, 054, 055
A330 Airworthiness Limitation Items

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ISSUE: 23 MAR 2012 PAGE: 11 

©AIRBUS SAS 2012. All rights reserved. 

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, 057, 058, 059, 

060, 061, 062 Group 32E 

A330-200F 000, 001, 002 - 

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, 054, 055 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. 

 
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INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 12 

©AIRBUS SAS 2012. All rights reserved. 

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 
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©AIRBUS SAS 2012. All rights reserved. 

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. 
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ACCESS

This column indicates the access requirements to adequately perform the inspection, i.e. 

all items listed must be removed or opened unless otherwise stated (e.g. NOTE 1). 

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

TASK DESCRIPTION

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

description and the boundaries of the DT ALI to be inspected. All 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. 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.2 AIRWORTHINESS LIMITATIONS

2-1 SECTION 2.1

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 521101-01-01 TASK DELETED IN ISSUE 18  521103-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 1 (FORWARD 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE. 

1280

 521105-01-01 ESCAPE SLIDE 

INSULATION LINING 

DETAILED INSPECTION OF TOP & BOTTOM CROSSBEAMS T8 & T1 ENDS AT FRAMES FR1 AND FR7 IN THEIR UNION TO DOOR STOP ASSEMBLIES, ON FORWARD PASSENGER/CREW DOOR, LH/RH. 

3390

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

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE. 

1280

 521203-01-01 TASK DELETED IN ISSUE 18  521203-01-02 TASK DELETED IN ISSUE 18  521301-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 4 (AFT 

PASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE. 

1280

 521303-01-01 TASK DELETED IN ISSUE 18  521303-01-02 TASK DELETED IN ISSUE 18  522201-01-02 N/A GENERAL VISUAL INSPECTION OF DOOR 3 

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

1280

 522203-01-01 TASK DELETED IN ISSUE 18  522203-01-02 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 523104-01-02 132AR 132BR 132CR 

132DR 132ER 132FR 132GR 132HR 132JR 132KR 132LR 

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

1580

 523106-01-01 821CR 

DOOR LOCKING HANDLE UNLOCKED 

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

1060

 523204-01-02 152AR 152BR 152CR 

152DR 152ER 152FR 152GR 152HR 152JR 152KR 152LR 

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

1580

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

LOWER ACCESS DOOR SKIN, EXTERNAL SURFACE. 

1030

 524103-01-02 811 

DOOR FLOOR PANEL 

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

3150

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

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

8300 

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

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

9600 

 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. 

1200

 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. 

2100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

3260

 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. 

2400

 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. 

1740

 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 . 

2870

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

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

1850

 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. 

1010

 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. 

8900 

 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. 

8700 

 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. 

3700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

STRUCTURE, NOSE LANDING GEAR WELL PANELS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1300 OR 3900 

 531124-01-03 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2850OR 8200

 531124-01-05 TASK DELETED IN ISSUE 18  531125-01-03 811 821 

AVIONICS BAY FLOOR PANELS 

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

3950

 531125-01-04 811 821 

AVIONICS BAY FLOOR PANELS 

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

2140

 531125-02-01 811 821 

AVIONICS BAY FLOOR PANELS 

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

1820

 531129-02-02 713 714 715 

716 BOLTS NLG ACTUATORS DISCONNECTED 

SPECIAL DETAILED INSPECTION OF NOSE LANDING GEAR ACTUATOR FITTING. 

3290
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

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

2190

 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. 

1850

 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. 

1850

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

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

3510

 531133-01-03 TASK DELETED IN ISSUE 18  531134-01-01 TASK DELETED IN ISSUE 18  531134-01-02 TASK DELETED IN ISSUE 18  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. 

3900

 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. 

4850 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 531136-01-02 CEILING PANELS 

NOTE 1 

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

1750

 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. 

3470

 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. 

3470

 531140-01-01 831 

LINING NOTE 1 GALLEYS AND TOILETS IF INSTALLED 

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

1570

 531141-01-02 LINING 

NOTE 1 

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

1750
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

3490

 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. 

3490

 531143-01-02 NOTE 1 

AIR DUCTS VACUUM PIPES 

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

1660

 531144-01-02 NOTE 1 

LINING TOILET 

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

1660
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

R 531144-01-03 LINING 

NOTE 1 TOILET 

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

2900

 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. 

2440

 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. 

3710

 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. 

2770

 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. 

3530
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 531154-01-02 LININGS 

SLIDING WINDOWS OPENED NOTE 1 

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

1580

 531154-01-03 LININGS 

SLIDING WINDOWS OPENED NOTE 1 

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

3130

 531155-01-01 LINING 

NOTE 1 

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

1750

 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. 

3130

 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. 

3530

 531160-01-01 811 821 

AVIONICS BAY FLOOR PANELS 

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

9900 

 531161-01-02 TASK DELETED IN ISSUE 18  531163-01-01 713 714 

NLG 

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

1380

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

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

7000 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

1560

 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. 

2270

 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. 

1740

 531178-01-01 125AL 125BL 125CL 

126BR 126CR 713 714 

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

2310

 531179-01-01 125AL 125BL 125CL 

126BR 126CR 713 714 

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

1190

 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. 

3150

 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. 

2870

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

EXTERNAL STRUCTURE, RIVET LINES AT UPPER LONGITUDINAL LAP JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A AND FROM FR.14 TO FR.16A, LH/RH. 

2110
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 531185-01-02 TASK DELETED IN ISSUE 18 

R 531186-01-02 TOILETS & CRR 

LININGS NOTE 1 TITANIUM RIVETS 

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

3150

 531186-01-03 TOILETS & CRR 

LININGS NOTE 1 TITANIUM RIVETS 

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

2870

 531188-01-02 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. 

3150
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

2870

 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. 

2930

 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. 

2180
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

2180

 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. 

2930

 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 

2250 

 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 

6900 

 532114-01-02 TASK DELETED IN ISSUE 18  532114-01-03 TASK DELETED IN ISSUE 18  532114-01-04 TASK DELETED IN ISSUE 18  532114-01-05 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL FRAMES (FR 20A AND FR 25A). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1730OR 5210

 532117-01-03 TASK DELETED IN ISSUE 18  532117-02-03 TASK DELETED IN ISSUE 18  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. 

2600

 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. 

1930

 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. 

2260

 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. 

2600

 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. 

2130

 532124-02-09 832 842 

SCUFF PLATE 

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

2600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

2600

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

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

8800 

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

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

3600 

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

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

9700 

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

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

5400 

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

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

4200 

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

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

4400 

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

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

7300 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 532126-01-01 832 842 

DOOR FRAME LINING INSULATION 

DETAILED INSPECTION OF DOOR 2, COVER PLATE OF TORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND STR 13, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2070OR 6210

 532127-01-01 832 842 

DOOR FRAME LINING NOTE 1 

DETAILED INSPECTION OF DOOR NO 2, FR 33, BETWEEN STR 13 AND STR 15, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1900OR 6210

 532128-01-01 TASK DELETED IN ISSUE 18  532129-01-02 TASK DELETED IN ISSUE 18  532129-01-03 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2040

 532130-01-03 TASK DELETED IN ISSUE 18  532130-01-04 TASK DELETED IN ISSUE 18  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. 

2650

 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. NOTE: THIS TASK IS APPLICABLE ONLY IF THE CUTOUT IS EMBODIED IN THE SKIN. 

2210

 532143-01-02 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 532144-01-02 832 842 

CEILING PANELS NOTE 1 

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

2000

 532146-01-02 TASK DELETED IN ISSUE 18  532147-01-02 821 

CARGO COMPARTMENT FLOOR PANELS LININGS NOTE 1 

DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS 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. 

2060

 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. 

2320

 532149-01-02 TASK DELETED IN ISSUE 18  532150-01-02 TASK DELETED IN ISSUE 18  532150-01-03 N/A SPECIAL DETAILED INSPECTION OF FUSELAGE 

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

3540

 532150-01-04 TASK DELETED IN ISSUE 18  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. 

2310

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

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

2260
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

1390

 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. 

3160

 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, - FROM STR 24 TO STR 26, LH/RH 

2590

 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. 

1710

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3970OR 1189
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3970OR 1189

 532156-01-04 TASK DELETED IN ISSUE 18  532157-01-02 832 842 

SIDEWALL LINING INSULATION 

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

3880

 532158-01-02 833 843 

CEILING PANELS INSULATION 

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3970OR 1189

 532158-01-03 TASK DELETED IN ISSUE 18  532164-01-01 TASK DELETED IN ISSUE 18  532165-01-02 831 841 

CEILING PANELS LINING INSULATION 

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

3580

 532165-01-03 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 

4500 

 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 532166-01-03 

6900 

 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 

1390

 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. 

1210

 533005-01-02 191AB 191AT 191BB 

191CB 192AT 192BB 192CB 197AT 197FB 197GB 197HB 198AT 198GB 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. 

1640

 533009-01-01 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3070OR 9210
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533009-01-02 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-02NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3280OR 1151

 533009-01-03 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-03NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8610

 533009-01-04 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-04NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8830
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533009-02-01 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3070OR 9210

 533009-02-02 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-02NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3280OR 1151

 533009-02-03 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-03NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8610
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533009-02-04 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-04NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8830

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3070OR 9210

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3280OR 1151

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8610

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8830
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533012-01-01 261CC 262CC 

OVERHEAD STOWAGE BINS NOTE 1 RIVETS 

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 533012-02-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3140OR 9430

 533012-02-01 261CC 262CC 

OVERHEAD STOWAGE BINS NOTE 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 533012-01-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3140OR 9430

 533013-01-02 TASK DELETED IN ISSUE 18  533013-01-03 TASK DELETED IN ISSUE 18  533013-01-04 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 9600

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2950OR 9640
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3150OR 9460

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 9250

 533016-01-03 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2960OR 8880

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3190OR 1119

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2780OR 8360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2850OR 8570

 533021-01-01 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

9000 OR 2954

 533021-01-02 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8350 OR 2750

 533021-01-03 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8650 OR 2830

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

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

1510
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533104-01-03 ANTICOLLISION LIGHT: 

LENS 7LV ADF: 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3790OR 1139

 533105-01-02 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 9110

 533106-01-03 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3770OR 1321

 533107-01-03 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1730OR 5210
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533107-01-04 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1560OR 5480

 533107-01-05 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1430OR 4310

 533107-01-06 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2220OR 6670

 533107-01-07 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2630OR 9220
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533107-01-08 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1470OR 4420

 533107-01-09 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2610OR 9130

 533107-01-10 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7170

 533107-01-11 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2450OR 7360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. 

3380

 533112-01-01 N/A SPECIAL DETAILED INSPECITON OF FUSELAGE 

EXTERNAL STRUCTURE, LONGITUDINAL JOINT AT STRINGER 39 AHEAD OF FRAME 53.2, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3850OR 1257

 533112-01-02 N/A SPECIAL DETAILED INSPECITON OF FUSELAGE 

EXTERNAL STRUCTURE, LONGITUDINAL JOINT AT STRINGER 39 AHEAD OF FRAME 53.2, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3570OR 1168

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1360OR 4100

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

9300 OR 2800
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1100OR 3870

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1280OR 3860

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1400OR 4920

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1320OR 3970

 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. 

1190

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2540OR 7630
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1890OR 5680

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2060OR 7240

 533115-01-04 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1650OR 4970

 533115-01-05 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1360OR 4100

 533115-01-06 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1670OR 5010

 533115-01-07 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1970OR 6920
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533115-01-08 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1490OR 5220

 533115-01-09 251XW 252XW 

NOTE 1 

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

1300

 533115-01-10 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1790OR 5380

 533124-01-02 TASK DELETED IN ISSUE 18  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. 

1500 

 533126-01-03 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

4050 OR 1320
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533126-01-05 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

4000 OR 1310

 533126-01-06 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

5300 OR 1730

 533127-03-01 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

4000 OR 1310

 533127-03-02 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

4050 OR 1320
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533127-03-03 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

5300 OR 1730

 533127-03-04 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

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

1900

 533137-01-01 TASK DELETED IN ISSUE 18  533137-01-02 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2460OR 8040

 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. 

2940

 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. 

2470

R 533151-01-01 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2130OR 6410
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

R 533151-01-02 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1760OR 5290

R 533151-01-03 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1920OR 6730

 533152-01-01 151GW 

152 GW ACT IF INSTALLED 

SPECIAL DETAILED INSPECTION OF INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31 AT FILLET FAIRING LEVEL, LH/RH 

2940

 533152-01-02 151GW 

152 BX ACT IF INSTALLED LDMCR IF INSTALLED 

SPECIAL DETAILED INSPECTION OF INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31 AT FILLET FAIRING LEVEL, LH/RH 

2940

 533152-01-03 151HX 

152 HX LDL IF INSTALLED 

SPECIAL DETAILED INSPECTION OF INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31 AT FILLET FAIRING LEVEL, LH/RH 

2940
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533152-01-04 151GW 152GW 

ACT IF INSTALLED 

SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET FAIRING LEVEL, LH/RH. 

2470

 533152-01-05 151GW 152BX 

ACT IF INSTALLED LD-MCR IF INSTALLED 

SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET FAIRING LEVEL, LH/RH. 

2470

R 533152-01-06 151HX 152HX 

LDL IF INSTALLED 

SPECIAL DETAILED INSPECTION OF STRINGER 31, INTERNAL FUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLET FAIRING LEVEL, LH/RH. 

2470

 533154-01-04 CABIN FLOOR PANELS 

GALLEYS TOILETS 

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

1210
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533154-01-05 CABIN FLOOR PANELS 

GALLEYS TOILETS 

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

2000

 533154-01-06 TASK DELETED IN ISSUE 18  533155-01-01 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3610OR 1180

 533155-01-02 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2900OR 9480

 533155-01-03 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3560OR 1165

 533156-01-01 822 

LINING NOTE 1 LD-MCR IF INSTALLED POST 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3040OR 9940
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533156-01-02 822 

LD-MCR IF INSTALLED OR POST 46678 LDL TOILETS AND FURNISHINGS LINING NOTE 1 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3480OR 1139

 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1630OR 5340

 533164-01-03 734 744 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1920OR 6290

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2450OR 8020

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2500OR 8170
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1930OR 6310

 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. 

2920

 533165-01-02 251MG 251SG 252MG 

252SG NOTE 1 GALLEYS & TOILETS IF INSTALLED 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 48 TO 53.1 HORIZONTAL LEG AT STRINGER PASSAGE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1140OR 3750

 533179-01-02 TASK DELETED IN ISSUE 18  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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2730OR 9600

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2040OR 6170
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533180-01-05 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3460OR 1044

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2770OR 9730

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2070OR 6240

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3540OR 1067
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

R 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3010OR 9080

R 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 9880

 533187-01-01 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2610OR 9150

 533187-01-02 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2480OR 7440

 533187-01-03 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2090OR 6290
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 533187-01-05 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1990OR 5990

 533192-01-01 TASK DELETED IN ISSUE 18  533193-01-01 TASK DELETED IN ISSUE 18  533194-01-04 834 844 SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN 

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 6020

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3580

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 5970

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 6020
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2600OR 7820

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 8410

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1700OR 5970

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 7220

R 533195-02-04 834 844 

SCUFF PLATE 

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 7220

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3580
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 5970

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 6020

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2600OR 7820

 533195-02-09 834 844 

SCUFF PLATE 

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 8410

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1700OR 5950
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 7220

 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. 

1530

R 533197-01-01 N/A GENERAL VISUAL INSPECTION OF FUSELAGE SKIN 

BETWEEN FR 53.3 AND FR 54 FROM STRINGER 6 LH TO STRINGER 6 RH, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-02-01 

4500 

R 533197-02-01 N/A DETAILED INSPECTION OF FUSELAGE SKIN BETWEEN 

FR 53.3 AND FR 54 FROM STRINGER 6 LH TO STRINGER 6 RH, EXTERNAL SURFACE. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-01-01 

6900 

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3210OR 9610

 534102-01-04 TASK DELETED IN ISSUE 18  534102-01-05 TASK DELETED IN ISSUE 18  534104-01-04 TASK DELETED IN ISSUE 18  534104-01-05 TASK DELETED IN ISSUE 18  534104-01-06 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534104-01-08 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS, 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8800 OR 2650

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3730OR 1124

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3170OR 9560

 534105-01-05 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2490OR 8690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534107-01-02 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS, INSULATION 

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1017

 534107-01-03 TASK DELETED IN ISSUE 18  534107-01-04 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS INSULATION 

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2490OR 8690

R 534108-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3170OR 1111

R 534110-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM STR 6 TO STR 13 LH/RH, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3170OR 1111

 534120-01-02 TASK DELETED IN ISSUE 18  534120-01-03 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1940OR 6810

 534124-01-02 TASK DELETED IN ISSUE 18  534124-02-02 TASK DELETED IN ISSUE 18  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 54 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-02-02 

2250 

 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 54 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-01-02 

6900 

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1050OR 3690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1050OR 3130

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1050OR 3690

534132-02-01 833 843 

SCUFF PLATE 

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

2280

 534132-02-02 TASK DELETED IN ISSUE 18  534132-02-03 TASK DELETED IN ISSUE 18  534135-01-01 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2280OR 6860

 534137-01-02 TASK DELETED IN ISSUE 18  534137-01-03 TASK DELETED IN ISSUE 18  534139-01-04 822 GENERAL VISUAL INSPECTION OF AFT CARGO 

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A AND 65) AS FAR AS VISIBLE.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1730OR 5210

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

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

5900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

5500 OR 1920

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8000 OR 2400

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8500 OR 2980

 534143-01-06 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

5300 OR 1610

 534144-01-02 823 

SCUFF PLATE 

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2340OR 7060

 534144-01-03 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534144-01-04 823 

SCUFF PLATE 

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2830OR 9890

 534146-01-02 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2570OR 7700

 534148-01-03 TASK DELETED IN ISSUE 18  534148-01-04 TASK DELETED IN ISSUE 18  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. 

3600 

 534150-01-02 TASK DELETED IN ISSUE 18  534150-01-03 823 

LININGS NOTE 1 

DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS 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. 

2790OR 8380

 534150-01-04 TASK DELETED IN ISSUE 18  534150-01-05 823 

LININGS NOTE 1 

DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS 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. 

2940
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534150-01-06 823 

LININGS NOTE 1 

DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS 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. 

1550

 534151-01-01 TASK DELETED IN ISSUE 18  534151-01-02 TASK DELETED IN ISSUE 18  534151-01-03 833 843 

DOOR FRAME LINING 

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

1260

 534152-01-01 833 843 

SIDEWALL LININGS NOTE 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. 

2000

 534153-01-01 162ZW 823 

NOTE 1 

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

2000

 534154-01-02 TASK DELETED IN ISSUE 18  534154-01-03 833 843 

LINING INSULATION 

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

2000

 534154-01-04 833 843 

LINING INSULATION 

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

1180
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534155-01-02 833 843 

LINING INSULATION 

SPECIAL DETAILED INSPECTION OF TORSION BOX LONGITUDINAL BEAM ADJACENT TO RUNOUT OF 

CORNER DOUBLER BETWEEN FR 73A AND FR 74, LH/RH. 

2000

 534156-01-02 822 

LINING CARGO FLOOR PANELS INSULATION 

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. 

3060

 534164-01-01 TASK DELETED IN ISSUE 18  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. 

2000

 534166-01-02 TASK DELETED IN ISSUE 18  534166-01-03 ANTENNA SPECIAL DETAILED INSPECTION OF SKIN AROUND 

VHF2 ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 51 TO STR 52, LH. 

2200

 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 

4500 

 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 

6900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 534182-01-01 835 

LINING NOTE1 

SPECIAL DETAILED INSPECTION OF FRAME AND FRAME COUPLING FROM FR 60 TO FR 64 BETWEEN STR 20X AND STR 23, RH. 

1030OR 3090

 534184-01-01 821 

LINING NOTE1 

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

2320OR 6960

 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. 

1650

 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. 

5100 

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

END OF ARMS AT ENGINE FORWARD MOUNT FITTING. 

1810
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1310OR 3930

 545104-02-04 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1350OR 4050

 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. (2 FASTENER LOCATIONS/PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1170OR 3510
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545104-02-12 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1300OR 4550

 545104-02-13 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1340OR 4690

 545104-02-14 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1160OR 4060
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545108-03-01 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

6100 OR 1860
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545108-03-03 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

5100 OR 1560

 545108-03-09 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

9300 OR 2790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545108-03-11 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

7200 OR 2160

 545108-03-12 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

9100 OR 3180

 545108-03-14 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

7100 OR 2480

 545108-04-19 415AL 416AR 425AL 

426AR 415BL 416BR 425BL 426BR 

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

7700 

 545108-04-20 415AL 416AR 425AL 

426AR 

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

7700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545111-02-01 ENGINE 

AFT ENGINE MOUNT DISASSEMBLED 

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

9500 OR 9830

 545129-01-03 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2690OR 8790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545129-01-04 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2690OR 8790

R 545129-01-09 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 1007

 545138-01-06 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2850OR 8550

 545138-01-09 TASK DELETED IN ISSUE 18  545138-01-10 TASK DELETED IN ISSUE 18  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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2820OR 9870

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2850OR 8550

 545138-02-05 TASK DELETED IN ISSUE 18  545138-02-06 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 11 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-12 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2820OR 9870

 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1120OR 3360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545140-01-02 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 545140-02-02. 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 (3770 FC OR 11310 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3600

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (3060 FC OR 9180 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8400 OR 2520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545140-01-06 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 545140-02-06. 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 (4560 FC OR 22800 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1100OR 3840

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (3620 FC OR 18090 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1170OR 4090
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (2930 FC OR 14680 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8300 OR 2900

 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. 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1120OR 3360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (7100 FC OR 21310 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3600

 545140-02-03 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 545140-01-03. 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 (5630 FC OR 16900 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8400 OR 2520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (7290 FC OR 36450 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1100OR 3840

 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. 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 ALI INTERVAL (6810 FC OR 34080 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1170OR 4090
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (5400 FC OR 27030 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8300 OR 2900

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1120OR 3360

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3600

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8400 OR 2520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1100OR 3850

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

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1170OR 4090

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8300 OR 2900

 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. 

7950 

 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. 

1120
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

7500 OR 2250

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

6700 OR 2010
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1240OR 3720

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1040OR 3120

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1220OR 4270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1020OR 3570

 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 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

7400 OR 2590

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

6600 OR 2310

 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. 

1170OR 3520

 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. 

1400OR 4210
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8610

 545143-02-09 TASK DELETED IN ISSUE 18  545143-02-10 TASK DELETED IN ISSUE 18  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 11 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-13 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2930OR 1025

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8610

 545143-03-04 TASK DELETED IN ISSUE 18  545143-03-05 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-13 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2930OR 1025

 545146-03-01 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3120OR 9360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545146-03-02 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2410OR 7230

 545146-03-03 TASK DELETED IN ISSUE 18  545146-03-04 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 9180

 545146-03-05 TASK DELETED IN ISSUE 18  545146-03-06 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3020OR 1057
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545146-03-07 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-04-07NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 1078

 545146-03-08 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-04-08NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2380OR 8330
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545146-04-01 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3120OR 9360

 545146-04-02 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2410OR 7230

 545146-04-03 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545146-04-04 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 9180

 545146-04-05 TASK DELETED IN ISSUE 18  545146-04-06 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3020OR 1057

 545146-04-07 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-07NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 1078
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545146-04-08 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-08NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2380OR 8330

 545150-02-01 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2200OR 6720

 545150-02-02 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 8190

 545150-02-06 TASK DELETED IN ISSUE 18  545150-02-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545150-02-08 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3330OR 9990

 545150-02-09 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 1141

 545150-02-10 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1011

 545150-02-11 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3680OR 1288
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545150-02-13 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

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

1940

 545150-02-14 452AL 462AL 

AIR DUCT PRE-COOLER RODS 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3760OR 1128

 545166-02-05 TASK DELETED IN ISSUE 18  545166-02-06 TASK DELETED IN ISSUE 18  545166-02-08 TASK DELETED IN ISSUE 18  545166-02-09 TASK DELETED IN ISSUE 18  545166-02-10 TASK DELETED IN ISSUE 18  545166-02-13 TASK DELETED IN ISSUE 18  545166-02-14 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3160OR 1033

 545168-02-08 TASK DELETED IN ISSUE 18  545168-02-09 TASK DELETED IN ISSUE 18  545168-02-10 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545168-02-13 452CL 452CR 462CL 

462CR 454BL 454BR 464BL 464BR 

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2590OR 8460

 545168-02-14 TASK DELETED IN ISSUE 18  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) 

1700

 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) 

1700
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545174-02-03 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000

 545174-02-06 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545174-02-07 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000

 545174-02-09 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000

 545174-02-10 454KL 454KR 454ML 

454MR 464KL 464KR 464ML 464MR 

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

1700

 545174-02-11 454KL 454KR 454ML 

454MR 464KL 464KR 464ML 464MR 

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

1700

 545174-02-12 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545174-02-13 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000

 545174-02-14 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000

 545174-02-15 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545180-04-04 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1850OR 5550

 545180-04-05 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1750OR 5250

 545180-04-06 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1740OR 6090

 545180-04-07 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1830OR 6400
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 545180-04-09 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

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

1700

 545180-04-10 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

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

1700

 545180-04-11 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1880OR 5640

 545180-04-12 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1870OR 6540

 551008-01-04 312AR 

313AL 

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES. 

2720OR 8160

 551008-01-06 312AR 

313AL 

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2310OR 6940
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 551008-01-07 312AR 

313AL 

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2310OR 6940

 551015-01-04 312AR GENERAL VISUAL INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO RIB 3 RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2270OR 6810

 551016-01-02 TASK DELETED IN ISSUE 18  551016-01-06 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3240OR 9740

 551016-01-07 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3240OR 9740

 551019-01-04 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN INTERGRAL FLANGE AT ATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH TO RIB 3 RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2880OR 1009

 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. 

1660OR 4980
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

R 571102-01-01 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

1500OR 7540

R 571102-01-02 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

2150OR 1079

 571102-01-03 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

1720OR 5160

 571102-01-04 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

1650OR 4970

 571102-01-05 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

2420OR 7270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571102-01-06 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

2240OR 1120

R 571102-01-07 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

2370OR 7110

 571102-01-08 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

2440OR 7320

 571102-01-09 821 

NOTE 1 LINING AIR CONDITIONING DUCTS 

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

1630

 571103-01-03 191HB 192HB 821 

NOTE 1 LINING AIR CONDITIONING DUCTS FASTENER (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. 

1560OR 4690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571103-01-04 191HB 192HB 821 

NOTE 1 LINING AIR CONDITIONING DUCTS FASTENER (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. 

1440OR 7200

 571103-01-05 191HB 192HB 821 

NOTE 1 LINING AIR CONDITIONING DUCTS FASTENER (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 

1560OR 4680

 571103-01-06 191HB 192HB 821 

NOTE 1 LINING AIR CONDITIONING DUCTS FASTENER (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 571103-02-06. 

1580OR 4750

 571103-02-03 821 

NOTE 1 LINING AIR 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 

1560OR 4690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571103-02-04 821 

NOTE 1 LINING AIR 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. 

1440OR 7200

 571103-02-05 821 

NOTE 1 LINING AIR 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 

1560OR 4680

 571103-02-06 821 

NOTE 1 LINING AIR 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. 

1580OR 4750

 571104-01-01 191KB 192PB 

FASTENER TO BE REMOVED 821 131CX 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. 

2810OR 8450

 571104-01-02 191KB 192PB 

FASTENER TO BE REMOVED 821 131CX 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. 

1650OR 4960
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571104-01-03 191KB 192PB 

FASTENER TO BE REMOVED 821 131CX 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. 

2610OR 7840

R 571104-01-04 191KB 192PB 

FASTENER TO BE REMOVED 821 131CX 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. 

1950OR 9780

 571104-01-05 191KB 192PB 

FASTENER TO BE REMOVED 821 131CX 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. 

2320OR 6960

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

BOX LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & 21, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3520OR 1234

 571107-01-03 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3210OR 1051

 571107-01-05 TASK DELETED IN ISSUE 18  571108-01-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571108-01-05 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3870OR 1162

 571108-01-06 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3860OR 1353

 571108-01-07 TASK DELETED IN ISSUE 18  571110-01-01 821 

NOTE 1 LINING AIR 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. 

2500OR 7500

 571114-01-05 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3270OR 9830

 571114-01-06 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2610OR 9150
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571114-01-07 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2890OR 8690

 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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3520OR 1234

 571116-01-03 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3210OR 1051

 571116-01-05 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3520OR 1234

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3210OR 1051

 571118-01-08 TASK DELETED IN ISSUE 18  571118-01-09 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571119-01-01 CABIN FLOOR PANELS, 

GALLEYS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, LONGITUDINAL BEAMS ABOVE CWB, WEB HOLE AREA BETWEEN FRAMES 41 AND 42 FROM Y=-1456 TO Y=1456. 

3300

 571121-01-03 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1959 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2960OR 8900

 571121-01-04 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1960 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2970OR 8910

 571121-01-05 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1961 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2990OR 1047
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571122-01-04 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2880OR 8640

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 8030

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2290OR 8040

 571123-01-04 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2740OR 8230

 571123-01-05 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 8390

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3020OR 9890
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2230OR 7830

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2350OR 7680

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3360OR 1009

 571126-01-04 734 SPECIAL DETAILED INSPECTION OF CENT WING BOX, 

REAR SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2750OR 9640

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2920OR 8780

 571129-01-04 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3840OR 1256
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571130-01-03 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUTOUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3840OR 1256

R 571130-01-04 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUTOUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3750OR 1226

 571133-01-01 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 1121

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3790OR 1138

 571145-01-01 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3170OR 9530
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3150OR 1103

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3120OR 9380

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 1078

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3290OR 9890

 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. 

3200
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3420OR 1028

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2900OR 1017

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3040OR 9140

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2930OR 1028
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 9260

 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. 

3060

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2130OR 6960

 571153-01-01 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2140OR 7010

 571153-01-02 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2050OR 7190
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571153-01-03 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1360OR 4440

 571153-01-04 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1900OR 6220

R 571153-01-05 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2070OR 6780

 571153-01-06 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1820OR 6380
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571153-01-07 147AZ 148AZ 

734 744 SEALANT 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. 

1110

 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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2970OR 9700

 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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2800OR 9170

 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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 9200

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1260OR 4120
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

R 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1200OR 3940

R 571163-01-02 191HB 192HB SPECIAL DETAILED INSPECTION OF FRAME 40 NODE, 

FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAM FITTING AND LOWER PANEL, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1090OR 3560

 571164-01-01 191HB 192HB DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, KEEL BEAM FITTING ANGLE AND DOUBLER AT FR 40, LH/RH. 

1960
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 571164-01-02 191HB 192HB DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, KEEL BEAM FITTING ANGLE AND DOUBLER AT FR 40, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1920OR 6290

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1220OR 3670

 572001-02-01 TASK DELETED IN ISSUE 18  572001-02-03 TASK DELETED IN ISSUE 18  572001-02-04 TASK DELETED IN ISSUE 18  572002-01-05 454DL 454DR 454FL 

454FR 464DL 464DR 464FL 464FR 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 9790

 572002-01-08 454KL 454KR 454ML 

454MR 464KL 464KR 464ML 464MR 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 9790

 572003-01-04 TASK DELETED IN ISSUE 18  572003-01-06 TASK DELETED IN ISSUE 18  572003-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3350OR 1173

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3280OR 9840

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3200OR 9610

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3200OR 9610

 572005-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2550OR 7660
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572005-01-07 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2850OR 1000

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 8450

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 8450

 572005-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2550OR 7660

 572006-01-01 TASK DELETED IN ISSUE 18  572006-01-02 TASK DELETED IN ISSUE 18  572006-01-03 TASK DELETED IN ISSUE 18  572006-02-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572006-02-09 N/A GENERAL VISUAL INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3540OR 1241

 572006-02-10 N/A GENERAL VISUAL INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2970OR 8930

 572007-01-04 TASK DELETED IN ISSUE 18  572007-01-05 TASK DELETED IN ISSUE 18  572007-01-06 TASK DELETED IN ISSUE 18  572007-01-08 TASK DELETED IN ISSUE 18  572008-01-04 TASK DELETED IN ISSUE 18  572009-01-04 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2910OR 1019

 572009-01-05 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2750OR 8270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572009-01-06 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2720OR 8170

 572009-02-04 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2910OR 1019

 572009-02-05 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2750OR 8270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572009-02-06 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2720OR 8170

 572010-02-04 TASK DELETED IN ISSUE 18  572010-02-06 TASK DELETED IN ISSUE 18  572010-02-07 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3500OR 1227

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2740OR 8230

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3490OR 1048

 572012-02-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572013-03-01 TASK DELETED IN ISSUE 18  572013-03-02 TASK DELETED IN ISSUE 18  572013-03-03 TASK DELETED IN ISSUE 18  572013-03-04 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3720OR 1118

 572015-02-01 TASK DELETED IN ISSUE 18  572015-02-02 TASK DELETED IN ISSUE 18  572015-02-03 TASK DELETED IN ISSUE 18  572015-02-04 TASK DELETED IN ISSUE 18  572016-02-04 TASK DELETED IN ISSUE 18  572016-02-05 TASK DELETED IN ISSUE 18  572016-02-06 TASK DELETED IN ISSUE 18  572016-02-07 TASK DELETED IN ISSUE 18  572016-02-08 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3190OR 9580

 572016-02-09 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2730OR 9560

 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. 

2690OR 8090

 572018-01-05 TASK DELETED IN ISSUE 18  572018-01-06 TASK DELETED IN ISSUE 18  572018-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572018-01-08 TASK DELETED IN ISSUE 18  572018-01-09 TASK DELETED IN ISSUE 18  572018-01-10 TASK DELETED IN ISSUE 18  572018-01-11 TASK DELETED IN ISSUE 18  572018-01-12 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3620OR 1270

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3320OR 9970

 572019-01-07 TASK DELETED IN ISSUE 18  572019-01-08 TASK DELETED IN ISSUE 18  572019-01-09 TASK DELETED IN ISSUE 18  572019-01-10 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3560OR 1068

 572019-01-12 TASK DELETED IN ISSUE 18  572021-03-02 TASK DELETED IN ISSUE 18  572022-01-04 TASK DELETED IN ISSUE 17  572022-01-05 TASK DELETED IN ISSUE 17  572022-01-06 TASK DELETED IN ISSUE 17  572022-01-07 TASK DELETED IN ISSUE 17 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3150OR 1102

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2630OR 7910

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 9240

 572023-02-06 TASK DELETED IN ISSUE 18  572027-01-05 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3640OR 1275
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572027-01-06 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2900OR 8720

 572027-01-10 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3560OR 1070

 572029-01-03 TASK DELETED IN ISSUE 18  572029-01-04 TASK DELETED IN ISSUE 18  572029-01-05 TASK DELETED IN ISSUE 18  572029-01-06 TASK DELETED IN ISSUE 18  572030-01-04 TASK DELETED IN ISSUE 18  572030-01-05 TASK DELETED IN ISSUE 18  572030-01-06 TASK DELETED IN ISSUE 18  572030-01-07 TASK DELETED IN ISSUE 18  572030-01-08 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1560OR 5470

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1590OR 4730
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1440OR 4330

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1440OR 4330

 572032-01-08 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1560OR 5470

 572032-01-10 TASK DELETED IN ISSUE 18  572032-01-11 TASK DELETED IN ISSUE 18  572032-01-12 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1850OR 5560

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2240OR 7850
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2200OR 6600

 572033-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1990OR 5980

 572033-01-07 TASK DELETED IN ISSUE 18  572033-01-08 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1990OR 5980

 572033-01-09 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2240OR 7850

 572034-01-04 TASK DELETED IN ISSUE 18  572034-01-05 TASK DELETED IN ISSUE 18  572034-01-06 TASK DELETED IN ISSUE 18  572034-01-07 TASK DELETED IN ISSUE 18  572035-01-04 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3330OR 1001
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572035-01-06 TASK DELETED IN ISSUE 18  572035-01-07 TASK DELETED IN ISSUE 18  572036-01-04 TASK DELETED IN ISSUE 18  572036-01-05 TASK DELETED IN ISSUE 18  572036-01-06 TASK DELETED IN ISSUE 18  572036-01-07 TASK DELETED IN ISSUE 18  572037-01-05 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 AND TOP SKIN LOWER SURFACE AT ROOT JOINT FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3170OR 9520

 572039-01-04 TASK DELETED IN ISSUE 18  572039-01-05 TASK DELETED IN ISSUE 18  572039-01-06 TASK DELETED IN ISSUE 18  572039-01-07 TASK DELETED IN ISSUE 18  572040-01-04 TASK DELETED IN ISSUE 18  572040-01-05 TASK DELETED IN ISSUE 18  572040-01-06 TASK DELETED IN ISSUE 18  572040-01-07 TASK DELETED IN ISSUE 18  572043-01-04 TASK DELETED IN ISSUE 18  572043-01-05 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3020OR 9080

 572043-01-06 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3990OR 1198

 572043-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572043-01-10 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3890OR 1169

 572043-01-11 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3750OR 1315

 572046-01-04 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 1062

 572046-01-05 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2510OR 7550

 572046-01-06 TASK DELETED IN ISSUE 18  572046-01-07 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2820OR 8460

 572046-01-08 TASK DELETED IN ISSUE 18  572046-01-09 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2690OR 9410
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572046-01-10 TASK DELETED IN ISSUE 18  572046-01-11 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2610OR 7830

 572046-01-12 TASK DELETED IN ISSUE 18  572046-01-13 541AB 541BB 541CB 

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

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

2220OR 6680

 572047-01-03 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3190OR 1117

 572047-01-04 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 9200

 572047-01-05 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2880OR 8640
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572047-01-06 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3520OR 1056

 572047-01-07 TASK DELETED IN ISSUE 18  572047-01-08 TASK DELETED IN ISSUE 18  572047-01-09 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1184

 572047-01-10 TASK DELETED IN ISSUE 18  572048-01-01 TASK DELETED IN ISSUE 18  572048-01-02 TASK DELETED IN ISSUE 18  572048-01-03 TASK DELETED IN ISSUE 18  572048-01-04 TASK DELETED IN ISSUE 18  572049-01-04 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 1030

 572049-01-05 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3830OR 1150
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572049-01-06 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2800OR 8400

 572049-01-07 TASK DELETED IN ISSUE 18  572049-01-08 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2640OR 7920

 572049-01-09 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2520OR 8840

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3510OR 1231

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2220OR 6660

 572050-01-06 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3420OR 1028

 572050-01-08 TASK DELETED IN ISSUE 18  572050-01-09 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 9850

 572050-01-10 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2950OR 8870

 572050-01-11 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2950OR 8870

 572050-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 9850
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572051-01-05 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2380OR 8340

 572051-01-06 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1015

 572051-01-07 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1390OR 4170

 572051-01-08 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2210OR 6640

 572051-01-09 TASK DELETED IN ISSUE 18  572051-01-10 FLAPS EXTENDED 

SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2820OR 9880

 572051-01-12 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3180OR 9550
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572052-03-01 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2090OR 9650

 572052-03-02 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1600OR 5120

 572052-03-04 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2140OR 6420

 572052-03-05 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2140OR 6430

 572052-03-06 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2360OR 7390

 572052-03-07 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2360OR 7390
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572052-03-08 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2030OR 1193

 572052-03-09 TASK DELETED IN ISSUE 18  572052-03-10 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. 

2750OR 8250

 572054-01-05 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 7010

 572054-01-06 TASK DELETED IN ISSUE 18  572054-01-07 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1410OR 4240

 572054-01-08 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1820OR 5470

 572054-01-09 TASK DELETED IN ISSUE 18  572054-01-10 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1740OR 6090
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572054-01-11 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1530OR 4610

 572054-01-12 TASK DELETED IN ISSUE 18  572054-01-13 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2120OR 6360

 572054-01-14 TASK DELETED IN ISSUE 18  572054-01-15 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. 

2680OR 8040

 572063-01-05 TASK DELETED IN ISSUE 18  572063-01-06 TASK DELETED IN ISSUE 18  572063-01-07 TASK DELETED IN ISSUE 18  572063-01-08 TASK DELETED IN ISSUE 18  572063-01-10 TASK DELETED IN ISSUE 18  572063-01-11 TASK DELETED IN ISSUE 18  572064-01-05 TASK DELETED IN ISSUE 18  572064-01-06 TASK DELETED IN ISSUE 18  572064-01-07 TASK DELETED IN ISSUE 18  572064-01-08 TASK DELETED IN ISSUE 18  572064-01-09 TASK DELETED IN ISSUE 18  572064-01-10 TASK DELETED IN ISSUE 18  572064-01-11 TASK DELETED IN ISSUE 18  572064-01-12 TASK DELETED IN ISSUE 18  572064-01-13 541EB 641EB DETAILED INSPECTION OF OUTER WING FRONT SPAR 

AFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND BOTTOM FLANGES. 

2480OR 7450

 572065-01-04 TASK DELETED IN ISSUE 18  572066-01-05 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572067-01-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1850OR 5550

 572067-01-06 TASK DELETED IN ISSUE 18  572067-01-15 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3880OR 1166

 572067-01-17 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2770OR 8330
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572067-03-03 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 641FZ 

SPECIAL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2770OR 8330

R 572067-03-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 641FZ 

SPECIAL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3880OR 1166

 572068-01-04 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3770OR 1321
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572068-01-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3650OR 1097

 572068-01-06 TASK DELETED IN ISSUE 18  572068-01-13 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2600OR 7810

 572069-01-04 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2710OR 9510

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7170
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7170

 572069-01-08 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2990OR 8980

 572069-01-11 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3490OR 1048

 572069-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3240OR 1136

 572071-01-06 TASK DELETED IN ISSUE 18  572071-01-07 TASK DELETED IN ISSUE 18  572073-01-05 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572081-01-05 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2270OR 7970

 572081-01-06 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1850OR 5560

 572081-01-07 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7190

 572081-01-08 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2130OR 6410

 572081-01-10 TASK DELETED IN ISSUE 18  572081-01-13 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2190OR 6590

 572081-01-14 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2190OR 7690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572081-01-15 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. 

3010OR 9040

 572082-01-05 TASK DELETED IN ISSUE 18  572082-01-06 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2210OR 6630

 572082-01-07 TASK DELETED IN ISSUE 18  572082-01-08 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3340OR 1003

 572082-01-09 TASK DELETED IN ISSUE 18  572082-01-10 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3190OR 1119

 572082-01-11 TASK DELETED IN ISSUE 18  572082-01-12 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3660OR 1100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572082-01-13 TASK DELETED IN ISSUE 18  572082-01-14 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. 

1910OR 5740

 572084-01-01 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3250OR 9760

 572084-01-03 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 7760

 572084-01-04 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2380OR 7150

 572084-01-05 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2350OR 8220
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572084-01-06 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2510OR 7540

 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. 

2450

 572090-01-01 TASK DELETED IN ISSUE 18  572090-01-03 TASK DELETED IN ISSUE 18  572090-01-04 TASK DELETED IN ISSUE 18  572090-02-01 TASK DELETED IN ISSUE 18  572090-02-03 TASK DELETED IN ISSUE 18  572090-02-04 TASK DELETED IN ISSUE 18  572092-01-04 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 1007

 572092-01-05 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2580OR 7740

 572092-01-06 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2890OR 8690
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572093-01-06 TASK DELETED IN ISSUE 18  572093-01-07 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 572093-02-07 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 9100

 572093-01-08 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 572093-02-08 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2630OR 7910

 572093-01-09 TASK DELETED IN ISSUE 18  572093-01-10 TASK DELETED IN ISSUE 18  572093-01-13 TASK DELETED IN ISSUE 18  572093-01-14 TASK DELETED IN ISSUE 18  572093-02-06 TASK DELETED IN ISSUE 18  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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 9100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572093-02-08 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 572093-01-08 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2630OR 7910

 572093-02-09 TASK DELETED IN ISSUE 18  572093-02-10 TASK DELETED IN ISSUE 18  572093-02-13 TASK DELETED IN ISSUE 18  572093-02-14 TASK DELETED IN ISSUE 18  572094-01-05 TASK DELETED IN ISSUE 18  572094-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3390OR 1018

 572094-01-10 TASK DELETED IN ISSUE 18  572095-01-05 TASK DELETED IN ISSUE 18  572095-01-06 TASK DELETED IN ISSUE 18  572095-01-07 TASK DELETED IN ISSUE 18  572095-01-08 TASK DELETED IN ISSUE 18  572101-01-04 TASK DELETED IN ISSUE 18  572101-01-06 TASK DELETED IN ISSUE 18  572101-01-07 TASK DELETED IN ISSUE 18  572104-01-04 TASK DELETED IN ISSUE 18  572104-01-05 TASK DELETED IN ISSUE 18  572104-01-06 TASK DELETED IN ISSUE 18  572104-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572107-01-05 N/A SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-05 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1014

 572107-02-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT RUNOUTS OF STRINGER 

BETWEEN RIB 23 AND RIB 39. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-05 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1014

 572108-02-04 TASK DELETED IN ISSUE 18  572108-02-06 TASK DELETED IN ISSUE 18  572108-02-07 TASK DELETED IN ISSUE 18  572109-02-05 542EB 542FB 542GB 

542HB 542JB 542KB 550AB 550BB 550CB 550DB 550EB 550FB 642EB 642FB 642GB 642HB 642JB 642KB 650AB 650BB 650CB 650DB 650EB 650FB 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3210OR 9630

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2860OR 1001
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2830OR 8500

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2870OR 8620

 572110-01-07 TASK DELETED IN ISSUE 18  572111-01-04 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1980OR 6960

 572111-01-05 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1920OR 5760

 572111-01-06 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2000OR 6020

 572111-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572111-01-09 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3230OR 1133

 572111-01-10 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3540OR 1064

 572111-01-11 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3230OR 1133

 572116-02-01 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 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3810OR 1334

 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 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3650OR 1095

 572117-01-05 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572119-02-05 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3200OR 1121

 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. 

2730OR 8190

 572121-01-04 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2430OR 8520

 572121-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7180

 572121-01-06 TASK DELETED IN ISSUE 18  572121-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2460OR 7390
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572121-01-08 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3680OR 1288

 572121-01-09 TASK DELETED IN ISSUE 18  572122-01-04 TASK DELETED IN ISSUE 18  572122-01-05 TASK DELETED IN ISSUE 18  572122-01-06 TASK DELETED IN ISSUE 18  572122-01-07 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2730OR 9570

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 9790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-06. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2800OR 8420

 572125-01-09 TASK DELETED IN ISSUE 18  572125-02-04 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-06. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2730OR 9570

 572125-02-05 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-07. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3260OR 9790

 572125-02-06 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-08. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2800OR 8420

 572125-02-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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 AS TASK 572129-02-03. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3040OR 9140

 572129-02-03 541SB 641SB 

SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-01-03. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3040OR 9140

 572130-01-03 TASK DELETED IN ISSUE 18  572130-02-03 TASK DELETED IN ISSUE 18  572131-01-04 TASK DELETED IN ISSUE 18  572131-01-05 TASK DELETED IN ISSUE 18  572131-01-06 TASK DELETED IN ISSUE 18  572131-01-07 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3590OR 1256

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 9910
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3690OR 1108

 572133-01-10 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3690OR 1108

 572133-01-11 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3590OR 1256

 572138-01-05 TASK DELETED IN ISSUE 18  572138-01-07 TASK DELETED IN ISSUE 18  572138-01-09 TASK DELETED IN ISSUE 18  572138-01-10 TASK DELETED IN ISSUE 18  572139-01-05 TASK DELETED IN ISSUE 18  572139-01-07 TASK DELETED IN ISSUE 18  572139-01-09 TASK DELETED IN ISSUE 18  572139-01-10 TASK DELETED IN ISSUE 18  572140-01-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572140-01-05 541EB 541FB 541GB 

541HB 541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641EB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3600OR 1081

 572140-01-10 541EB 541FB 541GB 

541HB 541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641EB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 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. 

3020OR 9080

 572141-01-04 TASK DELETED IN ISSUE 18  572141-01-05 TASK DELETED IN ISSUE 18  572141-01-08 TASK DELETED IN ISSUE 18  572144-01-05 TASK DELETED IN ISSUE 18  572144-01-07 TASK DELETED IN ISSUE 18  572144-01-09 TASK DELETED IN ISSUE 18  572144-01-10 TASK DELETED IN ISSUE 18  572148-01-04 TASK DELETED IN ISSUE 18  572148-01-05 TASK DELETED IN ISSUE 18  572148-01-06 TASK DELETED IN ISSUE 18  572148-01-07 TASK DELETED IN ISSUE 18  572153-01-04 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3850OR 1349
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572153-01-05 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2360OR 7090

 572153-01-06 TASK DELETED IN ISSUE 18  572153-01-08 TASK DELETED IN ISSUE 18  572153-01-11 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3940OR 1184

 572153-01-12 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3590OR 1257

 572154-01-04 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1860OR 6520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572154-01-05 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1920OR 5780

 572154-01-06 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1670OR 5030

 572154-01-07 TASK DELETED IN ISSUE 18  572154-01-08 TASK DELETED IN ISSUE 18  572154-01-09 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1630OR 5710
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572154-01-10 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1780OR 5360

 572154-01-11 TASK DELETED IN ISSUE 18  572154-01-13 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. 

3280OR 9840

 572158-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2900OR 1016

 572158-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2680OR 8040
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572158-01-10 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2960OR 8880

 572158-01-12 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3920OR 1374

 572159-01-04 TASK DELETED IN ISSUE 18  572159-01-05 TASK DELETED IN ISSUE 18  572159-01-09 TASK DELETED IN ISSUE 18  572162-01-05 TASK DELETED IN ISSUE 18  572164-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3740OR 1310
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572164-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2980OR 8950

 572164-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3550OR 1067

 572164-01-09 TASK DELETED IN ISSUE 18  572164-01-11 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3470OR 1216
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572164-01-12 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3470OR 1042

 572166-01-05 TASK DELETED IN ISSUE 17  572180-01-04 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2030OR 7130

 572180-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1960OR 5900

 572180-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2050OR 6150
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572180-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3340OR 1003

 572180-01-08 TASK DELETED IN ISSUE 18  572180-01-09 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 1072

 572180-01-10 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 1072

 572180-01-11 TASK DELETED IN ISSUE 18  572180-01-12 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. 

2860OR 8590

 572181-01-04 TASK DELETED IN ISSUE 18  572181-01-05 TASK DELETED IN ISSUE 18  572181-01-06 TASK DELETED IN ISSUE 18  572181-01-07 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572183-01-04 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2230OR 7800

 572183-01-05 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2520OR 7570

 572183-01-06 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2240OR 6720

 572183-01-07 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-7 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8840
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572183-01-08 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 9360

 572183-01-10 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-10 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8840

 572183-01-11 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-11 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 9360

 572183-02-04 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2230OR 7800
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572183-02-05 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2520OR 7570

 572183-02-06 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2240OR 6720

 572183-02-07 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-7 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8840

 572183-02-08 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 9360
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572183-02-10 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-10 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 8840

 572183-02-11 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-11 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2670OR 9360

 572184-01-04 TASK DELETED IN ISSUE 18  572184-01-05 TASK DELETED IN ISSUE 18  572184-01-06 TASK DELETED IN ISSUE 18  572184-01-07 TASK DELETED IN ISSUE 18  572184-02-04 TASK DELETED IN ISSUE 18  572184-02-05 TASK DELETED IN ISSUE 18  572184-02-06 TASK DELETED IN ISSUE 18  572184-02-07 TASK DELETED IN ISSUE 18  572185-01-01 TASK DELETED IN ISSUE 18  572185-01-02 TASK DELETED IN ISSUE 18  572185-01-03 TASK DELETED IN ISSUE 18  572185-01-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 572606-01-02 532CB 533CB 534CB 

632CB 633CB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3380OR 1014

 572606-01-03 532CB 533CB 534CB 

632CB 633CB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2890OR 1013

 572606-01-07 532CB 533CB 534CB 

632CB 633CB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. 

2010OR 6030

 572607-01-01 531AB 531CB 532AB 

532CB 533AB 533CB 534AB 534CB 631AB 631CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3850OR 1155

 572607-01-06 531AB 531CB 532AB 

532CB 533AB 533CB 534AB 534CB 631AB 631CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. 

2210OR 6640

 572607-01-07 531AB 531CB 532AB 

532CB 533AB 533CB 534AB 534CB 631AB 631CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3300OR 1155
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2410OR 8460

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2640OR 7940

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2660OR 7990

 573001-01-10 TASK DELETED IN ISSUE 18  573002-01-05 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2410OR 8460

 573002-01-07 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2640OR 7940
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 573002-01-08 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2660OR 7990

 573002-01-09 TASK DELETED IN ISSUE 18  573003-02-04 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON 

WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2940OR 1029

 573003-02-05 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3080OR 9250

 573003-02-06 TASK DELETED IN ISSUE 18  573003-02-07 TASK DELETED IN ISSUE 18  573003-02-08 TASK DELETED IN ISSUE 18  573003-02-09 TASK DELETED IN ISSUE 18  573003-02-10 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON 

WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3240OR 9720

 573003-02-12 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). 

1640OR 4920
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-04 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2400OR 8430
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-05 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2390OR 7190
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-06 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2650OR 7960
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-07 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3250OR 1140

 574106-01-08 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-11 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3250OR 1140
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574106-01-12 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3500OR 1051

 574107-02-04 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3410OR 1193
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574107-02-05 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3690OR 1107

 574107-02-06 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3620OR 1088
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-01 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1350OR 4750
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-02 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1350OR 4050
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-03 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1970OR 5920

 574109-02-04 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-05 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1830OR 6430

 574109-02-06 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-07 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1490OR 4480

 574109-02-08 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574109-02-09 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. 

1830OR 5500

 574110-02-01 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 1074
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574110-02-02 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3060OR 9190

 574110-02-03 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2930OR 8810

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3050OR 1069

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3340OR 1002

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 9090
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3030OR 9090

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1650OR 5800

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1910OR 5730

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1590OR 4790

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1590OR 4790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574115-02-07 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3140OR 9420

 574115-02-09 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3350OR 1175

 574704-02-03 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS 

AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. 

3110OR 1090

 574704-03-02 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 5, SKIN 

CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. 

3110OR 1090

 574804-01-02 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN 

CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. 

6100 OR 2150

 574804-01-03 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN 

CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1980OR 5950
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 574804-02-04 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS 

AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1980OR 5950

 574804-02-05 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS 

AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. 

6100 OR 2150

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3800OR 1330

 575011-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1900OR 5700

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3960OR 1190

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3960OR 1190

 575011-01-08 TASK DELETED IN ISSUE 18  575011-01-09 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3800OR 1330

 575011-01-11 TASK DELETED IN ISSUE 18  575011-01-12 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. 

2860OR 8580

 575011-01-13 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3790OR 1137

 575012-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2190OR 7670

 575012-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2530OR 7610
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 575012-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2140OR 6420

 575012-01-10 TASK DELETED IN ISSUE 18  575012-01-11 TASK DELETED IN ISSUE 18  575014-01-06 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING 

TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG REINFORCING. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3430OR 1031

 575016-01-04 TASK DELETED IN ISSUE 18  575016-01-05 531AB 631AB DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3490OR 1048

 575016-01-06 TASK DELETED IN ISSUE 18  575016-01-08 TASK DELETED IN ISSUE 18  575017-01-04 TASK DELETED IN ISSUE 18  575017-01-06 TASK DELETED IN ISSUE 18  575017-01-07 TASK DELETED IN ISSUE 18  575018-01-03 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2340OR 8190
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 575018-01-04 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2780OR 8340

 575018-01-05 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2570OR 7730

 575018-01-06 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2710OR 8150

 575018-01-07 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2710OR 8150

 575018-01-08 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2520OR 8840

 575018-01-09 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2520OR 8840

 575018-01-10 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1440OR 5040

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1400OR 4210

 575022-01-03 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1300OR 4570
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1540OR 4640

 575022-01-06 TASK DELETED IN ISSUE 18  575022-01-07 TASK DELETED IN ISSUE 18  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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3820OR 1339

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1970OR 6900

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1880OR 5640
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2140OR 6440

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1740OR 5220

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1430OR 5000

 575025-01-09 TASK DELETED IN ISSUE 18  575051-01-01 734 744 

FLAPS EXTENDED 

DETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPER FLANGES RADII OF ROLLER TRACKS. 

3560

 575051-01-02 TASK DELETED IN ISSUE 18  575053-01-02 TASK DELETED IN ISSUE 18  575054-01-01 TASK DELETED IN ISSUE 18  575054-01-02 TASK DELETED IN ISSUE 18  575055-01-02 TASK DELETED IN ISSUE 18  575055-01-03 TASK DELETED IN ISSUE 18  575057-01-02 TASK DELETED IN ISSUE 18  575059-01-02 TASK DELETED IN ISSUE 18  575061-01-02 TASK DELETED IN ISSUE 18  575061-01-03 TASK DELETED IN ISSUE 18  575063-01-01 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2250OR 6750

 575067-01-03 TASK DELETED IN ISSUE 18  575067-02-02 FWD FLAP TRACK 

FAIRINGS FAIL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2250OR 6750

 575067-02-03 TASK DELETED IN ISSUE 18  575069-01-02 TASK DELETED IN ISSUE 18  575069-01-03 TASK DELETED IN ISSUE 18  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. 

3000 

 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. 

5900 

 575402-01-01 TASK DELETED IN ISSUE 18  575403-01-02 TASK DELETED IN ISSUE 18  575403-01-03 TASK DELETED IN ISSUE 18  575403-02-02 TASK DELETED IN ISSUE 18  575403-02-03 TASK DELETED IN ISSUE 18  575405-01-02 TASK DELETED IN ISSUE 18  575503-01-02 TASK DELETED IN ISSUE 18 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 575503-02-02 TASK DELETED IN ISSUE 18  575505-01-02 TASK DELETED IN ISSUE 18  575505-02-02 TASK DELETED IN ISSUE 18  575507-01-02 TASK DELETED IN ISSUE 18  575507-02-02 TASK DELETED IN ISSUE 18  575509-01-02 TASK DELETED IN ISSUE 18  575509-02-02 TASK DELETED IN ISSUE 18  576105-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1360OR 5130

 576105-01-02 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1. 

1110OR 3350

 576108-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

3020OR 1138

 576108-01-02 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. 

1540OR 9260

 576114-02-01 JACK FAIRINGS SPECIAL DETAILED INSPECTION OF INNER AILERONS, 

LOWER FLANGE OF OUTER JACK FITTING. 

3000OR 1955

 576115-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGERADIUS AT LUG SIDE OF HINGE1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

2810OR 1061

 576115-01-02 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGERADIUS AT LUG SIDE OF HINGE1. 

2040OR 6140
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 576117-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACK FITTING. 

1190OR 7800

 576117-01-02 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACK FITTING. 

1310OR 3940

 576118-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

1550OR 6200

 576118-01-02 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. 

1070OR 5360

 577003-01-02 TASK DELETED IN ISSUE 18  711141-01-02 415AL 416AR 425AL 

426AR 

GENERAL VISUAL INSPECTION OF INLET COWL ATTACHMENT (A1 FLANGE). 

8000 

 711200-01-02 415AL 416AR 425AL 

426AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). 

8000 

 711246-01-02 415AL 416AR 425AL 

426AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). 

8000 

 711301-02-02 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 

GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). 

8000 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 711302-02-02 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 

GENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). 

8000 

 711341-02-02 415AL 416AR 425AL 

426AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). 

8000 

 711343-02-01 415AL 416AR 425AL 

426AR 

GENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). 

8000 

 711345-02-01 414AL 414AR 424AL 

424AR 

GENERAL VISUAL INSPECTION OF CORE COWL DOOR HINGES AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). 

8000 

 711347-01-01 414AL 414AR 424AL 

424AR 

GENERAL VISUAL INSPECTION OF CORE COWL DOOR LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). 

8000 

 712102-01-01 417AL 418AR 427AL 

428AR 

DETAILED INSPECTION OF CF6-80E1 FORWARD ENGINE MOUNT EXCLUDING THE PLATFORM. 

4000 OR 3080

 712103-01-01 ENGINE 

FORWARD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT PLATFORM. 

6300 OR 6580

 712103-01-02 ENGINE 

FORWARD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT PLATFORM. 

6600 OR 6830

 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. 

2360 OR 2440
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 712105-01-01 ENGINE 

FWD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT THRUST TRUNNION. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8000 OR 3020

 712105-01-02 ENGINE 

FWD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT THRUST TRUNNION. 

8000 OR 3020

 712106-01-01 ENGINE 

FORWARD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT. 

8000 OR 5200

 712107-01-01 415AL 416AR 425AL 

426AR 417AL 418AR 427AL 428AR 

SPECIAL DETAILED INSPECTION OF PYLON BOLTS OF THE FORWARD ENGINE MOUNT 

4000 OR 3080

 712202-01-01 414AL 414AR 424AL 

424AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT EXCLUDING THE UPPER BEAM. 

8000 OR 6840

 712204-01-01 417AL 418AR 427AL 

428AR 

DETAILED INSPECTION OF AFT ENGINE MOUNT FAILSAFE LINK. NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH. 

4130 OR 4260

 712204-02-01 417AL 418AR 427AL 

428AR ENGINE ENGINE MOUNT 

DETAILED INSPECTION OF AFT ENGINE MOUNT FAILSAFE LINK. NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH. 

8000 OR 5200

R 712205-01-01 417AL 418AR 427AL 

428AR ENGINE 

SPECIAL DETAILED INSPECTION OF AFT ENGINE MOUNT LINKS NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FC OPTIMIZED 

8000 OR 3020

R 712205-01-02 417AL 418AR 427AL 

428AR ENGINE 

SPECIAL DETAILED INSPECTION OF AFT ENGINE MOUNT LINKS 

8000 OR 3020
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.1 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THR

 783200-01-02 417DL 417EL 418DR 

418ER 427DL 427EL 428DR 428ER 

GENERAL VISUAL INSPECTION OF THRUST RESERVER HINGES, SLEEVES, PINS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE FITTINGS). 

2000 

 783201-03-01 415BL 416BR 417AL 

418AR 425BL 426BR 427AL 428AR 

GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE ATTACHMENTS). 

8000 

 783201-04-01 415BL 416BR 417AL 

418AR 425BL 426BR 427AL 428AR 

GENERAL VISUAL INSPECTION OF THRUST REVERSER HINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND HINGE ATTACHMENTS). 

8000 

 783202-01-02 415BL 416BR 417AL 

418AR 425BL 426BR 427AL 428AR LATCH ACCESS DOOR 

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS). 

8000 

 783202-02-02 415BL 416BR 417AL 

418AR 425BL 426BR 427AL 428AR LATCH ACCESS DOOR 

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE (15 CM AROUND LATCH ATTACHMENTS). 

8000 

 783245-02-01 418HR 418JR 428HR 

428JR 

GENERAL VISUAL INSPECTION OF THRUST REVERSER LATCHES AND SURROUNDING STRUCTURE (15 CM AROUND LATCH FITTINGS). 

8000 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.2 AIRWORTHINESS LIMITATIONS

2-2 SECTION 2.2

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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

STRUCTURE, NOSE LANDING GEAR WELL PANELS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

1150 OR 6750 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 14410

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

COMPARTMENT DOOR CUTOUT, VISIBLE PART OF LATERAL FRAMES (FR 20A AND FR 25A). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 97400 

532126-01-01 832 842 

DOOR FRAME LINING INSULATION 

DETAILED INSPECTION OF DOOR 2, COVER PLATE OF TORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND STR 13, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17300 OR 10430

532127-01-01 832 842 

DOOR FRAME LINING NOTE 1 

DETAILED INSPECTION OF DOOR NO 2, FR 33, BETWEEN STR 13 AND STR 15, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15900 OR 10830
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

35200 OR 23960

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

35200 OR 23960

532158-01-02 833 843 

CEILING PANELS INSULATION 

SPECIAL DETAILED INSPECTION OF FUSELAGE CIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TO CROWN CENTER LINE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

35200 OR 23960
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533009-01-01 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 15810

533009-01-02 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-02NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26900 OR 17520

533009-01-03 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-03NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24600 OR 14790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533009-01-04 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 1 FASTENERS 

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 533009-02-04NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 15160

533009-02-01 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 15810

533009-02-02 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-02NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26900 OR 17520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533009-02-03 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-03NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24600 OR 14790

533009-02-04 251JC 251VW 252JC 

252VW OVERHEAD STOWAGE BINS NOTE 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 533009-01-04NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 15160

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 15810

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26900 OR 17520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24600 OR 14790

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

CIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWN CENTERLINE TO STRINGER 17, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 15160

533012-01-01 261CC 262CC 

OVERHEAD STOWAGE BINS NOTE 1 RIVETS 

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 533012-02-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27000 OR 16200

533012-02-01 261CC 262CC 

OVERHEAD STOWAGE BINS NOTE 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 533012-01-01NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27000 OR 16200

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28200 OR 19130
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27700 OR 18040

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25000 OR 16920

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24400 OR 16550

533016-01-03 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23500 OR 15900

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 17040
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 14360

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24500 OR 14710

533021-01-01 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8150 OR 55100 

533021-01-02 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7550 OR 49200 

533021-01-03 734 

744 

SPECIAL DETAILED INSPECTION OF RADII OF TEE FITTINGS CONNECTING HYDRAULIC BRACKET TO VERTICAL BEAMS Y=953 and Y=450, BELOW PRESSURE FLOOR, AT PRESSURE BULKHEAD FR 53,2, LH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7800 OR 51400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533104-01-03 ANTICOLLISION LIGHT: 

LENS 7LV ADF: 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33900 OR 22960

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19000 OR 12880

533106-01-03 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 16180

533107-01-03 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10800 OR 73600 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533107-01-04 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9900 OR 67200 

533107-01-05 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8900 OR 60800 

533107-01-06 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13900 OR 94200 

533107-01-07 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16700 OR 11300
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533107-01-08 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9200 OR 62500 

533107-01-09 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 11190

533107-01-10 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14900 OR 10130

533107-01-11 LINING 

NOTE 1 AIR CONDITIONING DUCTS 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 10410

533112-01-01 N/A SPECIAL DETAILED INSPECITON OF FUSELAGE 

EXTERNAL STRUCTURE, LONGITUDINAL JOINT AT STRINGER 39 AHEAD OF FRAME 53.2, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

37000 OR 25050
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533112-01-02 N/A SPECIAL DETAILED INSPECITON OF FUSELAGE 

EXTERNAL STRUCTURE, LONGITUDINAL JOINT AT STRINGER 39 AHEAD OF FRAME 53.2, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

34000 OR 22160

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8500 OR 58000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

5800 OR 39500 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7000 OR 47400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8050 OR 54600 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8900 OR 60300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8250 OR 56100 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15900 OR 10780

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11800 OR 80300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13100 OR 88700 

533115-01-04 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10300 OR 70300 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533115-01-05 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8500 OR 57900 

533115-01-06 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10400 OR 70700 

533115-01-07 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12500 OR 84800 

533115-01-08 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9400 OR 64000 

533115-01-10 251XW 252XW 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO 23, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11200 OR 76100 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533126-01-03 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

3800 OR 24700 

533126-01-05 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

3850 OR 26100 

533126-01-06 734 744 GENERAL VISUAL INSPECTION OF SKIN PANEL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

5000 OR 32800 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533127-03-01 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

3850 OR 26100 

533127-03-02 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

3800 OR 24700 

533127-03-03 FAIRING PANELS 

BETWEEN FR.39.1 AND FR.47 

DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

5000 OR 32800 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22100 OR 15010

R 533151-01-01 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13400 OR 90600 

R 533151-01-02 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11000 OR 74700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

R 533151-01-03 832 842 

GALLEYS AND TOILETS, IF INSTALLED. SIDEWALL LININGS AT FR 40 (LH/RH) 

DETAILED INSPECTION OF FR.40 FRONT FITTING AT STRINGER 21 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12200 OR 82500 

533155-01-01 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33900 OR 22090

533155-01-02 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27900 OR 18880

533155-01-03 251FG 252FG 

NOTE 1 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAME 46 CUTOUT AT STRINGER 28 LEVEL, LH/RH NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

34300 OR 23210

533156-01-01 822 

LINING NOTE 1 LD-MCR IF INSTALLED POST 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29200 OR 19800
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

533156-01-02 822 

LD-MCR IF INSTALLED OR POST 46678 LDL TOILETS AND FURNISHINGS LINING NOTE 1 

SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33200 OR 21600

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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15700 OR 10640

533164-01-03 734 744 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 10630

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20900 OR 13630

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22300 OR 15100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17200 OR 11660

533165-01-02 251MG 251SG 252MG 

252SG NOTE 1 GALLEYS & TOILETS IF INSTALLED 

DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, FRAMES 48 TO 53.1 HORIZONTAL LEG AT STRINGER PASSAGE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10300 OR 69900 

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20100 OR 13630

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14500 OR 98400 

R 533180-01-05 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24600 OR 16660
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20400 OR 13810

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 99500 

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 17040

R 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21400 OR 14490
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

R 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20700 OR 14000

533187-01-01 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23500 OR 15900

533187-01-02 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22100 OR 15010

533187-01-03 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18700 OR 12670

533187-01-05 CABIN FLOOR PANELS 

GALLEYS & TOILETS IF INSTALLED 

SPECIAL DETAILED INSPECTION OF LARGE MEMBRANES AROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17800 OR 12070

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 11200
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10000 OR 68200 

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 11180

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 11200

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21500 OR 14560

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 13740
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 99900 

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

AT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 13440

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 13440

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10000 OR 68200 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 11180
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 11200

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21500 OR 14560

533195-02-09 834 844 

SCUFF PLATE 

SPECIAL DETAILED INSPECTION OF DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT, STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 13740

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 97300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 13440
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26500 OR 17960

534104-01-08 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS, 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7300 OR 49600 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33700 OR 20240

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28000 OR 17220
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21100 OR 13730

534107-01-02 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS, INSULATION 

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28300 OR 18320

534107-01-04 833 843 

CEILING PANELS OVERHEAD STOWAGE BINS INSULATION 

SPECIAL DETAILED INSPECTION OF SPLICE PLATE AT CIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TO STR 7, AND STR 11 TO STR 13, AT INTERSECTION OF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21100 OR 13730

R 534108-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAS AT FR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28500 OR 18560

R 534110-01-02 N/A DETAILED INSPECTION OF FUSELAGE SKIN IN 

CIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80 FROM STR 6 TO STR 13 LH/RH, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28500 OR 18560
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16400 OR 10690

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8000 OR 52500 

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8700 OR 52300 

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

PASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8000 OR 52400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 13100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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

COMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL FRAMES (FR 59A AND 65) AS FAR AS VISIBLE.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 97400 

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

4400 OR 29200 

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7000 OR 42200 

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

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6900 OR 45300 

534143-01-06 N/A DETAILED INSPECTION OF SKIN OF BULK CARGO 

COMPARTMENT DOOR CUT-OUT AT UPPER CORNERS, EXTERNAL SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

4700 OR 28400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

534144-01-02 823 

SCUFF PLATE 

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18600 OR 11170

534144-01-04 823 

SCUFF PLATE 

DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21100 OR 13730

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20600 OR 13950

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12100 OR 81900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545104-02-04 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12500 OR 84600 

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. (2 FASTENER LOCATIONS/PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10800 OR 73100 

545104-02-12 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11800 OR 76700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545104-02-13 415AL 415BL 416AR 

416BR 425AL 425BL 426AR 426BR 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12200 OR 79300 

545104-02-14 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10500 OR 68200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545108-03-01 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

5600 OR 36400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545108-03-03 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

4700 OR 30500 

545108-03-09 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8500 OR 57500 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545108-03-11 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6600 OR 44600 

545108-03-12 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8100 OR 52600 

545108-03-14 415AL 416AR 425AL 

426AR 

DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINE FORWARD MOUNT FITTING TO RIB 1 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6300 OR 40900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545129-01-03 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21200 OR 14350
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545129-01-04 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21200 OR 14350

R 545129-01-09 454DL 454DR 464DL 

464DR 

DETAILED INSPECTION OF PYLON AFT UPPER SPAR, WEB CUTOUT BETWEEN RIB 16 AND RIB 17 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24300 OR 16450
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 17730

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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 16700

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 17730
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 11 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-12 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 16700

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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10500 OR 63000 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545140-01-02 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 545140-02-02. 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 (3770 FC OR 11310 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11200 OR 67200 

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (3060 FC OR 9180 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7900 OR 47400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545140-01-06 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 545140-02-06. 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 (4560 FC OR 22800 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9900 OR 64300 

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (3620 FC OR 18090 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10600 OR 68900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (2930 FC OR 14680 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7500 OR 48700 

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. 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) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10500 OR 63000 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL (7100 FC OR 21310 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11200 OR 67200 

545140-02-03 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 545140-01-03. 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 (5630 FC OR 16900 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7900 OR 47400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (7290 FC OR 36450 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9900 OR 64300 

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. 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 ALI INTERVAL (6810 FC OR 34080 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10600 OR 68900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 A330-54A3025 FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL (5400 FC OR 27030 FH) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7500 OR 48700 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10500 OR 63000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11200 OR 67200 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7900 OR 47400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9900 OR 64300 

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

PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL, EXTERNAL SURFACE,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10600 OR 68900 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7500 OR 48700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6900 OR 46700 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6200 OR 41900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11300 OR 76500 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9500 OR 64300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10800 OR 70200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9100 OR 59100 

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 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6800 OR 44200 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

6000 OR 39000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22900 OR 15500
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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 11 NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-13 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23200 OR 15700

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22900 OR 15500

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. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-13 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23200 OR 15700
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545146-03-01 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28700 OR 19420

545146-03-02 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22200 OR 15020
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545146-03-04 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28000 OR 18950

545146-03-06 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26800 OR 17420

545146-03-07 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-04-07NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28100 OR 18260
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545146-03-08 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-04-08NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21700 OR 14100

545146-04-01 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28700 OR 19420
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545146-04-02 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22200 OR 15020

545146-04-04 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28000 OR 18950

545146-04-06 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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.NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26800 OR 17420
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545146-04-07 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-07NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28100 OR 18260

545146-04-08 452AL 453BL 453BR 

462AL 463BL 463BR PRE-COOLER RODS, 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 545146-03-08NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21700 OR 14100

545150-02-01 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 12600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545150-02-02 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24100 OR 15360

545150-02-08 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

31300 OR 18780

545150-02-09 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29500 OR 19170
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545150-02-10 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29800 OR 18960

545150-02-11 452AL 462AL 

PRE-COOLER RODS AIR DUCT 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33300 OR 21640

545150-02-14 452AL 462AL 

AIR DUCT PRE-COOLER RODS 

DETAILED INSPECTION OF PYLON, UPPER SPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

35300 OR 21180
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24900 OR 16850
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545168-02-13 452CL 452CR 462CL 

462CR 454BL 454BR 464BL 464BR 

DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20400 OR 13810

545174-02-03 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545174-02-06 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000

545174-02-07 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000

R 545174-02-09 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545174-02-12 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000

545174-02-13 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000

545174-02-14 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

545174-02-15 PRE 43271: 

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

DETAILED INSPECTION OF PYLON TO WING ATTACHEMENT FITTING AND LINKS AT RIB 18A. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33000 OR 10000

545180-04-04 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 97800 

545180-04-05 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15400 OR 92400 

545180-04-06 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14200 OR 92300 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

R 545180-04-07 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15000 OR 97500 

545180-04-11 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16600 OR 99600 

545180-04-12 ENGINE 

LINKS SLEEVES AFT SECONDARY STRUCTURE 

SPECIAL DETAILED INSPECTION OF PYLON TO WING ATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3 PLACES PER PYLON) NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 99400 

551008-01-06 312AR 

313AL 

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 10410

551008-01-07 312AR 

313AL 

DETAILED INSPECTION OF HORIZONTAL STABILIZER CENTER BOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGE FAIRING LINES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 10410
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

551015-01-04 312AR GENERAL VISUAL INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX FRONT SPAR FORWARD FACE FROM RIB 3 LH TO RIB 3 RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16900 OR 11480

551016-01-06 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26500 OR 17970

551016-01-07 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN REAR UPPER FLANGE JUST OUTBOARD OF RIB 3, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26500 OR 17970

551019-01-04 313AL SPECIAL DETAILED INSPECTION OF HORIZONTAL 

STABILIZER CENTER BOX TOP SKIN INTERGRAL FLANGE AT ATTACHMENT TO REAR SPAR WEB FROM RIB 3 LH TO RIB 3 RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18900 OR 12840

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

BOX LOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN STRINGERS 20 & 21, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 17120

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24900 OR 16860
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571108-01-05 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29600 OR 20060

571108-01-06 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, LOWER SKIN PANEL AND STIFFENERS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29400 OR 19150

571114-01-05 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25000 OR 16960

571114-01-06 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19900 OR 12960

571114-01-07 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27 AND 28. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22100 OR 15010

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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 17120
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24900 OR 16860

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 17120

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24900 OR 16860

571121-01-03 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1959 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24500 OR 15280

571121-01-04 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1960 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25500 OR 15300
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571121-01-05 734 744 SPECIAL DETAILED INSPECTION OF FUSELAGE 

INTERNAL STRUCTURE, LONGITUDINAL BEAM FITTING AND LONGITUDINAL BEAM AT JUNCTION WITH CWB AFT PANEL FROM Y=-1959 TO Y=1961 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24500 OR 15940

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19900 OR 11960

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18500 OR 11120

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14100 OR 91700 

571123-01-04 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19000 OR 11400

571123-01-05 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 95700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23400 OR 15880

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16700 OR 10870

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18200 OR 12330

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 17410

571126-01-04 734 SPECIAL DETAILED INSPECTION OF CENT WING BOX, 

REAR SPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE LOWER CORNER. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21000 OR 13650

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22400 OR 15160
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571129-01-04 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

34300 OR 23210

571130-01-03 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUTOUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

34300 OR 23210

R 571130-01-04 147AZ 148AZ 734 

744 

SPECIAL DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR, 30 MM AROUND MANHOLE CUTOUTS (2 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

31800 OR 20700

571133-01-01 147AZ 148AZ 734 

744 

DETAILED INSPECTION OF CENTER WING BOX, STRUT LUGS ON LONGITUDINAL STIFFENERS AND ROD FITTING CONNECTIONS (63 PLACES). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24300 OR 15850

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

31100 OR 21100
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571145-01-01 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26100 OR 17680

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25100 OR 16360

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 17390

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24600 OR 15990

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27100 OR 18340
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 17740

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22100 OR 14390

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23300 OR 15780

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22400 OR 14560
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23600 OR 15990

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 11170

571153-01-01 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17200 OR 11660

571153-01-02 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16600 OR 10790
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571153-01-03 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10900 OR 73900 

571153-01-04 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 10350

R 571153-01-05 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16600 OR 11290

571153-01-06 147AZ 148AZ 

734 744 SEALANT 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 95800 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26400 OR 17920

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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23800 OR 15500

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). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25100 OR 17000

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11500 OR 78200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

R 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11000 OR 74800 

R 571163-01-02 191HB 192HB SPECIAL DETAILED INSPECTION OF FRAME 40 NODE, 

FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAM FITTING AND LOWER PANEL, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9700 OR 63100 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

571164-01-02 191HB 192HB DETAILED INSPECTION OF FUSELAGE EXTERNAL 

STRUCTURE, KEEL BEAM FITTING ANGLE AND DOUBLER AT FR 40, LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16400 OR 10690

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9300 OR 63400 

 572002-01-05 454DL 454DR 454FL 

454FR 464DL 464DR 464FL 464FR 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24400 OR 14640

572002-01-08 454KL 454KR 454ML 

454MR 464KL 464KR 464ML 464MR 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIB BAY 10-10A NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24400 OR 14640

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23400 OR 15270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24500 OR 14720

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 14380

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 14380

572005-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18900 OR 11360

572005-01-07 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19600 OR 12750
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20800 OR 12530

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20800 OR 12530

572005-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18900 OR 11360

572006-02-09 N/A GENERAL VISUAL INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27000 OR 17550

572006-02-10 N/A GENERAL VISUAL INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24300 OR 14610
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572009-01-04 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 12930

572009-01-05 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20200 OR 12100

572009-01-06 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUN-OUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19900 OR 11970
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572009-02-04 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 12930

572009-02-05 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20200 OR 12100

572009-02-06 454GL 454GR 464GL 

464GR 531AB 631AB INBOARD FUEL PUMP FAIRING 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3) NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19900 OR 11970
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24800 OR 16160

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20500 OR 12320

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26100 OR 15680

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26700 OR 16060

572016-02-08 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21000 OR 12640
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572016-02-09 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN VISIBLE SURFACES OF FUEL PUMP APERTURES BETWEEN RIB 2 AND RIB 4. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15700 OR 10220

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 16430

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24200 OR 14570

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26000 OR 15600

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20100 OR 13110
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18500 OR 11120

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21600 OR 12990

572027-01-05 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23600 OR 15370

572027-01-06 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20200 OR 12130

572027-01-10 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAP AT STRINGER 13 & STRINGER 20 BETWEEN RIB 1 AND RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24800 OR 14890
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9600 OR 62900 

 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15900 OR 47300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10100 OR 61000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10100 OR 61000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9600 OR 62900 

572032-01-12 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13000 OR 78300 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14500 OR 94300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 95100 

572033-01-06 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 86200 

572033-01-08 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 86200 

572033-01-09 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14500 OR 94300 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25100 OR 15060
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572037-01-05 541AB 541AZ 541BB 

541BZ 541CB 541CZ 541DB 541DZ 541EZ 541FZ 641AB 641AZ 641BB 641BZ 641CB 641CZ 641DB 641DZ 641EZ 641FZ 

DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9 AND TOP SKIN LOWER SURFACE AT ROOT JOINT FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22200 OR 13340

572043-01-05 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25100 OR 15070

572043-01-06 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33100 OR 19900

572043-01-10 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

32300 OR 19410

572043-01-11 573FB 673FB DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28400 OR 18490

572046-01-04 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23300 OR 15180
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572046-01-05 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 12180

572046-01-07 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22900 OR 13770

572046-01-09 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20700 OR 13450

572046-01-11 541AB 541BB 541CB 

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

DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21000 OR 12620

572047-01-03 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 17040
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572047-01-04 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26100 OR 15660

572047-01-05 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24500 OR 14710

572047-01-06 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29900 OR 17980

572047-01-09 541AB 541BB 541BZ 

541CB 541CZ 641AB 641BB 641BZ 641CB 641CZ SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARD PINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAY FITTING) BOLTING AREAS AND TOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27800 OR 18070

572049-01-04 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22400 OR 14590
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572049-01-05 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

30800 OR 18510

572049-01-06 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22500 OR 13530

572049-01-08 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21200 OR 12760

572049-01-09 531AB 631AB SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19200 OR 12520

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26700 OR 17360

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17900 OR 10770
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27600 OR 16600

572050-01-09 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21300 OR 13890

572050-01-10 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 14340

572050-01-11 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23900 OR 14340

572050-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21300 OR 13890
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572051-01-05 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15300 OR 99900 

572051-01-06 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23700 OR 14260

572051-01-07 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9700 OR 58600 

572051-01-08 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15500 OR 93300 

572051-01-10 FLAPS EXTENDED 

SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18200 OR 11830

572051-01-12 DEPLOY FLAPS 

SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22300 OR 13410

 572052-03-01 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20900 OR 96500 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

 572052-03-02 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16000 OR 51200 

572052-03-04 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17700 OR 10670

572052-03-05 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17800 OR 10690

 572052-03-06 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23600 OR 73900 

 572052-03-07 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23600 OR 73900 

 572052-03-08 541BB 541CB 641BB 

641CB SEALANT REMOVAL AS PER NTM. 

SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOP AND BOTTOM FLANGE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 11930
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572054-01-05 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 10300

572054-01-07 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11600 OR 70000 

572054-01-08 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15000 OR 90400 

572054-01-10 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13700 OR 89400 

572054-01-11 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12700 OR 76300 

572054-01-13 DEPLOY FLAPS SPECIAL DETAILED INSPECTION OF OUTER WING 

REAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10520
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572067-01-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12800 OR 77000 

572067-01-15 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29500 OR 17710

572067-01-17 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19200 OR 11560
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572067-03-03 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 641FZ 

SPECIAL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19200 OR 11560

R 572067-03-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 641FZ 

SPECIAL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29500 OR 17710

572068-01-04 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 16750
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572068-01-05 541CB 541DB 541EZ 

541FZ 641CB 641DB 641EZ 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26200 OR 15720

R 572068-01-13 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18600 OR 11190

R 572069-01-04 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18400 OR 11960

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 94800 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 94800 

R 572069-01-08 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19800 OR 11880

572069-01-11 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23100 OR 13860

572069-01-12 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22000 OR 14300

572081-01-05 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18700 OR 12170
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572081-01-06 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14800 OR 89300 

572081-01-07 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19700 OR 11830

572081-01-08 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10540

572081-01-13 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 10850

572081-01-14 541AB 541AZ 641AB 

641AZ 

DETAILED INSPECTION OF OUTER WING CENTER SPAR ASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 11750

572082-01-06 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15200 OR 91200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572082-01-08 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23000 OR 13800

572082-01-10 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23000 OR 14950

572082-01-12 541AB 541AZ 541BB 

541CB 541DB 541DZ 541EB 541EZ 541FB 541FZ 641AB 641AZ 641BB 641CB 641DB 641DZ 641EB 641EZ 641FB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25200 OR 15140

572084-01-01 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26700 OR 18090

572084-01-03 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19200 OR 12480
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572084-01-04 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19600 OR 13260

572084-01-05 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18700 OR 12200

572084-01-06 541AB 641AB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20600 OR 13990

572092-01-04 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19500 OR 12700

572092-01-05 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18200 OR 10950
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572092-01-06 541EB 541FB 641EB 

641FB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 AND RIB 12, EXCLUDING JOINT OF STRINGER 15 TO CENTER SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20500 OR 12300

572093-01-07 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 572093-02-07 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20000 OR 12050

572093-01-08 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 572093-02-08 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17400 OR 10470

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 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20000 OR 12050
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572093-02-08 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 572093-01-08 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17400 OR 10470

572094-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23400 OR 14080

572107-01-05 N/A SPECIAL DETAILED INSPECTION OF OUTER WING 

BOTTOM SKIN LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-05 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20800 OR 12520

572107-02-05 N/A DETAILED INSPECTION OF OUTER WING BOTTOM SKIN 

LOWER SURFACE AT RUNOUTS OF STRINGER BETWEEN RIB 23 AND RIB 39. NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-05 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20800 OR 12520

572109-02-05 542EB 542FB 542GB 

542HB 542JB 542KB 550AB 550BB 550CB 550DB 550EB 550FB 642EB 642FB 642GB 642HB 642JB 642KB 650AB 650BB 650CB 650DB 650EB 650FB 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN UPPER AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20500 OR 12340
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20100 OR 13120

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21300 OR 12820

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21600 OR 12990

572111-01-04 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13400 OR 87400 

572111-01-05 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13700 OR 82600 

572111-01-06 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 86200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572111-01-09 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21900 OR 14240

572111-01-10 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25400 OR 15250

572111-01-11 532AB 532CB 533AB 

533CB 534AB 534CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN LOWER SURFACE IN AREAS COVERED BY FLAP TRACK FAIRINGS 3,4 AND 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21900 OR 14240

572116-02-01 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 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23600 OR 15350

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 & 5. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23800 OR 14330
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572119-02-05 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

32000 OR 11210

572121-01-04 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16400 OR 10700

572121-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17000 OR 10250

572121-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10540
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572121-01-08 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24800 OR 16180

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 11700

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20700 OR 12470

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. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-02-06. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17800 OR 10730
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572125-02-04 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-06. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 11700

572125-02-05 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-07. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20700 OR 12470

572125-02-06 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572125-01-08. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17800 OR 10730

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 AS TASK 572129-02-03. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18900 OR 11380
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572129-02-03 541SB 641SB 

SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572129-01-03. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18900 OR 11380

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26500 OR 17240

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24900 OR 14980

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27900 OR 16760

572133-01-10 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27900 OR 16760
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572133-01-11 N/A DETAILED INSPECTION OF OUTER WING TOP SKIN 

UPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPAR TO REAR SPAR. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26500 OR 17240

572140-01-05 541EB 541FB 541GB 

541HB 541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641EB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

29000 OR 17400

572153-01-04 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26000 OR 16930

572153-01-05 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 10840

572153-01-11 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

30100 OR 18090

572153-01-12 574AT 674AT DETAILED INSPECTION OF OUTER WING REAR SPAR 

AFT FACE SPAR JOINT PLATE AT RIB 27. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24200 OR 15780
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572154-01-04 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14000 OR 91300 

572154-01-05 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14100 OR 84800 

572154-01-06 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12200 OR 73700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572154-01-09 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12200 OR 79900 

572154-01-10 541FB 541GB 541HB 

541JB 541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641FB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13100 OR 78600 

572158-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18000 OR 11730

572158-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17400 OR 10490
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572158-01-10 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN BUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 11580

572158-01-12 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24300 OR 15850

572164-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27700 OR 18040

572164-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22100 OR 13270
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572164-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

26300 OR 15820

572164-01-11 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 16750

572164-01-12 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 542AB 542BB 542CB 542DB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 642AB 642BB 642CB 642DB 

DETAILED INSPECTION OF OUTER WING FRONT SPAR AFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP AND BOTTOM FLANGES. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25700 OR 15460

572180-01-04 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13900 OR 90400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572180-01-05 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14200 OR 85300 

572180-01-06 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14800 OR 88800 

572180-01-07 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24100 OR 14490

572180-01-09 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20900 OR 13600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572180-01-10 541GB 541HB 541JB 

541KB 541LB 541MB 541NB 541PB 541QB 541RB 541SB 641GB 641HB 641JB 641KB 641LB 641MB 641NB 641PB 641QB 641RB 641SB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20900 OR 13600

572183-01-04 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14600 OR 94900 

572183-01-05 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 99300 

572183-01-06 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 88200 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572183-01-07 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-7 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 11600

572183-01-08 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 11370

572183-01-10 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-10 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 11600

572183-01-11 542DB 542EB 642DB 

642EB 

DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-02-11 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 11370
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572183-02-04 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-4 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14600 OR 94900 

572183-02-05 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-5 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16500 OR 99300 

572183-02-06 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-6 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14700 OR 88200 

572183-02-07 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-7 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 11600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572183-02-08 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-8 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 11370

572183-02-10 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-10 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19300 OR 11600

572183-02-11 542DB 542EB 642DB 

642EB SEALANT REMOVAL AS PER NTM 

SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28 INCLUDING STRINGER JOINTS. NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK 572183-01-11 NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 11370

572606-01-02 532CB 533CB 534CB 

632CB 633CB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22300 OR 13410
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

572606-01-03 532CB 533CB 534CB 

632CB 633CB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4 AND 5 AFT PICK-UP, ASSEMBLY. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20600 OR 13410

572607-01-01 531AB 531CB 532AB 

532CB 533AB 533CB 534AB 534CB 631AB 631CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25400 OR 15280

572607-01-07 531AB 531CB 532AB 

532CB 533AB 533CB 534AB 534CB 631AB 631CB 632AB 632CB 633AB 633CB 634AB 634CB 

DETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23500 OR 15280

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 10650

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10500

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17600 OR 10570
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

573002-01-05 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 10650

573002-01-07 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10500

573002-01-08 N/A DETAILED INSPECTION OF WINGTIP BOX TOP SKIN 

UPPER SURFACE AND BOTTOM SKIN LOWER SURFACE. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17600 OR 10570

573003-02-04 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19900 OR 12940

573003-02-05 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20400 OR 12240

573003-02-10 WINGLET SPECIAL DETAILED INSPECTION OF WINGTIP TO 

WINGLET FORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET). NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21400 OR 12850
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-04 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16300 OR 10600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-05 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 95100 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-06 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17500 OR 10530
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-07 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22000 OR 14350
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-11 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22000 OR 14350
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574106-01-12 521BB 521CB 521DB 

521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 

DETAILED INSPECTION OF OUTER WING FIXED LEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ON TRACK RIB 1 TO TRACK RIB 16. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23100 OR 13900

574107-02-04 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

24000 OR 15600
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574107-02-05 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27800 OR 16690

574107-02-06 521FB 521GB 521HB 

521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

27300 OR 16400
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574109-02-01 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9100 OR 59700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574109-02-02 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8900 OR 53600 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574109-02-03 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13000 OR 78400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574109-02-05 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12400 OR 80900 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574109-02-07 521AB 521BB 521CB 

521DB 521EB 521FB 521GB 521HB 521JB 522AB 522BB 522CB 522DB 522EB 522FB 522GB 522HB 522JB 522KB 522LB 522MB 522NB 522PB 522QB 522RB 522SB 523CB 523DB 523EB 523FB 523GB 523HB 523JB 523KB 523LB 523MB 523NB 523PB 621AB 621BB 621CB 621DB 621EB 621FB 621GB 621HB 621JB 622AB 622BB 622CB 622DB 622EB 622FB 622GB 622HB 622JB 622KB 622LB 622MB 622NB 622PB 622QB 622RB 622SB 623CB 623DB 623EB 623FB 623GB 623HB 623JB 623KB 623LB 623MB 623NB 623PB 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9800 OR 59300 

574110-02-01 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22400 OR 14610
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574110-02-02 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23500 OR 14100

574110-02-03 N/A DETAILED INSPECTION OF OUTER WING FIXED 

LEADING EDGE BOTTOM SKIN OVERHANG LOWER SURFACE FORWARD OF FRONT SPAR FROM RIB 1 TO RIB 9. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22500 OR 13510

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21500 OR 13970

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

22400 OR 13480

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 12230
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

20300 OR 12230

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11500 OR 74900 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

12900 OR 77400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10700 OR 64700 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10700 OR 64700 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

574115-02-07 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21100 OR 12710

574115-02-09 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

23300 OR 15170

574804-01-03 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 6, SKIN 

CONNECTIONS AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10300 OR 61900 

574804-02-04 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONS 

AT TRACK RIB AND HOLD DOWN RIB STATIONS, EXTERNAL,LH/RH. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10300 OR 61900 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

30300 OR 19700
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

575011-01-05 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16100 OR 96800 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33600 OR 20200

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

33600 OR 20200

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

30300 OR 19700

575011-01-13 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE TOP SKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 14. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

32100 OR 19280

575012-01-02 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15400 OR 10020
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

575012-01-03 N/A DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BY FLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OF REAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19000 OR 11420

575012-01-06 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

16000 OR 96300 

575014-01-06 573DB 673DB SPECIAL DETAILED INSPECTION OF OUTER WING 

TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BY MLG REINFORCING. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

28600 OR 17200

575016-01-05 531AB 631AB DETAILED INSPECTION OF OUTER WING TRAILING 

EDGE BOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25800 OR 15530

575018-01-03 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

15800 OR 10300
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

575018-01-04 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18300 OR 11030

575018-01-05 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17000 OR 10230

575018-01-06 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17900 OR 10780

575018-01-07 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17900 OR 10780

575018-01-08 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17100 OR 11120

575018-01-09 147AT 148AT 191CT 

192CT DEPLOY FLAPS 

DETAILED INSPECTION OF OUTER WING TRAILING EDGE ATTACHMENT OF SHROUD BOX. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

17100 OR 11120
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9700 OR 63400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

9200 OR 55700 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

8800 OR 57500 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10200 OR 61400 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25900 OR 16850

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

19700 OR 69000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

11600 OR 69700 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13200 OR 79400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10700 OR 64500 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

14300 OR 50000 

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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18200 OR 10920

575067-02-02 FWD FLAP TRACK 

FAIRINGS FAIL 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. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

18200 OR 10920

576105-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

10700 OR 70400 
A330 AIRWORTHINESS LIMITATIONS SECTION

ISSUE: 23 MAR 2012 ALI SECTION 2.2 

EASA APPROVED 

©AIRBUS SAS 2012. All rights reserved.

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRE

576108-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF OUTER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

25000 OR 16340

576115-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWER FLANGERADIUS AT LUG SIDE OF HINGE1. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

21900 OR 14300

576118-01-01 FAIRING 

PANEL 

SPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

13900 OR 94500 

712105-01-01 ENGINE 

FWD ENGINE MOUNT DISASSEMBLED 

SPECIAL DETAILED INSPECTION OF FORWARD ENGINE MOUNT THRUST TRUNNION. NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7100 OR 47900 

712205-01-01 417AL 418AR 427AL 

428AR ENGINE 

SPECIAL DETAILED INSPECTION OF AFT ENGINE MOUNT LINKS NOTE: THE THRESHOLDS/INTERVALS OF THIS MAINTENANCE REQUIREMENT ARE FH OPTIMIZED 

7100 OR 47900 
A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA -1 

©AIRBUS SAS 2012. All rights reserved. 

1 SUMMARY OF CHANGES

Section 1 INTRODUCTION

The WV 062 has been added in the applicability table for A330/200 aircraft. 

The WV 055 has been added in the applicability table for A330/300 aircraft. 

Section 2 AIRWORTHINESS LIMITATIONS:

REV 

CODE 

TASK 

REFERENCE SUMMARY OF CHANGES 

SECTION 2-1 

STANDARD 

(SR) 

SECTION 2-2

ALTERNATIVE 

(LR) 

R 531144-01-03 Task number updated x 

R 531186-01-02 Applicability updated x 

R 532152-01-01 Task number updated x 

R 533010-01-02 Applicability updated x x 

R 533151-01-01 Access updated x x 

R 533151-01-02 Access updated x x 

R 533151-01-03 Access updated x x 

R 533152-01-06 Task number updated x 

R 533180-01-05 Interval updated x 

R 533181-01-06 Applicability updated x x 

R 533181-01-07 Applicability updated x x 

R 533195-02-04 Threshold updated x 

R 533197-01-01 Note updated in task description x 

R 533197-02-01 Note updated in task description x 

R 534108-01-02 Task number updated x x 

R 534110-01-02 Task number updated x x 

R 545129-01-09 Applicability updated x x 

R 545174-02-09 Threshold udpated x 

R 545180-04-07 Threshold udpated x 

R 571102-01-01 Applicability updated x 

R 571102-01-02 Applicability updated x 

R 571102-01-07 Applicability updated x 

R 571104-01-04 Applicability updated x 

R 571130-01-04 Applicability updated x x 

R 571153-01-05 Applicability updated x x 

R 571163-01-01 Applicability updated x x 

R 571163-01-02 Applicability updated x x 

D 572022-01-04 Task kept for historical reference x 

D 572022-01-05 Task kept for historical reference x 

D 572022-01-06 Task kept for historical reference x 

D 572022-01-07 Task kept for historical reference x 

R 572067-03-05 Applicability updated x x 
A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA -2 

©AIRBUS SAS 2012. All rights reserved. 

REV 

CODE 

TASK 

REFERENCE SUMMARY OF CHANGES 

SECTION 2-1 

STANDARD 

(SR) 

SECTION 2-2

ALTERNATIVE 

(LR) 

R 572068-01-13 Interval updated x 

R 572069-01-04 Interval updated x 

R 572069-01-08 Interval updated x 

D 572166-01-05 Task kept for historical reference x 

R 712205-01-01 Threshold/Interval updated x 

R 712205-01-02 Threshold/Interval updated x 

APPENDIX A SUMMARY OF CHANGES

Correction of ALI Rev 18 Summary of Changes further to identified anomalies: 

REV 

CODE 

TASK 

REFERENCE SUMMARY OF CHANGES 

SECTION 2-1 

STANDARD 

(SR) 

SECTION 2-2

ALTERNATIVE 

(LR) 

R 523104-01-02 Interval updated x 

R 523204-01-02 Interval updated x 

R 531142-02-02 Interval updated x 

R 532148-01-02 Threshold and interval updated x 

R 532166-02-03 Note updated in the description x 

R 533014-01-02 Threshold/Interval updated 

Note added in the description 

Applicability updated 

x x 

R 533115-01-06 Threshold/Interval updated 

Note added in the description 

x x 

R 533115-01-07 Threshold/Interval updated 

Note added in the description 

x x 

R 533126-01-03 Threshold/Interval updated 

Description updated 

Note added in the description 

x x 

R 533126-01-05 Threshold/Interval updated 

Description updated 

Note added in the description 

x x 

R 533126-01-06 Threshold/Interval updated 

Description updated 

Note added in the description 

x x 

R 534132-02-01 Applicability updated x 

R 545138-02-03 Threshold updated 

Note added in the description 

Applicability updated 

x x 

N 571164-01-02 New task x x 

R 572047-01-04 Threshold updated 

Note added in the description 

x x 

R 572052-03-08 Threshold updated 

Interval updated 

Note added in the description 

Applicability updated 

x x 
A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA -3 

©AIRBUS SAS 2012. All rights reserved. 

REV 

CODE 

TASK 

REFERENCE SUMMARY OF CHANGES 

SECTION 2-1 

STANDARD 

(SR) 

SECTION 2-2

ALTERNATIVE 

(LR) 

R 572069-01-04 Threshold updated 

Note added in the description 

x x 

R 572069-01-08 Threshold updated 

Note added in the description 

Applicability updated 

x x 

R 572164-01-12 Threshold/Interval updated 

Note added in the description 

Applicability updated 

x x 

R 574106-01-06 Threshold updated 

Note added in the description 

Applicability updated 

x x 

R 574106-01-11 Threshold updated 

Note added in the description 

x x 

R 574106-01-12 Threshold updated 

Note added in the description 

x x 

R 575018-01-05 Threshold updated 

Note added in the description 

Applicability updated 

x x 

R 575018-01-06 Threshold updated 

Note added in the description 

x x 

R 575018-01-07 Threshold updated 

Note added in the description 

x x 

R 575018-01-08 Threshold updated 

Note added in the description 

x x 

R 575401-02-01 Applicability updated x 

R 712105-01-01 Threshold/Interval updated 

Note added in the description 

Applicability updated 

x x 
A330 Airworthiness Limitation Items

APPENDIX B – ABBREVIATIONS

ISSUE: 23 MAR 2012 PAGE: APXB -1 

©AIRBUS SAS 2012. All rights reserved. 

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 
A330 Airworthiness Limitation Items

APPENDIX C – TERMS AND DEFINITIONS

ISSUE: 23 MAR 2012 PAGE: APXC -1 

©AIRBUS SAS 2012. All rights reserved. 

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. 
A330 Airworthiness Limitation Items

ISSUE: 23 MAR 2012 

©AIRBUS SAS 2012. All rights reserved. 

INTENTIONALLY LEFT BLANK