# AIRBUS

Customer Services Directorate



# A330 Airworthine ss Limitation Items



# A330

Airworthiness Limitation Items

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

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

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

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

purposes of performing t he tasks described hereunde r and provided that an y recipient of such

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

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

for which it is supplied. 

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

28 May 2010

Issue 17

# AIRWORTHINESS LIMITATION ITEMS

TABLE OF CONTENTS

SUBJECT SECTION

ISSUE: 28 MAY 2010 PAGE: 1-TOC

© AIRBUS SAS 2010. All rights reserved. 

# A330

RECORD OF REVISIONS ROR

INTRODUCTION 1

GENERAL 1-1

Airworthiness Limitations 1-1- A

RULES FOR COMPLIAN CE DEMONSTRATION 1-2

General 1-2- A

Conditions for DT ALI inspection 1-2- B

Reporting 1-2- C

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

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

LIMIT OF VALIDITY (LOV) 1-3

APPLICABILITY 1-4



# General 1-4- A

Weight Variant (WV) applicability 1-4- B



# Applicability System 1-4-C

EXPLANATION OF SECTION 2 TABLE FORMAT 1-5

AIRWORTHINESS LIMITATIONS 2

SUMMARY OF CHANGES APPENDIX A



# ABBREVIATIONS APPENDIX B



# TERMS AND DEFINITIONS APPENDIX C

# AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 1-ROR

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. 

# A330

Issue Date Reason for revision Approved

by EASA

1 22 Aug 97 Section 2 of CMR documents originally identified

‘Structural Inspections’ These are not CMRs. New

document created.

Target date for inclusion of these requirements in

MRB report extended from 1998 to 1999.

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

Document retitled ‘Airworthiness Limitation Items’.

It was originally called ‘Structural Inspection

Requirements’.

Text of Section 1 modified to refer to A330-200

and to add a new paragraph to justify

acceptability of 1999 target date.

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

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

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

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

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

Text of Section 1 modified to revise target dates

for publication of ALIs.

8 31 Oct 01 Document completely revised to introduce ALIs

following completion of the full scale fatigue test

and teardown analysis.

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

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

025 added for A330-300. Reference to Zonal

Program deleted from paragraph 1.5.

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

052 in new WV GROUP 33E. New DSG added

for GROUP 33E. To provide compatibility with

MRBR and MPD, task numbering changed to 9

digits and applicability amended.

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

engines (A330-300 WV 051) included.

Tasks that were deleted in Issue 10 reintroduced.

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

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

included.

Requirements of WV GROUP 33E for RR

# AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 2-ROR

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. 

# A330

Issue Date Reason for revision Approved

by EASA

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

Requirements for enhanced modifications

embodied on non-fully enhanced aircraft

included.

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

A330-303.

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

WV022) included.

Task applicabilities changed due to impact of

product improvement mods for A330 WV000 up

to WV030 series.

New numbering rules (ALI task previously with 9

digits replaced by 10 Digit number system)

included in section 2.

WV053, 054, 055 added for Group 32E.

WV027 added for Group 32A.

WV026, 027 added for Group 33C.

WV053 added for Group 33E.

Confidentiality statement added. Approved by

EASA

under reference

EASA.A.C.01277

on 17 January 2006

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

Task applicabilities changed due to impact of

modifications.

GE requirements updated due to new calculation. Approved by

EASA

under reference

EASA.A.C.07222

on 9 July 2007

16 13 Jun 08 New compliance time requirements introduced in

the Record Of Revisions.

Introduction reworded with :

New Limits Of Validity (LOV)

New information concerning Rules for

Compliance Demonstration (Alternative

inspections, Multiple WV configuration...)

Task requirements updated due to:

Intermediate Service Goal exercise

Fleet survey results

Modifications/In-service experience Approved by

EASA

under reference

EASA.A.C.10414

on 4 Nov 2008

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

Task applicabilities changed due to impact of

modifications. Approved by

EASA

under reference

10031148

on 29 July 2010

# AIRWORTHINESS LIMITATION ITEMS

RECORD OF REVISIONS

ISSUE: 28 MAY 2010 PAGE: 3-ROR

EASA APPROVED

© AIRBUS SAS 2010. All rights reserved. 

# A330

COMPLIANCE TIME:

1. From the 29 th 

# of July 2011, it is mandatory to comply with the airworthiness limitations as

defined in the A330 ALI Document revision 17.

2. From the 29 th 

# of July 2010 to 28 th 

# of July 2011, except for those specific task/applicabilities

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

defined in, either:

- The ALI Document at issue 16

or,

- The ALI Document at issue 17.

3. From the 29 th 

# of July 2010 to 28 th 

# of July 2011, for the following task/applicabilities limitations,

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

- Table 1

Or

- The ALI document at issue 17:

TABLE 1

Task

reference Adapted Threshold

(whichever occurs first, from aircraft first

flight) Applicability

FH FC

545140-01-03/ 58010 7760 MSN 524

545140-02-03 57690 7760 MSN 542

58320 7760 MSN 533

57250 7760 MSN 549

58070 7760 MSN 552

57460 7760 MSN 578

58690 7760 MSN 588

58120 7760 MSN 591

24870 8290 MSN 640

55700 7760 MSN 663

57710 7760 MSN 674

24870 8290 MSN 676

57870 7760 MSN 690

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 1

© AIRBUS SAS 2010. All rights reserved. 

# A330

1 INTRODUCTION

1-1 GENERAL

The data provided has been established with the following rules:

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

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

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

Note: The ALI Document is covered by the Certification Document 00G050A3301/C01.

1-1-A Section 2 - Airworthiness Limitations

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

on structural element that could contribute to catastrophic failure of the aircraft



# .

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

or assemblies which contribute significantly to ca rrying 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 perf ormed with the same inspection level, as

frequently, or more frequently, than the inspection threshold and interval quoted in this

document. Additional information concerning DT ALI requirements can be found in the

following Airbus supporting publications:

− Maintenance Planning Document (MPD),

− Aircraft Maintenance Manual (AMM),

− Non-Destructive Testing Manual (NTM)

− Structural Repair Manual (SRM).

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 2

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-2 RULES FOR COMPLIANCE DEMONSTRATION

1-2-A General

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

whichever occurs first. (Refer to paragraph 3 for definition of the LOV). No aircraft shall be

operated beyond the LOV of the ALI Document, unless the Type Certificate Holder (i.e.

Airbus) has updated this document to reflec t a LOV extension approved by the Type

Certification Authority (EASA).

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

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

flight.

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

embodiment, unless otherwise stated.

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

from manufacturer, unless otherwise stated.

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

performed.

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

associated with the inspection method used at last inspection.

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

be performed at the threshold if the period (years, FC or FH) between initial task

accomplishment and the threshold is greater than the interval.

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

Cycles up to threshold inspection or between two consecutive inspections.

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

inspection or between two consecutive inspections.

1-2-B Conditions for DT ALI inspection

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

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

Where existing Temporary Protection System (TPS) permits unobscured assessment of the

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

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

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

Repair Manual SRM or other documentation acceptable to the relevant Airworthiness

Authority.

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

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© AIRBUS SAS 2010. All rights reserved. 

# A330

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

extent of any damage must be clearly identif ied using appropriate inspection techniques

and/or disassembly when necessary. This may require additional access to that stated for

the DT ALI maintenance requirement.

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

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

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

must be applied.

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

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

1-2-C Reporting

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

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

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

− DT ALI maintenance requirement reference,

− Aircraft Manufacturer Serial Number (MSN) affected,

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

the finding,

− Identification of the affected structure,

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

− Circumstance of detection and inspection method used.

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

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

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

Compliance (AMOC).

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

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

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

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

Operator is responsible for obtaining approval by the relevant Airworthiness Authority for

any necessary adaptations of the limitations.

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 4

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-3 LIMIT OF VALIDITY (LOV)

Aircraft series LOV

Flight Hours Flight Cycles

A330-200 series excl. WV050’s and above or 0 60000 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 0 60000 40000

100000 33000

A330-300 series WV050’s and above 100000 33000

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

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

These aircraft shall be operated within the envelope of:

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

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

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 5

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-4 APPLICABILITY

1-4-A General

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

Aircraft series Aircraft models WV

A330-200 A330-201 020, 023, 024, 050, 052, 055, 056, 059, 060

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

056, 059, 060

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

055,056, 059, 060

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

059, 060

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

050, 052, 055, 056, 059, 060

A330-200F A330-223F 000, 001

A330-243F 000, 001

A330-300 A330-301 000, 001, 002, 003, 004, 010, 051

A330-302 050, 052, 053

A330-303 050, 052

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

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

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

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

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

014, 022, 052

A330-343 020, 022, 024, 050, 052

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 6

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-4-B Weight Variant (WV) applicability

A/C Series Weight Variants WV Group

A330-200 020, 021, 022, 023, 024, 025, 026, 027 Group 32A

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

A330-200F 000, 001

-

A330-300 000, 001, 002, 003, 004 Group 33A

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

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

022 Group 33D

050, 051, 052, 053 Group 33E

Interpretation: Group XYZ

− X: Aircraft Type 3 for A330

− Y: Series (2 for -200, 3 for -300)

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

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

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

These groups are given in addition to the general applicability system in order to improve the

readability of the applicability column.

The ALI section 2 table provides limitations depending on the aircraft weight variants within

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

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

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

Table 1 “Airplane Allocation List” of the Structural Repair Manual (SRM) introduction. This

Table 1 does not necessarily reflect the actual current status of the aircraft that needs to be

confirmed using the weight variant inform ation 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 embodie ment of the referenced Service Bulletins in

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

(MSN).

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

MTOW have to be applied.

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 7

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-4-C Applicability system

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

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

Examples are given below:

Applicability Task applicable to

ALL All A330 aircraft.

A330-xxx -xxx series aircraft.

A330-200 A330-200 Pax aircraft

A330-200F A330-200 Freighter aircraft

PRE nnnnn All A330 PRE MOD nnnnn.

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

POST nnnnn All A330 POST MOD nnnnn.

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

POST nnnnn

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

POST nnnnn

POST mmmmm All A330 POST MOD nnnnn and POST MOD mmmmm.

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

A330-200

OR

A330-300

PRE nnnnn All A330-200,

Or,

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

A330-200

POST nnnnn

OR

POST mmmm All A330-200 that do have MOD nnnnn embodied,

Or,

All A330-200 that do have MOD mmmm embodied.

A330-200

POST nnnnn

OR

A330-300

POST nnnnn

PRE mmmmm All A330-200 that do have MOD nnnnn embodied,

Or,

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

embodied.

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

PW All A330 equipped with PW 4000 engines.

RR All A330 equipped with RR Trent 700 engines.

Door Type 1 Door Type 1 = 1.60 m High, 0. 61 m Wide - Emergency exit type door.

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

GROUP XYZ All aircraft with weight variant group XYZ



# GROUP XYZ

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

embodied

GROUP XYZ

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

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 8

© AIRBUS SAS 2010. All rights reserved. 

# A330

1-5 EXPLANATION OF SECTION 2 TABLE FORMAT

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

REV CODE

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

compared to previous issue of the document.

<Blank> = No amendment.

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

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

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

TASK REFERENCE

This column indicates the task number, e.g. 532114-01-03. It is composed of 10 digits as

follows:

XXXXXX-XX-XX

Applicability index

Sequential number

SSI number

The SSI number is represented by the six first digits, e.g. 532114.

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

Detailed or Special Detailed.

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

aircraft series, mod status, WV group etc ...It is also used to differentiate between access

differences e.g. different access panel numbers.

# AIRWORTHINESS LIMITATION ITEMS

INTRODUCTION

ISSUE: 28 MAY 2010 PAGE: 9

© AIRBUS SAS 2010. All rights reserved. 

# A330

ACCESS

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

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

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

TASK DESCRIPTION

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

description and the boundaries of the DT ALI to be inspected. All structutral items within this

boundary are to be inspected, unless otherwise stated. Additional information may be

added to clarify the inspection area.

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

performed at the same time, are included.

THRESHOLD

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

INTERVAL

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

subsequent times.

APPLICABILITY

This column indicates the applicability of the task.2 AIRWORTHINESS LIMITATIONSTASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY521101-01-01 831 841DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 1 (FORWARD PASSENGER/CREW DOOR).11000 FC 11000 FC ALLR 521103-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 1 (FORWARDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A330-200ORA330-300R 521201-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A330-200ORA330-300521203-01-01 832 842DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 2 (MID PASSENGER/CREW DOOR).11000 FC 11000 FC GROUP 32APOST 42350ORGROUP 32EORAIRWORTHINESS LIMITATION SECTIONA330GROUP 33APOST 42350ORGROUP 33BPOST 42350ORGROUP 33CPOST 42350ORGROUP 33DPOST 42350ORGROUP 33E521203-01-02 832 842DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 2 (MID PASSENGER/CREW DOOR).6000 FC 6000 FC GROUP 33APRE 42350ORGROUP 33BPRE 42350R 521301-01-02 N/AGENERAL VISUALINSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.8500 FC 8500 FC A330-200ORA330-300A330ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 1TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330521303-01-01 833 843DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 4 (AFT PASSENGER/CREW DOOR).11000 FC 11000 FC GROUP 32APOST 42350ORGROUP 32EORGROUP 33APOST 42350ORGROUP 33BPOST 42350ORGROUP 33CPOST 42350ORGROUP 33DPOST 42350ORGROUP 33E521303-01-02 833 843 DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 4 (AFT PASSENGER/CREW DOOR).6000 FC 6000 FC GROUP 33APRE 42350ORGROUP 33BPRE 42350R 522201-01-02 N/A GENERALVISUAL INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) SKIN, EXTERNALSURFACE.8500 FC 8500 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 2TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330522203-01-01 834 844DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).11000 FC 11000 FC GROUP 32APOST 42350ORGROUP 32EORGROUP 33APOST 42350ORGROUP 33BPOST 42350ORGROUP 33CPOST 42350ORGROUP 33DPOST 42350ORGROUP 33E522203-01-02 834 844DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ONDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR).6000 FC 6000 FC GROUP 33APRE 42350ORGROUP 33BPRE 42350N 523104-01-02 132AR 132BR 132CR132DR 132ER 132FR132GR 132HR 132JR132KR 132LRDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR HINGE ASSEMBLIES AT FR 20B TOFR25 (10 PLACES).15800 FC 5600 FCALLR 523106-01-01 821CRDOOR LOCKING HANDLEUNLOCKEDDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT , DOOR FRAME C20B BETWEEN BEAM 3 AND4.10600 FC 2600 FC A330-200PRE 51038PRE 50528ORA330-300PRE 51038PRE 50528N 523204-01-02 152AR 152BR 152CR152DR 152ER 152FR152GR 152HR 152JR152KR 152LRDETAILED INSPECTION OF AFT CARGO COMPARTMENT DOORHINGE ASSEMBLIES AT FR 60 TO FR 64A (10 PLACES)15800 FC 5600 FCALLISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 3TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330524101-01-02 N/ADETAILED INSPECTION OFAVIONICS COMPARTMENT LOWERACCESS DOOR SKIN, EXTERNAL SURFACE.10400 FC 10400 FC ALL524103-01-02 811DOOR FLOOR PANELDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, AVIONICS COMPARTMENT LOWER ACCESSDOOR CROSS MEMBERS.31600 FC 14300 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D528104-01-02 734 744DETAILEDINSPECTION OF MAIN LANDING GEAR, MAIN DOOR,CENTER FITTING AND SURROUNDING AREA (300 MMAROUND), LH/RH.8300 FC 8300 FCALLR 528203-01-02 713 714DETAILED INSPECTION OF NOSE LANDING GEAR, FORWARDDOOR, HINGES (NO 1, NO 2, NO 3) INCLUDING FITTINGS ON9600 FC 9600 FC A330-200OR, (, , )FUSELAGE, LH/RH.A330-300N 528206-01-01 713 714 715 716DETAILED INSPECTION OF NOSE LANDING GEAR DOORS,HINGES (NO 1, NO 2, NO 3, NO4, NO5) INCLUDING FITTINGSON FUSELAGE, LH/RH.12000 FC 12000 FC A330-200F531106-01-03 N/ADETAILED INSPECTION OFFUSELAGE SKIN BETWEEN FR.9AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNERAREA, EXTERNAL SURFACE, LH/RH.21000 FC 10200 FC GROUP 33APRE 41652ORGROUP 33BPRE 41652531106-01-04 N/ADETAILED INSPECTION OFFUSELAGE SKIN BETWEEN FR.9AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNERAREA, EXTERNAL SURFACE, LH/RH.32700 FC 10200 FC GROUP 33APOST 41652ORGROUP 33BPOST 41652ORGROUP 32AORGROUP 33CORGROUP 33DN 531106-01-06 N/ADETAILEDINSPECTION OF FUSELAGE SKIN BETWEEN FR.9AND FR.10A AT COCKPIT LATERAL WINDOW LOWER CORNERAREA, EXTERNAL SURFACE, LH/RH.24000 FC 7900 FC A330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 4TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 531108-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTAT FRAME 18 BETWEEN STRINGER 3 AND STRINGER 7, BUTTJOINT AND REAR PANEL, LH.17400 FC 11900 FC A330-200FN 531109-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIALJOINT AT FRAME 18 BETWEENSTRINGER 11 AND STRINGER13, BUTT JOINT AND REAR PANEL, RH .28700 FC 19700 FC A330-200FR 531110-02-02 N/ADETAILEDINSPECTION OF FUSELAGE SKIN BETWEEN FR 10AND FR 13 FROM FLOOR LEVEL TO STR 9 FWD, EXTERNALSURFACE, LH/RH.18500 FC 18500 FC A330-200ORA330-300N 531110-02-03 N/ADETAILEDINSPECTION OF FUSELAGE SKIN BETWEEN FR 10AND FR 13 FROM FLOOR LEVEL TO STR 9 FWD, EXTERNALSURFACE, LH/RH.10100 FC 10100 FC A330-200FR 531112-02-01 N/ADETAILED INSPECTIONOF FUSELAGE STRUCTURE AROUNDDOOR 1 (FORWARD PASSAGER / CREW DOOR), EXTERNALSURFACE, BETWEEN FR 13 AND FR 18 FROM LATERALLONGITUDINAL LAP JOINT TO STR 9 AFT, LH/RH.9000 FC 9000 FC A330-200ORA330-300,N 531112-02-02 N/ADETAILED INSPECTIONOF FUSELAGE STRUCTURE AROUNDDOOR 1 (FORWARD PASSAGER / CREW DOOR), EXTERNALSURFACE, BETWEEN FR 13 AND FR 18 FROM LATERALLONGITUDINAL LAP JOINT TO STR 9 AFT, LH/RH.8700 FC 8700 FC A330-200FR 531118-01-01 121AL 121EL713 714GENERAL VISUAL INSPECTION OF GROUND SERVICESCONNECTION ACCESS DOORS CUTOUTS AND NOSE LANDINGGEAR CUTOUT, BETWEEN FR 4 AND FR 19 ON LOWERFUSELAGE.3100 FC 3100 FC A330-200ORA330-300R 531120-01-02 713 714GENERAL VISUALINSPECTION OF NLG BAY INTERNALSTRUCTURE, NOSE LANDING GEAR WELL PANELS.1400 FC 1400 FC A330-200ORA330-300531124-01-03 713 714DETAILEDINSPECTION OF NLG BAY SIDE PANEL TOP INNERRADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFTPANEL, LH/RH.23200 FC 10100 FC GROUP 33AORGROUP 33B531124-01-04 713 714DETAILEDINSPECTION OF NLG BAY SIDE PANEL TOP INNERRADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFTPANEL, LH/RH.21200 FC 10100 FC GROUP 32AORGROUP 33C531124-01-05 713 714DETAILEDINSPECTION OF NLG BAY SIDE PANEL TOP INNERRADIUS FROM NLG BAY FORWARD PANEL TO NLG BAY AFTPANEL, LH/RH.20800 FC 10100 FC GROUP 33D531125-01-03 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENTTO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH.38600 FC 5700 FC GROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 5TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531125-01-04 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FRAME 17 ATTACHMENTTO BOTTOM SKIN FROM STRINGER 48 TO 51, LH/RH.20000 FC 7100 FC GROUP 32AORGROUP 33CORGROUP 33DN 531125-02-01 811 821AVIONICS BAY FLOORPANELSDETAILED INSPECTION OF FRAME 17 ATTACHMENT TOBOTTOM SKIN FROM STRINGER 46 TO 51, LH/RH.18200 FC 16700 FC A330-200F531129-02-02 713 714 715716BOLTSNLG ACTUATORSDISCONNECTEDSPECIAL DETAILED INSPECTION OF NOSE LANDING GEARACTUATOR FITTING.28000 FC 4700 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531130-01-02 NOTE 1SPECIAL DETAILEDINSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 16A AT CABIN FLOOR LEVEL, LH/RH.22000 FC 6550 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258531131-01-02 NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 16A, JOINT AREA BETWEEN STRINGERS28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 531131-02-02.18500 FC 9800 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258531131-02-02 NOTE 1SPECIAL DETAILEDINSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 16A, JOINT AREA BETWEEN STRINGERS28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 531131-01-02.18500 FC 9800 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 6TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531132-01-02 NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 14 JOINT BETWEEN STRINGERS 28 AND30 LEVEL, LH/RH.35100 FC 12900 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531133-01-03 NOTE 1AIR DUCTSDETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREBELOW CABIN FLOOR LEVEL, FLOOR BEAM JUNCTION ONFRAME 12A AT STRINGER 26 LEVEL, LH/RH.22600 FC 9800 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531134-01-01 AVIONICS COMPT DOOROPENEDSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, BOOMERANG FRAMES 11A TO 16AATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47,LH/RH.35400 FC 7000 FC GROUP 33AORGROUP 33B531134-01-02 AVIONICS COMPT DOOROPENEDSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, BOOMERANG FRAMES 11A TO 16AATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47,LH/RH.25800 FC 3500 FC GROUP 32AORGROUP 33C531134-01-03 AVIONICS COMPT DOOROPENEDSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, BOOMERANG FRAMES 11A TO 16AATTACHMENT TO SKIN, BETWEEN STRINGERS 46 AND 47,LH/RH.25300 FC 3500 FC GROUP 33D531135-01-02 N/ASPECIAL DETAILED INSPECTION OF REAR LOWER CORNEROF THE COCKPIT LATERAL WINDOW FRAME, FORWARD OFFR.10, EXTERNAL SURFACE, LH/RH.4850 FC 4850 FCALL531136-01-02 CEILING PANELSNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 12 AND 13 DOUBLER AREA AT CROWNCENTRELINE.17500 FC 10100 FC GROUP 33APRE 42481ORGROUP 33BPRE 42481ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 7TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531138-01-02 RADOME OPENEDINSULATION PANELSDETAILED INSPECTION OF FORWARD PRESSURE BULKHEADFORWARD FACE STRINGERS AND SKIN, FROM Y=-50 TO Y=50ABOVE COCKPIT FLOOR LEVEL.34700 FC 9200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531139-01-02 811NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FORWARD PRESSURE BULKHEAD AFT FACEVERTICAL BEAMS AND UPPER SHEET AT Y=-330, Y=0 ANDY=330, ABOVE COCKPIT FLOOR LEVEL.34700 FC 9200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531140-01-01 831LININGNOTE 1GALLEYS AND TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LATERAL FRAME 10 ATFLOOR LEVEL ATTACHMENT, ABOVE COCKPIT FLOOR,INTERNAL STRUCTURE, LH/RH.15700 FC 8400 FC GROUP 33APRE 42829ORGROUP 33BPRE 42829531141-01-02 LININGNOTE 1DETAILED INSPECTION OF LATERAL FRAME 11, SPLICEABOVE COCKPIT FLOOR LEVEL ATTACHMENT, INTERNALSTRUCTURE, LH/RH.17600 FC 9080 FC GROUP 33APRE 41652ORGROUP 33BPRE 41652531142-01-02 CEILINGNOTE 1DETAILED INSPECTION OF FRAME 10 UPPER CURVEDMEMBER BETWEEN CROWN CENTRELINE AND UPPERLATERAL SPLICING, SPLICE EXCLUDED, INTERNALSTRUCTURE, LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK531142-02-02.35000 FC 5250 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 8TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531142-02-02 CEILINGNOTE 1SPECIAL DETAILED INSPECTION OF FRAME 10 UPPERCURVED MEMBER BETWEEN CROWN CENTRELINE ANDUPPER LATERAL SPLICING, SPLICE EXCLUDED, INTERNALSTRUCTURE, LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK531142-01-02.35000 FC 7800 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531143-01-02 NOTE 1AIR DUCTSVACUUM PIPESDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FLOOR BEAM AND CRUCIFORM FITTING ATFR.14, LH/RH.16600 FC 4000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531144-01-02 NOTE 1LININGTOILETSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FRAME 14 ANDCRUCIFORM FITTING, LH/RH.16600 FC 7100 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DN 531145-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTAT FRAME19 BETWEEN STRINGER 45 AND STRINGER 47,BUTT JOINT AND REAR PANEL, RH.24400 FC 23700 FC A330-200F531146-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, LATERAL AND AFT WINDOW FRAMES JUNCTIONWITH FRAME 7 UPPER MEMBER, LH/RH.37100 FC 8750 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 9TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 531148-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF CIRCUMFERENTIAL JOINTAT FRAME18 BETWEEN STRINGER 30 AND STRINGER 32,BUTT JOINT AND REAR PANEL, LH.27700 FC 23700 FC A330-200F531149-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, ANGLE GUSSET ABOVE FRONT WINDSHIELDPANELS, INCLUDING TOP 3 NUTS ON CENTRE POST.35300 FC 8500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531154-01-02 LININGSSLIDING WINDOWSOPENEDNOTE 1DETAILED INSPECTION OF LOWER SURFACE OF UPPERCLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELDSIDE POST, INTERNAL STRUCTURE, LH/RH.14000 FC 8100 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DR 531154-01-03 LININGSSLIDING WINDOWS OPENEDNOTE 1DETAILED INSPECTION OF LOWER SURFACE OF UPPERCLOSING PANEL BETWEEN FR 7 AND FRONT WINDSHIELDSIDE POST, INTERNAL STRUCTURE, LH/RH.31300 FC 8100 FC GROUP 32EORGROUP 33EORA330-200FN 531155-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 14C, FROM STRINGER 9TO STRINGER 12, LH/RH.17500 FC 9100 FC A330-200F531157-01-02 LININGNOTE 1DETAILED INSPECTION OF PASSENGER / CREW DOOR UPPERKEEL FITTINGS AT FRAME 17 AND AT STGR.12 LEVEL,INTERNAL STRUCTURE, LH/RH.31400 FC 10170 FC GROUP 33APRE 41652ORGROUP 33BPRE 41652ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 10TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531158-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN AFT WINDOWFRAME AND FRAMES 8 AND 9 UPPER MEMBERS, LH/RH.35400 FC 15600 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DN 531160-01-01 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RADIUSOF LUGS ON UPPER CORNER OFPORTAL FRAME 15A, LH/RH.9900 FC 6300 FC A330-200F531161-01-02 LININGNOTE 1DETAILED INSPECTION OF PAX / CREW DOOR UPPER KEELFITTING AT FR 18 FORWARD AND AFT FACE AT STGR 12LEVEL, INTERNAL STRUCTURE, LH/RH.14100 FC 10700 FC GROUP 33APRE 41675ORGROUP 33BPRE 41675N 531163-01-01 713 714NLGSPECIAL DETAILED INSPECTION OF NOSE LANDING GEARMAIN ATTACHEMENT BEARING BORE, LH/RH.13800 FC 13800 FC A330-200FN 531164-01-01 713 714SPECIAL DETAILED INSPECTION OF NOSE LANDING GEARBAY LATERAL PANELS, JUNCTION TO LOWER FRAME 17FITTING, LH/RH.7000 FC 7000 FC A330-200FN 531169-02-01 125AL 125BL 125CL126BR 126CR713 714DETAILED INSPECTION OF NOSE FUSELAGE LOWER SKINAND FAIRING SUBSTRUCTURE, AREA COVERED BY NOSEFAIRING BETWEEN FR10 AND FR17 INCLUDING NLG BAYLATERAL PANEL EXTERNAL SURFACE, FLAT PANEL, FR16AAND FORWARD FACE OF LOWER FR17 FITTING, LH/RH.15600 FC 15600 FC A330-200F531175-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREAT JUNCTION BETWEEN FR.17 AND MACHINED STIFFENERSAT STGR.14/18/22/24, LH/RH.22700 FC 8000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DN 531177-01-01 125AL 125BL 125CL126BR 126CR713 714SPECIAL DETAILED INSPECTIONOF LONGITUDINAL JUNCTIONCENTRAL AND LATERAL PANELS AT STRINGER 46, EXTERNALSURFACE BETWEEN FR11 TO FR12A, LH/RH.17400 FC 17400 FC A330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 11TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 531178-01-01 125AL 125BL 125CL126BR 126CR713 714DETAILED INSPECTION OF Y750 AFT FITTING, TOP RADIUS,LH/RH.23100 FC 13000 FC A330-200FN 531179-01-01 125AL 125BL 125CL126BR 126CR713 714SPECIAL DETAILED INSPECTION OF LOWER FRAME 17FITTING AT Y750 FITTING JUNCTION, LH/RH.11900 FC 6700 FC A330-200F531183-01-01 TOILETS, LINING,INSULATION TO BEDISPLACED, FASTENERS TOBE REMOVEDSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWSFORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH.31500 FC 10400 FC A330PRE 40347PRE 55534531183-01-02 TOILETS, LINING,INSULATION TO BEDISPLACED, FASTENERS TOBE REMOVEDSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT, TWO FIRST RIVET ROWSFORWARD OF FR.13, BELOW STGR.9 FWD, LH/RH.28700 FC 9600 FC A330POST 40347PRE 53102PRE 55534N 531184-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, RIVET LINES ATUPPER LONGITUDINAL LAP21100 FC 16900 FC A330-200F,JOINT (STGR.9 AFT LEVEL) FROM FR.13 TO FR.13A AND FROMFR.14 TO FR.16A, LH/RH.531185-01-02 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FORWARD PASSENGER / CREW DOOR CUTOUTAFT UPPER CORNER, JUNCTION OF INTERNAL PLATE ON FR.17, BETWEEN STR.12 AND 13, LH/RH.29400 FC 8850 FC GROUP 32APRE 49194ORGROUP 33AORGROUP 33BORGROUP 33CPRE 49194ORGROUP 33DPRE49194531186-01-02 TOILETS & CRRLININGSNOTE 1TITANIUM RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OFFORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD,LH/RH.31500 FC 10400 FC GROUP 33APRE 40347ANDPRE 49411ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 12TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531186-01-03 TOILETS & CRRLININGSNOTE 1TITANIUM RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERS OFFORWARD UPPER PANEL ABOVE STRINGER 9 FORWARD,LH/RH.28700 FC 9600 FC GROUP 33APOST 40347PRE 49411ORGROUP 32APRE49411ORGROUP 33BPRE 49411ORGROUP 33CPRE 49411ORGROUP 33DPRE 49411531188-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE31500 FC 7600 FC GROUP 33ACIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OFFRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWSAT STGR.9 FWD LEVEL, LH/RH.PRE 40347PRE 53102531188-01-03 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OFFRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5 ROWSAT STGR.9 FWD LEVEL, LH/RH.28700 FC 7000 FC GROUP 33APOST 40347PRE 53102ORGROUP 32APRE 53102ORGROUP 33BPRE 53102ORGROUP 33CPRE 53102ORGROUP 33DPRE 53102ORGROUP 32EPRE 53102ORGROUP 33EPRE 53102ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 13TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330531189-01-02 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT,FORWARD UPPER LONGERON AT STRINGER 12 LEVEL,BETWEEN FR. 13A AND FR.13B, LH/RH.29400 FC 8850 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DR 531192-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FR. 13 FORWARDFACE AND STRINGER 9 FORWARD AND FR. 13 AFT FACE ANDSTRINGER 12, LH/RH.21800 FC 8100 FCALLR 531194-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, MACHINED STIFFENERS 14 AND 22 BETWEENFR. 17 AND FR.18, LH/RH.21800 FC 8100 FCALL,531198-01-02 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREBELOW CABIN FLOOR LEVEL, TORSION BOX INTERNAL PANELBETWEEN FRAMES 13A AND 14, AND 16A AND 17, LH/RH.29400 FC 8850 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DR 532101-01-02 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TOBOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAPJOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRINGLH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532101-02-022200 FC 2200 FC A330-200ORA330-300N 532101-02-02 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TOBOTTOM CENTER LINE, INCLUDING SKIN SPLICES AND LAPJOINTS, EXCLUDING AREAS UNDERNEATH BELLY FAIRINGLH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532101-01-026900 FC 6900 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 14TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532114-01-02 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENT DOORCUTOUT AT UPPER AND LOWER CORNERS.24000 FCOR120000 FH7290 FCOR38300 FHGROUP 32A532114-01-03 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENT DOORCUTOUT AT UPPER AND LOWER CORNERS.24000 FCOR126300 FH8000 FCOR42100 FHGROUP 32E532114-01-04 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENT DOORCUTOUT AT UPPER AND LOWER CORNERS.24000 FCOR84000 FH7220 FCOR29700 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532114-01-05 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AROUND FORWARD CARGO COMPARTMENT DOORCUTOUT AT UPPER AND LOWER CORNERS.24000 FCOR84000 FH8400 FCOR29400 FHGROUP 33ER 532115-01-02 821GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR CUTOUT,VISIBLE PART OF LATERALFRAMES (FR 20A AND FR 25A).3500 FC 3500 FC A330-200ORA330-300R 532117-01-03 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 STR 26,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532117-02-0320000 FC 2200 FC A330-200ORA330-300N 532117-02-03 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 STR 26,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532117-01-0320000 FC 6900 FC A330-200ORA330-300532124-02-04 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FCOR97500 FH8800 FCOR49100 FHGROUP 32A532124-02-05 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.20000 FCOR72700 FH3700 FCOR12700 FHGROUP 33APRE 45293PRE 41856ORGROUP 33BPRE 45293PRE 41856ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 15TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532124-02-06 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.24900 FCOR88900 FH10000 FCOR34200 FHGROUP 33APOST 45293PRE 41856ORGROUP 33BPOST 45293PRE 41856532124-02-07 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FCOR85200 FH5500 FCOR19100 FHGROUP 33APOST 41856ORGROUP 33BPOST 41856532124-02-08 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FCOR88900 FH4400 FCOR15100 FHGROUP 33CORGROUP 33D532124-02-09 832 842SPECIAL DETAILED INSPECTION OF DOOR 2 (MID26000 FC 4500 FC GROUP 33ESCUFF PLATE(PASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.OR88900 FHOR15300 FH532124-02-10 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FCOR143600 FH7300 FCOR40300 FHGROUP 32E532125-01-04 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.26000 FCOR97500 FH8800 FCOR49100 FHGROUP 32A532125-01-05 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.20000 FCOR72700 FH3700 FCOR12700 FHGROUP 33APRE 45293PRE 41856ORGROUP 33BPRE 45293PRE 41856532125-01-06 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.24900 FCOR88900 FH10000 FCOR34200 FHGROUP 33APOST 45293PRE 41856ORGROUP 33BPOST 45293PRE 41856ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 16TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532125-01-07 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.26000 FCOR85200 FH5500 FCOR19100 FHGROUP 33APOST 41856ORGROUP 33BPOST 41856532125-01-08 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.26000 FCOR88900 FH4400 FCOR15100 FHGROUP 33CORGROUP 33D532125-01-09 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.26000 FCOR88900 FH4500 FCOR15300 FHGROUP 33E532125-01-10 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.26000 FCOR143600 FH7300 FCOR40300 FHGROUP 32E532126-01-01 832 842DOOR FRAME LININGDETAILED INSPECTION OF DOOR 2, COVER PLATE OFTORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR 12 AND19400 FCOR11700 FCORGROUP 33APRE 45223INSULATION,STR 13, LH/RH.85600 FH 52000 FH ORGROUP 33BPRE 45223532127-01-01 832 842DOOR FRAME LININGNOTE 1DETAILED INSPECTION OF DOOR NO 2, FR 33, BETWEEN STR13 AND STR 15, LH/RH.15000 FCOR60000 FH10000 FCOR40000 FHGROUP 33APRE 44147ORGROUP 33BPRE 44147R 532128-01-01 832 842GENERAL VISUALINSPECTION OF DOOR NO 2 (MIDPASSENGER/CREW DOOR) STOP FITTINS ON FR33 AND FR35A, LH/RH.14000 FC 14000 FC A330-200ORA330-300532129-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.22800 FC 15200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532129-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 37.1 FROM STR 13 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.22800 FC 14000 FC GROUP 32EORGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 17TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532130-01-02 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AND VISIBLE PORTION OF WINDOW FORGINGS,BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROMSTR 18 TO STR 22, LH/RH.25000 FC 10000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532130-01-03 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AND VISIBLE PORTION OF WINDOW FORGINGS,BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROMSTR 18 TO STR 22, LH/RH.25000 FCOR97200 FH8000 FCOR31100 FHGROUP 33E532130-01-04 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AND VISIBLE PORTION OF WINDOW FORGINGS,BETWEEN FR18 AND FR 31, BETWEEN FR 36 AND FR 38 FROM25000 FCOR152700 FH7200 FCOR44000 FHGROUP 32E,STR 18 TO STR 22, LH/RH.R 532138-01-01 131AG 821DRAINMASTDETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37 AND FR37.1, FROM STR 53 TO STR 54, LH ONLY.20000 FC 8000 FC A330-200ORA330-300532139-01-01 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AT CLOSED DRAIN MAST CUT-OUT BETWEEN FR 28AND FR 29, FROM STR 46 TO STR 47, RH.20000 FC 8000 FC GROUP 33APOST 41367ORGROUP 33BPOST 41367R 532143-01-02 ANTENNADETAILED INSPECTION OF SKIN AROUND GPS ANTENNASCUT-OUTS BETWEEN FR 35 AND FR 36 AND FR 37 AND FR37.1, ON CROWN CENTER LINE, EXTERNAL SURFACE.24000 FC 8600 FC A330-200ORA330-300R 532144-01-02 832 842CEILING PANELSNOTE 1DETAILED INSPECTION OF FRAMES AND STRINGERCOUPLING AREA, BETWEEN FR 32 AND FR 34, FROM STR 9 TOSTR 13 LH/RH, INTERNAL STRUCTURE.20000 FC 10000 FC A330-200ORA330-300R 532146-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 26 FROM STR 13 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.24000 FC 16000 FC A330-200ORA330-300R 532147-01-02 821CARGO COMPARTMENTFLOOR PANELSLININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OFCARGO FLOOR ATTACHMENTS FITTINGS FROM FR 20 TO FR38 LH, FROM FR 26 TO FR 38 RH, BETWEEN STR 34 AND STR43.20000 FC 10000 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 18TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 532148-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREAAT FR 31 FROM STR 9 TO STR 15 LH/RH, EXTERNAL SURFACE.24000 FC 16000 FC A330-200ORA330-300R 532149-01-02 832 842CEILING AND SIDE WALLPANELSOVERHEAD STOWAGE BINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE AT FR 26, FROM STR 4 TO STR 6STR 12 TO STR 14 AND STR 21 TO STR 22, LH/RH.24000 FC 16000 FC A330-200ORA330-300532150-01-02 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTR 9, BETWEEN FR 31 ANDFR 37.1.30000 FC 4500 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532150-01-03 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTR 9, BETWEEN FR 31 ANDFR 37.1.20000 FC 4500 FC GROUP 33APRE 46636ORGROUP 33BPRE 46636ORGROUP 33CPRE 46636ORGROUP 33DPRE 46636532150-01-04 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTR 9, BETWEEN FR 31 ANDFR 37.1.30000 FC 8000 FC GROUP 32EORGROUP 33E532151-01-01 N/ASPECIAL DETAILED INSPECTION OF EXTERNAL SKIN OFLONGITUDINAL LAP JOINT AT STR 22, BETWEEN FR 37.1 ANDFR 38.25000 FC 3000 FC GROUP 33APRE 45226ORGROUP 33BPRE 45226ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 19TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532153-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOWVALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32 ANDFR 33, FROM STR 45 TO STR 49, LH ONLY.15000 FC 8000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532153-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE OUTFLOWVALVE DOUBLER EXTERNAL SURFACE, BETWEEN FR 32 ANDFR 33, FROM STR 45 TO STR 49, LH ONLY.17000 FCOR106000 FH8000 FCOR50000 FHGROUP 32EORGROUP 33E532154-01-02 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE AT SPOT LIGHT CUT-OUT, BETWEEN- FR 27 AND FR 28 AND BETWEEN- FR 30 AND FR 31,20000 FC 6000 FC GROUP 32AORGROUP 33AOR,- FROM STR 24 TO STR 26, LH/RHGROUP 33BORGROUP 33CORGROUP 33D532155-01-02 N/ADETAILED INSPECTION OFFUSELAGE SKIN AND DOUBLER ATPRESSURE RELIEF VALVE CUTOUT, BETWEEN FR 24 AND FR25, FROM STR 26 TO STR 30, LH ONLY.20000 FC 6500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532156-01-02 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH.30000 FC 4500 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 20TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532156-01-03 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH.20000 FC 4500 FC GROUP 33APRE 46636ORGROUP 33BPRE 46636ORGROUP 33CPRE 46636ORGROUP 33DPRE 46636532156-01-04 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH.30000 FC 8000 FC GROUP 32EORGROUP 33E532157-01-02 832 842SIDEWALL LININGSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TO STR 15,32000 FC 8000 FC A330-200ORINSULATION, ,LH/RH.GROUP 33CPOST 46636ORGROUP 33DPOST 46636ORGROUP 33E532158-01-02 833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH.30000 FC 4500 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532158-01-03 833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13 TOCROWN CENTER LINE, LH/RH.30000 FC 8000 FC GROUP 32EORGROUP 33E532164-01-01 821CEILING PANELSSPECIAL DETAILED INSPECTION OF FWD FUSELAGE, CARGODOOR ACTUATOR SUPPORT BEAM BETWEEN FR 22 AND FR23.20000 FC 6000 FC GROUP 33APOST 44072PRE 45489ORGROUP 33BPOST 44072PRE 45489ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 21TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330532165-01-02 831 841CEILING PANELSLININGINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTR 9, BETWEEN FR 31 ANDFR 37.1.30000 FC 4500 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532165-01-03 831 841CEILING PANELSLININGINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTR 9, BETWEEN FR 31 ANDFR 37.1.30000 FC 8000 FC GROUP 32EORGROUP 33EN 532166-01-03 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TOCROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532166-02-034500 FC 4500 FC A330-200ORA330-300N 532166-02-03 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TOCROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK532117-01-036900 FC 6900 FC A330-200ORA330-300N 532182-01-01 835LININGNOTE1SPECIAL DETAILED INSPECTION OF FRAME AND FRAMECOUPLING FROM FR 20 TO FR 26/28 AT STR 21 RH16000 FC 3600 FC A330-200FN 532183-01-01 835LININGNOTE1SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ANDCIRCUMFERENTIAL SPLICE AT FR 31 BETWEEN STR 5 ANDCROWN CENTER LINE, LH/RH.12100 FC 7200 FC A330-200F533005-01-02 191AB 191AT 191BB191CB 192AT 192BB192CB 197AT 197FB197GB 197HB 198AT198GB 198HBDETAILED INSPECTION OF FUSELAGE SKIN AT BELLY FAIRINGSEALING LIP ATTACHMENT FROM FRAME 37.1 TO 38 ANDFROM FRAME 53.6 TO 56.16400 FC 4800 FCALLISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 22TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533009-01-01 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-02-0130900 FCOR92800 FH13900 FCOR41700 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911533009-01-02 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-02-0229300 FCOR146900 FH10800 FCOR54200 FHGROUP 32APRE 49202PRE 52911ORPOST 50755PRE 56001533009-01-03 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-02-0331700 FCOR95100 FH11400 FCOR34300 FHGROUP 33DPRE 49202PRE 52911533009-01-04 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-02-0432500 FCOR97400 FH11600 FCOR34900 FHGROUP 33CPRE 49202PRE 52911533009-02-01 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-01-0130900 FCOR92800 FH4600 FCOR13900 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 23TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533009-02-02 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-01-0229300 FCOR146900 FH3600 FCOR18100 FHGROUP 32APRE 49202PRE 52911ORPOST 50755PRE 56001533009-02-03 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-01-0331700 FCOR95100 FH3800 FCOR11400 FHGROUP 33DPRE 49202PRE 52911533009-02-04 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45, BETWEENSTRINGER 3 AND 5, AND BETWEEN STRINGER 11 AND 13,LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533009-01-0432500 FCOR97400 FH3800 FCOR11600 FHGROUP 33CPRE 49202PRE 52911533010-01-01 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.30900 FCOR92800 FH3900 FCOR11700 FHGROUP 33AORGROUP 33B533010-01-02 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.29500 FCOR147600 FH3050 FCOR15300 FHGROUP 32APRE 49202ORPOST 50755533010-01-03 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.31700 FCOR95100 FH3200 FCOR9700 FHGROUP 33DPRE 49202533010-01-04 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.32500 FCOR97400 FH3250 FCOR9800 FHGROUP 33CPRE 49202ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 24TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 533012-01-01 261CC 262CCOVERHEAD STOWAGEBINSNOTE 1RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4TO 5, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533012-02-0126500 FCOR79700 FH8100 FCOR24400 FHGROUP 33APRE 41652PRE 52911ORGROUP 33BPRE 41652PRE 52911R 533012-02-01 261CC 262CCOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROM STRINGER 4TO 5, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 533012-01-0126500 FCOR79700 FH2300 FCOR6900 FHGROUP 33APRE 41652PRE 52911ORGROUP 33BPRE 41652PRE 52911533013-01-02 FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED PRESSURE PANEL STIFFENER22600 FCOR14700 FCORGROUP 32A,JUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 ANDY=2361, LH/RH.113300 FH 73900 FH533013-01-03 FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED PRESSURE PANEL STIFFENERJUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 ANDY=2361, LH/RH.23800 FCOR71400 FH15500 FCOR46500 FHGROUP 33D533013-01-04 FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED PRESSURE PANEL STIFFENERJUNCTION AT FRAME 48 CLEAT AT Y=2093, Y=2227 ANDY=2361, LH/RH.24000 FCOR72200 FH15600 FCOR46900 FHGROUP 33C533014-01-01 734744SPECIAL DETAILED INSPECTION OF MAIN LANDING GEARBAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFTOF FRAME 47 DATUM, LH/RH.26500 FCOR79700 FH6900 FCOR20900 FHGROUP 33APRE 45307ORGROUP 33BPRE 45307533014-01-02 734744SPECIAL DETAILED INSPECTION OF MAIN LANDING GEARBAY, LOWER FLANGE OF GANTRY Y=1456, 20 FASTENERS AFTOF FRAME 47 DATUM, LH/RH.28900 FCOR144600 FH7300 FCOR36800 FHGROUP 32APRE 45307533016-01-01 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.34900 FCOR104700 FH4400 FCOR13200 FHGROUP 33CISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 25TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533016-01-02 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.34100 FCOR102200 FH4300 FCOR13000 FHGROUP 33D533018-01-01 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.27500 FCOR137600 FH4300 FCOR21800 FHGROUP 32APRE 49202533018-01-02 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.29700 FCOR89100 FH4600 FCOR13800 FHGROUP 33DPRE 49202533018-01-03 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.30400 FCOR91300 FH4600 FCOR14000 FHGROUP 33CPRE 49202,533103-02-01 N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, SKIN PANEL RIVETING ON FR.40 FROMSTRINGER 17 TO 19, LH/RH.15100 FC 7330 FC GROUP 33APRE 41652PRE 45749ORGROUP 33BPRE 41652PRE 45749533104-01-03 ANTICOLLISION LIGHT:LENS 7LVADF: LENSES 2RP1 & SEALAND 2RP2 & SEALDETAILED 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.48AND FR.49 AND BETWEEN FR.52 & FR.53, BETWEENSTRINGER 1 LH AND STRINGER 1 RH.32200 FCOR96600 FH5000 FCOR15000 FHGROUP 33AORGROUP 33B533105-01-02 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER HOLE AREA ABOVE STRINGER 28 ATFRAME 39.1 WEB JUNCTION ON HOIST FITTING, LH/RH.10700 FCOR32100 FH7400 FCOR22300 FHGROUP 33APRE 40391533106-01-02 N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18 ANDSTRG. 22, FROM FRAME 38 TO 53.3, LH/RH.26900 FCOR80700 FH6800 FCOR20600 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 26TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533107-01-03 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.15300 FCOR46100 FH10500 FCOR31600 FHGROUP 33AORGROUP 33B533107-01-04 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.12100 FCOR60900 FH9000FCOR45200 FHGROUP 32A533107-01-05 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.14700 FCOR44200 FH10200 FCOR30800 FHGROUP 33D533107-01-06 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.27400 FCOR82300 FH11000 FCOR33000 FHGROUP 33E,533107-01-07 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.21900 FCOR110000 FH9900 FCOR49800 FHGROUP 32E533107-01-08 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 39 TO 39.2 WEB HOLE AREA JUSTBELOW STRINGER 28 AND FASTENERS AREA AT FRAMESJUNCTION BELOW STRINGER 29 LEVEL, LH/RH.15100 FCOR45400 FH10400 FCOR31400 FHGROUP 33C533109-01-01 N/ASPECIAL DETAILEDINSPECTION OF FUSELAGELONGITUDINAL LAP JOINT AT STRINGER 5 FROM FRAME 38TO 53.3, AT STRINGER 13 FROM FRAME 38 TO 47 AND ATSTRINGER 22 FROM FRAME 43 TO 53.3, EXCLUDING 3 RIVETROWS FORWARD AND AFT FRAME 45 LEVEL, LH/RH.33800 FC 10200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533113-01-04 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.12600 FCOR37800 FH7500 FCOR22500 FHGROUP 33AORGROUP 33B533113-01-05 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.11500 FCOR34600 FH7100 FCOR21200 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 27TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533113-01-06 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.9200 FCOR46100 FH6400 FCOR32000 FHGROUP 32E533113-01-07 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.11600 FCOR34900 FH6900 FCOR20900 FHGROUP 33D533113-01-08 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.10700 FCOR53800 FH6600 FCOR33000 FHGROUP 32A533113-01-09 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.11900 FCOR35700 FH7000 FCOR21200 FHGROUP 33CN 533113-01-10 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS ROWS AT FRAME 47, FROM BELOWSTRINGER 22 TO ABOVE STRINGER 24 LEVEL, LH/RH.11900 FC 7770 FC A330-200F533114-01-03 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47 WEB AT JUNCTION WITHSTABILIZERS STRINGER 20 TO 23, LH/RH.22500 FCOR67500 FH23800 FCOR71700 FHGROUP 33AORGROUP 33B533114-01-04 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47 WEB AT JUNCTION WITHSTABILIZERS STRINGER 20 TO 23, LH/RH.19900 FCOR59900 FH21700 FCOR65100 FHGROUP 33CORGROUP 33D533114-01-06 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47 WEB AT JUNCTION WITHSTABILIZERS STRINGER 20 TO 23, LH/RH.16000 FCOR80400 FH18700 FCOR93600 FHGROUP 32A533115-01-04 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO23, LH/RH.13400 FCOR40200 FH8200 FCOR24800 FHGROUP 33AORGROUP 33B533115-01-05 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO23, LH/RH.13100 FCOR39400 FH7900 FCOR23900 FHGROUP 33CORGROUP 33D533115-01-06 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO23, LH/RH.12300 FCOR37000 FH8200 FCOR24600 FHGROUP 33E533115-01-07 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO9800 FCOR7400 FCORGROUP 32E23, LH/RH.49300 FH 37100 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 28TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533115-01-08 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO23, LH/RH.10500 FCOR52900 FH6800 FCOR34300 FHGROUP 32AN 533115-01-09 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROM STRINGER 19 TO23, LH/RH.13000 FC 8500 FC A330-200F533124-01-02 734 744DETAILED INSPECTION OF BELLY FAIRING STRUCTURE ATCLG DOOR CUTOUT, "Z" STIFFENER AT HINGE 3 LOCATION,LH/RH.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.30800 FC 21300 FC GROUP 33APOST 42605S11998ORGROUP 33BPOST 42605S11998ORGROUP 32AORGROUP 33CORGROUP 33DR 533125-01-01 734 744GENERAL VISUAL INSPECTION OF FORWARD FACE OF FR53.2 PRESSURE BULKHEAD INCLUDING THE ATTACHMENTAREA OF THE CLG TRUNNION FITTINGS.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.1500 FC 1500 FC A330-200ORA330-300533126-01-03 734 744GENERAL VISUALINSPECTION OF AREA AROUND CLG ANDMLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNALSURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.4100 FCOR20500 FH4100 FCOR20500 FHGROUP 32AISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 29TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533126-01-05 734 744GENERAL VISUALINSPECTION OF AREA AROUND CLG ANDMLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNALSURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.4200 FCOR12700 FH4200 FCOR12700 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533126-01-06 734 744GENERAL VISUALINSPECTION OF AREA AROUND CLG ANDMLG CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN) EXTERNALSURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOT FITTEDTO THE A330. HOWEVER, THE TERM CLG HAS BEEN KEPT INTHE DESCRIPTION DUE TO FUSELAGE STRUCTURALCOMMONALITY WITH THE A340 IN THIS AREA.3300 FC 3300 FC GROUP 32EORGROUP 33E533127-03-01 FAIRING PANELS BETWEENFR.39.1 AND FR.47DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONINGACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.4200 FCOR12700 FH4200 FCOR12700 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533127-03-02 FAIRING PANELS BETWEENFR.39.1 AND FR.47DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONINGACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE4100 FCOR20500 FH4100 FCOR20500 FHGROUP 32A533127-03-03 FAIRING PANELS BETWEENFR.39.1 AND FR.47DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONINGACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.3300 FC 3300 FC GROUP 32EORGROUP 33EN 533127-03-04 FAIRING PANELS BETWEENFR.39.1 AND FR.47DETAILED INSPECTION OF AREA AROUND AIR-CONDITIONINGACCESS CUTOUT TO AN EXTENT OF 15.0 CM (6.0 IN)EXTERNAL SURFACE.19300 FC 19300 FC A330-200F533137-01-01 251FG 251MG 252FG252MGDETAILED INSPECTION OF HORIZONTAL PRESSURE PANELAND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52FROM FUSELAGE SKIN PANEL TO FIRST HORIZONTALSTIFFENER AT Y=2565, LH/RH.35700 FC 16600 FC GROUP 33AORGROUP 33B533137-01-02 251FG 251MG 252FG252MGDETAILED INSPECTION OF HORIZONTAL PRESSURE PANELAND ATTACHED STIFFENERS BETWEEN FR.51 AND FR.52FROM FUSELAGE SKIN PANEL TO FIRST HORIZONTALSTIFFENER AT Y=2565, LH/RH.38000 FC 20000 FC GROUP 32AORGROUP 33CORGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 30TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533138-01-02 FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FLOOR BEAM INBOARD FLANGE AT Y=1959, ATFR48 LEVEL LH/RH.21500 FCOR64600 FH19800 FCOR59500 FHGROUP 33APOSTMSB 53-3013533145-01-03 197AT 197HB 198AT198HBSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STRINGER 31 LEVEL FROMFRAME 53.3 TO FRAME 54, LH/RH.29400 FC 7050 FC GROUP 33AORGROUP 33B533145-01-04 197AT 197HB 198AT198HBSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STRINGER 31 LEVEL FROMFRAME 53.3 TO FRAME 54, LH/RH.24700 FC 6100 FC GROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533154-01-04 CABIN FLOOR PANELSGALLEYSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS AND12100 FC 8050 FC GROUP 33APRE 41652TOILETS,LONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1,LH/RH.ORGROUP 33BPRE 41652533154-01-05 CABIN FLOOR PANELSGALLEYSTOILETSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1,LH/RH.20000 FC 13300 FC GROUP 33APOST 41652ORGROUP 33BPOST 41652ORGROUP 32AORGROUP 33CORGROUP 33D533154-01-06 CABIN FLOOR PANELSGALLEYSTOILETSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO 53.1,LH/RH.28600 FC 17000 FC GROUP 32EORGROUP 33E533155-01-01 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUTAT STRINGER 28 LEVEL,LH/RH.35500 FCOR178100 FH12600 FCOR63100 FHGROUP 32A533155-01-02 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUTAT STRINGER 28 LEVEL,LH/RH26200 FCOR78600 FH9700 FCOR29100 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 31TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533155-01-03 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUTAT STRINGER 28 LEVEL,LH/RH36800 FCOR110500 FH13000 FCOR39100 FHGROUP 33CORGROUP 33D533156-01-01 822LININGNOTE 1LD-MCR IF INSTALLEDPOST 46678: LDL TOILETSAND FURNISHINGSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEENSTRINGERS 32 AND 33 AT FRAMES 53.3 TO 54, LH/RH.33500 FCOR100600 FH6100 FCOR18300 FHGROUP 33AORGROUP 33B533162-01-02 734744SPECIAL DETAILED INSPECTION OF MAIN LANDING GEARBAY, LOWER FLANGE OF GANTRY Y=1456, 40 FASTENERSFORWARD AND AFT FR. 48 DATUM, LH/RH.14700 FCOR44300 FH9300 FCOR27900 FHGROUP 33APRE 43852ORGROUP 33BPRE 43852533164-01-03 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OF30900 FCOR13700 FCORGROUP 32A,CANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES47 AND 48 FROM Y=450 TO Y=1959, LH/RH.154900 FH 68500 FH533164-01-04 734 744 DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OFCANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES47 AND 48 FROM Y=450 TO Y=1959, LH/RH.28800 FCOR144000 FH12500 FCOR62700 FHGROUP 32E533164-01-06 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OFCANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES47 AND 48 FROM Y=450 TO Y=1959, LH/RH.28500 FCOR85700 FH12200 FCOR36800 FHGROUP 33AORGROUP 33B533164-01-07 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OFCANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES47 AND 48 FROM Y=450 TO Y=1959, LH/RH.34000 FCOR102100 FH14800 FCOR44400 FHGROUP 33CORGROUP 33DN 533164-01-08 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTION AREA OFCANTED DIAPHRAGMS ON FLOOR BEAMS BETWEEN FRAMES47 AND 48 FROM Y=450 TO Y=1959, LH/RH.29200 FC 14400 FC A330-200F533165-01-02 251MG 251SG 252MG252SGNOTE 1GALLEYS & TOILETS IFINSTALLEDDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 48 TO 53.1 HORIZONTAL LEG ATSTRINGER PASSAGE, LH/RH.13400 FCOR40300 FH8350 FCOR25100 FHGROUP 33APOST 43904ORGROUP 33BPOST 43904ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 32TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533179-01-02 251MG 251SG 252MG252SGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 48 TO 53.1 VERTICAL LEG ATSTRINGER PASSAGE, LH/RH.23900 FCOR71700 FH11800 FCOR35400 FHGROUP 33APOST 43904ORGROUP 33BPOST 43904533180-01-03 N/ADETAILED INSPECTION OFSKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)24000 FCOR90000 FH8200 FCOR32600 FHGROUP 32A533180-01-04 N/ADETAILED INSPECTION OFSKIN IN CIRCUMFERENTIAL SPLICEAND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)20000 FCOR75000 FH4800 FCOR17900 FHGROUP 33AORGROUP 33B533180-01-05 N/ADETAILED INSPECTIONOF SKIN IN CIRCUMFERENTIAL SPLICE 24000 FC 6200 FC GROUP 33CAND STRINGER COUPLING AREAS BETWEEN FR 53,6 AND FR53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)OR90000 FHOR23400 FHORGROUP 33D533181-01-03 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 ,LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)24000 FCOR90000 FH11400 FCOR45000 FHGROUP 32A533181-01-04 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 ,LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)20000 FCOR75000 FH8300 FCOR30600 FHGROUP 33AORGROUP 33B533181-01-05 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 ,LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)24000 FCOR90000 FH9300 FCOR35200 FHGROUP 33CORGROUP 33D533181-01-06 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 ,LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)24000 FCOR84000 FH9300 FCOR34200 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 33TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533181-01-07 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE AT THECIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 AND FR 53.7 ,LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)17000 FCOR68000 FH8500 FCOR34000 FHGROUP 32EN 533187-01-01 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGE MEMBRANESAROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49,AT Y-1456 AND Y+1456.23100 FCOR115800 FH8600 FCOR43000 FHGROUP 32AN 533187-01-02 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGE MEMBRANESAROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49,AT Y-1456 AND Y+1456.23400 FCOR70200 FH8350 FCOR25000 FHGROUP 33AORGROUP 33BN 533187-01-03 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGE MEMBRANESAROUND 6 FASTENERS BETWEEN FRAME 48 AND FRAME 49,AT Y-1456 AND Y+1456.22400 FCOR67400 FH8000 FCOR24000 FHGROUP 33CORGROUP 33DR 533192-01-01 834 844GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS OFDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) AT FR 53.514000 FC 14000 FC A330-200OR( )AND 53.7 A, LH/RH.A330-300R 533193-01-01 N/AGENERAL VISUALINSPECTION OF FUSELAGE SKIN(INCLUDING DOOR 3 CUT-OUT) BETWEEN FR 53.3 AND FR 54FROM UPPER EDGE OF BELLY FAIRING TO CROWN CENTERLINE LH/RH, EXTERNAL SURFACE.3600 FC 3600 FC A330-200ORA330-300533194-01-04 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.24000 FCOR84000 FH11600 FCOR40600 FHGROUP 33E533194-01-05 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.12000 FCOR45000 FH6200 FCOR23250 FHGROUP 33ADOOR TYPE 1ORGROUP 33BDOOR TYPE 1533194-01-06 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.20000 FCOR75000 FH15000 FCOR56250 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 34TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533194-01-07 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.20000 FCOR75000 FH7700 FCOR27200 FHGROUP 33ADOOR TYPE APOST 42352ORGROUP 33BDOOR TYPE APOST 42352533194-01-08 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.26000 FCOR90000 FH7500 FCOR26200 FHGROUP 33ADOOR TYPE APOST 41848ORGROUP 33BDOOR TYPE APOST 41848533194-01-09 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT24000 FCOR10700 FCORGROUP 32A( )UPPER CORNERS.90000 FH 65200 FH533194-01-11 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.17000 FCOR102800 FH6600 FCOR39900 FHGROUP 32E533194-01-12 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKIN ATDOOR 3 (EMERGENCY/PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.24000 FCOR90000 FH11600 FCOR41100 FHGROUP 33CORGROUP 33D533195-02-04 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.24000 FCOR84000 FH11600 FCOR40600 FHGROUP 33E533195-02-05 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.12000 FCOR45000 FH6200 FCOR23250 FHGROUP 33ADOOR TYPE 1ORGROUP 33BDOOR TYPE 1533195-02-06 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.20000 FCOR75000 FH15000 FCOR56250 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 35TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330533195-02-07 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.20000 FCOR75000 FH7700 FCOR27200 FHGROUP 33ADOOR TYPE APOST 42352ORGROUP 33BDOOR TYPE APOST 42352533195-02-08 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.24000 FCOR90000 FH7500 FCOR26200 FHGROUP 33ADOOR TYPE APOST 41848ORGROUP 33BDOOR TYPE APOST 41848533195-02-09 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,24000 FCOR10700 FCORGROUP 32A( ),STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.90000 FH 65200 FH533195-02-11 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.17000 FCOR102800 FH6600 FCOR39900 FHGROUP 32E533195-02-12 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.24000 FCOR90000 FH11600 FCOR41100 FHGROUP 33CORGROUP 33DN 533196-01-01 734 744SPECIAL DETAILED INSPECTION OF MAIN LANDING GEARBAY, CATENARIES SKINS AT JUNCTION WITH GANTRIESY1456, OUTSIDE BOARD, AND Y1959, INSIDE BOARD,BETWEEN FR48 AND FR49 LH/RH.15300 FC 5200 FC A330-200F534102-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 58 FROM STRINGERS 13 TO CROWN CENTER LINE,EXTERNAL SURFACE, LH/RH.22800 FCOR90000 FH12350 FCOR48750 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534102-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 58 FROM STRINGERS 13 TO CROWN CENTER LINE,EXTERNAL SURFACE, LH/RH.22800 FCOR90000 FH9350 FCOR51600 FHGROUP 32AISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 36TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534102-01-05 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 58 FROM STRINGERS 13 TO CROWN CENTER LINE,EXTERNAL SURFACE, LH/RH.22800 FCOR126000 FH7100 FCOR39200 FHGROUP 32E534104-01-04 833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22,LH/RH.14250 FCOR56250 FH9500 FCOR37500 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534104-01-05 833 843CEILING PANELSOVERHEAD STOWAGESPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22,22800 FCOR90000 FH12350 FCOR48750 FHGROUP 33EBINS, INSULATION, ,LH/RH.534104-01-06 833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROM STRINGERS4 TO 6, STRINGERS 12 TO 14 AND STRINGERS 21 TO 22,LH/RH.22800 FCOR126000 FH9000 FCOR49700 FHGROUP 32E534105-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.24000 FCOR102000 FH12900 FCOR54400 FHGROUP 33APRE 40556ORGROUP 33BPRE 40556534105-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.24000 FCOR102000 FH16000 FCOR68000 FHGROUP 32AORGROUP 33APOST 40556ORGROUP 33BPOST 40556ORGROUP 33CPOST 40556ORGROUP 33DPOST 40556ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 37TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534105-01-05 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.24000 FCOR100000 FH16000 FCOR67300 FHGROUP 33E534105-01-06 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLING AREASAT FR 72 FROM STRINGERS 13 LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE.24000 FCOR138000 FH16000 FCOR92600 FHGROUP 32E534107-01-02 833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13,AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.15000 FCOR63750 FH10000 FCOR42500 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534107-01-03 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13,AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.24000 FCOR100000 FH16000 FCOR67300 FHGROUP 33E534107-01-04 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3 TOSTR 7, AND STR 11 TO STR 13,AT INTERSECTION OF LAPJOINTS AND CIRCUMFERENTIAL SKIN SPLICE, LH/RH.24000 FCOR138000 FH12000 FCOR69400 FHGROUP 32E534120-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGINGS BETWEEN FR 53.8 AND FR 73AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNALSURFACE.22800 FC 13490 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534120-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGINGS BETWEEN FR 53.8 AND FR 73AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNALSURFACE.22800 FCOR84000 FH13490 FCOR49700 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 38TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534120-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN AND VISIBLEPART OF WINDOW FORGINGS BETWEEN FR 53.8 AND FR 73AND BETWEEN STRINGERS 18 AND 22 LH/RH, EXTERNALSURFACE.17000 FCOR89400 FH9800 FCOR51500 FHGROUP 32ER 534124-01-02 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN BETWEENFR 54 AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDINGAREA UNDER VERTICAL STABILIZER FAIRING EXTERNALSURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK534124-02-0220000 FC 2200 FC A330-200ORA330-300N 534124-02-02 N/ADETAILEDINSPECTION OF FUSELAGE SKIN BETWEEN FR 54AND FR 80 FROM STR 6 TO STR 26, LH/RH, EXCLUDING AREAUNDER VERTICAL STABILIZER FAIRING EXTERNAL SURFACE.20000 FC 6900 FC A330-200ORA330-300NOTE: THIS TASK IS AN ALTERNATIVE TO TASK534124-01-02R 534126-01-02 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 TOBOTTOM CENTER LINE, LH/RH,INCLUDING SKIN SPLICES ANDLAP JOINTS AND INCLUDINGTHE LOWER, UNCOVERED AREAOF SKIN AFT OF THE BELLY FAIRING AND FWD OF FR 54NOTE: THIS TASK IS ANALTERNATIVE TOTASK534126-02-022200 FC 2200 FC A330-200ORA330-300N 534126-02-02 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 TOBOTTOM CENTER LINE, LH/RH,INCLUDING SKIN SPLICES ANDLAP JOINTS AND INCLUDINGTHE LOWER, UNCOVERED AREAOF SKIN AFT OF THE BELLY FAIRING AND FWD OF FR 54NOTE: THIS TASK IS ANALTERNATIVE TOTASK534126-01-026900 FC 6900 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 39TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534131-01-02 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.22800 FC 10500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534131-01-03 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.22800 FCOR102000 FH10500 FCOR46900 FHGROUP 33E534131-01-04 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPER CORNERS.22800 FCOR150000 FH10500 FCOR69000 FHGROUP 32E534132-02-01 833 843SPECIAL DETAILED INSPECTION OF DOOR 4 (AFT22800 FC 10500 FC GROUP 32ASCUFF PLATE(PASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE LH/RH.ORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534132-02-02 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE LH/RH.22800 FCOR102000 FH10500 FCOR46900 FHGROUP 33E534132-02-03 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR)CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE LH/RH.22800 FCOR150000 FH10500 FCOR69000 FHGROUP 32ER 534135-01-01 833 843GENERAL VISUAL INSPECTION OF DOOR STOP FITTINGS OFDOOR 4 (AFT PASSENGER/CREW DOOR) AT FR 73A AND 75ALH/RH.14000 FC 14000 FC A330-200ORA330-300534136-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE SKIN OF AFTCARGO COMPARTMENT DOOR CUT-OUT AT UPPER REARAND LOWER FORWARD CORNERS, EXTERNAL SURFACE.22800 FCOR90000 FH6245 FCOR24650 FHGROUP 33APRE 41045ORGROUP 33BPRE 41045ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 40TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534137-01-02 N/ADETAILED INSPECTION OFFUSELAGE SKIN OF AFT CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER AND LOWERCORNERS, EXTERNAL SURFACE.22800 FCOR90000 FH8360 FCOR33000 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DORGROUP 33E534137-01-03 N/ADETAILED INSPECTION OFFUSELAGE SKIN OF AFT CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER AND LOWERCORNERS, EXTERNAL SURFACE.22800 FCOR126000 FH8000 FCOR44200 FHGROUP 32ER 534139-01-04 822GENERAL VISUALINSPECTION OF AFT CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERAL3500 FC 3500 FC A330-200OR,FRAMES (FR 59A AND 65) AS FAR AS VISIBLE.A330-300R 534140-02-02 822GENERAL VISUAL INSPECTION OF LOCK FITTINGS OF AFTCARGO COMPARTMENT DOOR AT 10 POSITIONS BETWEENFR 59A AND FR 65.7500 FC 7500 FC A330-200ORA330-300534143-01-02 N/ADETAILED INSPECTIONOF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.22800 FC 5870 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534143-01-03 N/ADETAILED INSPECTIONOF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.22800 FCOR84000 FH8000 FCOR29400 FHGROUP 33E534143-01-04 N/ADETAILED INSPECTIONOF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.22800 FCOR120000 FH8000 FCOR42100 FHGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 41TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534144-01-02 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.22800 FC 5870 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534144-01-03 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.22800 FCOR84000 FH8000 FCOR29400 FHGROUP 33E534144-01-04 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGO COMPARTMENTDOOR CUT-OUT STRUCTURE UNDERNEATH SCUFF PLATE.22800 FCOR120000 FH8000 FCOR42100 FHGROUP 32ER 534146-01-02 823GENERAL VISUAL INSPECTIONOF BULK CARGO10000 FC 10000 FC A330-200COMPARTMENT DOOR STOP FITTINGS AT 10 POSITIONS ATFR 67 AND 69.ORA330-300534148-01-02 ANTENNADETAILEDINSPECTION OF SKIN AROUND VHF 3 ANTENNACUT-OUT BETWEEN FR 56 ANDFR 57 FROM STRINGERS 2LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.22800 FCOR84000 FH8170 FCOR30100 FHGROUP 33AORGROUP 33B534148-01-03 ANTENNADETAILEDINSPECTION OF SKIN AROUND VHF 3 ANTENNACUT-OUT BETWEEN FR 56 ANDFR 57 FROM STRINGERS 2LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.22800 FCOR84000 FH11400 FCOR42000 FHGROUP 32AORGROUP 33CORGROUP 33DORGROUP 33E534148-01-04 ANTENNADETAILEDINSPECTION OF SKIN AROUND VHF 3 ANTENNACUT-OUT BETWEEN FR 56 ANDFR 57 FROM STRINGERS 2LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE.22800 FCOR126000 FH11400 FCOR63000 FHGROUP 32ER 534149-01-02 823GENERAL VISUALINSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OF LATERALFRAMES (FR 67 AND FR 69) AS FAR AS VISIBLE.3500 FC 3500 FC A330-200ORA330-300R 534150-01-02 823LININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OFCARGO FLOOR ATTACHMENT FITTINGS, FROM FR 54 TO FR 64LH AND FROM FR 54 TO FR 58 RH, BETWEEN STR 39 AND STR45 FROM FR 65 TO FR 69 LH, BETWEEN STR 41 AND STR 50.20000 FC 10000 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 42TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 534150-01-03 823LININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUN-OUTS OFCARGO FLOOR ATTACHMENT FITTINGS, FROM FR 58 TO FR 64LH, BETWEEN STR 39 AND STR 45, FROM FR 65 TO FR 69 LH,BETWEEN STR 41 AND STR 50.27900 FCOR83800 FH7900 FCOR23700 FHA330-200F534151-01-01 833 843DOOR FRAME LININGDETAILED INSPECTION OF WEB OF FUSELAGE DOOR FRAME73A, FROM CABIN FLOOR TO STRINGER 11, LH/RH20000 FC 10000 FC GROUP 33APRE 44204ORGROUP 33BPRE 44204534152-01-01 833 843SIDEWALL LININGSNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTUREFROM FR 60 TO FR 66 AND FROM STR 18 TO STR 23 RH INFRAME COUPLING AREA.20000 FC 8000 FC GROUP 33APRE 44203ORGROUP 33BPRE 44203534153-01-01 162ZW 823NOTE 1DETAILED INSPECTION OF WEB OF FR 73A BELOW CABINFLOOR, BETWEEN STR 26 AND 26X LH/RH.20000 FC 8000 FC GROUP 33APRE 44989,PRE 44043ORGROUP 33BPRE 44989PRE 44043R 534154-01-02 833 843LININGINSULATIONDETAILED INSPECTION OFINTERNAL STRUCTURE OFTORSION BOX, INCLUDINGSKIN AND SPLICE PLATE,BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 AND FR76, LH/RH.20000 FC 8000 FC A330-200ORA330-300R 534155-01-02 833 843LININGINSULATIONSPECIAL DETAILED INSPECTION OF TORSION BOXLONGITUDINAL BEAM ADJACENTTO RUNOUT OF CORNERDOUBLER BETWEEN FR 73A AND FR 74, LH/RH.20000 FC 8000 FC A330-200ORA330-300534156-01-02 822LININGCARGO FLOOR PANELSINSULATIONDETAILED INSPECTION OFINTERNAL STRUCTURE BELOWAFT CARGO COMPARTMENT DOOR CUT-OUT BETWEEN FR 59AND 67, FROM CARGO FLOOR LEVEL TO STR 47 RH.15000 FC 8000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 43TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330534164-01-01 822CEILING PANELSSPECIAL DETAILED INSPECTION OF AFT FUSELAGE, CARGODOOR ACTUATOR SUPPORT BEAM BETWEEN FR 61 AND FR62.20000 FC 6000 FC GROUP 33APOST 44072PRE 45489ORGROUP 33BPOST 44072PRE 45489534165-01-01 162ZW 823NOTE 1DETAILED INSPECTION OF WEB OF FR 75A, BELOW CABINFLOOR, BETWEEN STR 26 AND STR 26X, LH/RH.20000 FC 8000 FC GROUP 33APRE 46866PRE 43517ORGROUP 33BPRE 46866PRE 43517534166-01-02 ANTENNASPECIAL DETAILED INSPECTION OF SKIN AROUND VHF2ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 5620000 FC 4700 FC GROUP 32APOST 46025,TO STR 57, RH.PRE 46849PRE 48442ORGROUP 33APOST 46025PRE 46849PRE 48442ORGROUP 33BPOST 46025PRE 46849PRE 48442ORGROUP 33CPOST 46025PRE 46849PRE 48442ORGROUP 33DPOST 46025PRE 46849PRE 48442534166-01-03 ANTENNASPECIAL DETAILED INSPECTION OF SKIN AROUND VHF2ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55, FROM STR 5122000 FC 18000 FC GROUP 32APOST 46849TO STR 52, LH.PRE 48442ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 44TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 534177-01-03 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TOCROWN CENTER LINE, EXLUDING AREA UNDER VERTICALSTABILIZER FAIRING.NOTE: THIS TASK IS ANALTERNATIVE TOTASK534177-02-034500 FC 4500 FC A330-200ORA330-300N 534177-02-03 N/ADETAILED INSPECTIONOF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TOCROWN CENTER LINE, EXLUDING AREA UNDER VERTICALSTABILIZER FAIRING.NOTE: THIS TASK IS ANALTERNATIVE TOTASK534177-02-036900 FC 6900 FC A330-200ORA330-300N 534182-01-01 835LININGSPECIAL DETAILED INSPECTION OF FRAME AND FRAMECOUPLING FROM FR 60 TO FR 64 BETWEEN STR 20X AND STR10300 FCOR3600 FCORA330-200FNOTE123, RH.30900 FH 10800 FHN 534184-01-01 821LININGNOTE1DETAILED INSPECTION OF FRAME AND FRAME COUPLING ATFR 67, STR 33 RH AND FR 69, STR 33 RH.23200 FCOR69600 FH7900 FCOR23700 FHA330-200F535103-01-02 312ARDETAILED INSPECTION OFREAR PRESSURE BULKHEAD AFTFACE, INCLUDING ATTACHMENT TO SKIN, BETWEEN STR 26LH/RH AND CROWN CENTER LINE.16500 FC 7500 FC GROUP 32APRE 48980ORGROUP 33APRE 48980ORGROUP 33BPRE 48980ORGROUP 33CPRE 48980ORGROUP 33DPRE 48980ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 45TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330535104-02-01 312ARGENERAL VISUAL INSPECTION OF REAR PRESSUREBULKHEAD AFT FACE, INCLUDING ATTACHMENT TO SKIN,BETWEEN STR 26 LH/RH AND BOTTOM CENTER LINE.3600 FC 3600 FC GROUP 32APRE 48980ORGROUP 33APRE 48980ORGROUP 33BPRE 48980ORGROUP 33CPRE 48980ORGROUP 33DPRE 48980N 545103-02-04 ENGINESPECIAL DETAILED INSPECTION OF PYLON PYRAMID, END OFARMS AT ENGINE FORWARD MOUNT FITTING.18100 FC 18100 FC A330-200F545104-02-03 415AL 416AR 425AL426AR 453AZ 463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)18400 FCOR55000 FH1500 FCOR4400 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CPRE 48298ORGEGROUP 33DPRE 48298ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 46TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545104-02-04 415AL 415BL 416AR416BR 425AL 425BL426AR 426BR 453AZ463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)18400 FCOR55000 FH1350 FCOR4100 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545104-02-05 415AL 416AR 425AL426AR 453AZ 463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.18400 FCOR55000 FH1250 FCOR3800 FHRRGROUP 33AOR(2 FASTENER LOCATIONS/PYLON)RRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545104-02-12 415AL 416AR 425AL426AR 453AZ 463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)18700 FCOR93600 FH1400 FCOR7000 FHGEGROUP 32APRE 48298545104-02-13 415AL 415BL 416AR416BR 425AL 425BL426AR 426BR 453AZ463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)18700 FCOR93600 FH1300 FCOR6600 FHPWGROUP 32APRE 48298545104-02-14 415AL 416AR 425AL426AR 453AZ 463AZSPECIAL DETAILED INSPECTION OF PYLON PYRAMIDATTACHMENT AREAS AT AFT END OF LOWER ARMSBETWEEN RIB 1 AND RIB 2.(2 FASTENER LOCATIONS/PYLON)18700 FCOR93600 FH1200 FCOR6100 FHRRGROUP 32APRE 48298N 545108-04-19 415AL 416AR 425AL 426AR415BL 416BR 425BL 426BRDETAILED INSPECTION OF PYLON PYRAMID FROM ENGINEFORWARD MOUNT FITTING TO RIB 1.7700 FC 7700 FCPWA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 47TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 545108-04-20 415AL 416AR 425AL426AR DETAILED INSPECTION OF PYLON PYRAMID FROM ENGINEFORWARD MOUNT FITTING TO RIB 1.7700 FC 7700 FC RRA330-200F545111-02-01 ENGINEAFT ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF PYLON, ENGINE AFTATTACHMENT UPPER BEAM AT RIB 9C.9500 FCOR98300 FH9500 FCOR98300 FHGE545138-01-06 N/ADETAILED INSPECTION OFPYLON LATERAL PANELS, AREAOF FASTENERS SECURING SUPPORT TO FRONT ACCESSDOOR, BEETWEEN RIB 10 AND RIB 11.39400 FCOR150000 FH12800 FCOR50000 FHGEGROUP 32AORPWGROUP 32A545138-01-07 N/ADETAILED INSPECTION OFPYLON LATERAL PANELS, AREAOF FASTENERS SECURING SUPPORT TO FRONT ACCESSDOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-02-03.19000 FCOR56900 FH6100 FCOR18400 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545138-01-09 N/ADETAILED INSPECTION OFPYLON LATERAL PANELS, AREAOF FASTENERS SECURING SUPPORT TO FRONT ACCESSDOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-02-05.25100 FCOR75300 FH8000 FCOR24100 FHRRGROUP 33E545138-01-10 N/ADETAILED INSPECTION OFPYLON LATERAL PANELS, AREAOF FASTENERS SECURING SUPPORT TO FRONT ACCESSDOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-02-06.21900 FCOR109000 FH7000 FCOR35100 FHRRGROUP 32E545138-01-12 N/ADETAILED INSPECTION OFPYLON LATERAL PANELS, AREAOF FASTENERS SECURING SUPPORT TO FRONT ACCESSDOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK545138-02-1217900 FCOR89500 FH5750 FCOR28800 FHRRGROUP 32AISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 48TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545138-02-03 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-01-07.19000 FCOR56900 FH12400 FCOR37200 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545138-02-05 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-01-09.25100 FCOR75300 FH16400 FCOR49300 FHRRGROUP 33E545138-02-06 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-01-10.21900 FCOR109000 FH14300 FCOR71700 FHRRGROUP 32E545138-02-12 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS ANALTERNATIVE TOTASK545138-01-1217900 FCOR89500 FH11700 FCOR50000 FHRRGROUP 32AISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 49TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 545140-01-01 N/ADETAILED INSPECTION OFPYLON, LATERAL PANELS, AREAOF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025 FOR A/CTHAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL(4750 FC OR 14250 FH)10950 FCOR32850 FH4750 FCOR14250 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304R 545140-01-02 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS, AREA 11720 FC 3770 FCRR,OF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALIINTERVAL (3770 FC OR 11310 FH)OR35180 FHOR11310 FHGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 50TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 545140-01-03 N/ADETAILED INSPECTION OFPYLON, LATERAL PANELS, AREAOF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALIINTERVAL (3060 FC OR 9180 FH)8290 FCOR24870 FH3060 FCOR9180 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304545140-01-06 N/ADETAILEDINSPECTION OF PYLON,LATERAL PANELS,AREA 10500 FC 4560 FCGER545140 01 06N/ADETAILEDINSPECTIONOFPYLONLATERALPANELSAREAOF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALIINTERVAL (4560 FC OR 22800 FH)10500FCOR52500 FH4560FCOR22800 FHGEGROUP 32AORGEGROUP 32EPRE 57304R 545140-01-07 N/ADETAILED INSPECTION OFPYLON, LATERAL PANELS, AREAOF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL(3620 FC OR 18090 FH)11250 FCOR56250 FH3620 FCOR18090 FHRRGROUP 32AORRRGROUP 32EPRE 57304ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 51TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 545140-01-08 N/ADETAILED INSPECTION OFPYLON, LATERAL PANELS, AREAOF FASTENERS NEAR UPPER EDGE AT RIB 8 LEVEL,EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-02-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL(2930 FC OR 14680 FH)7950 FCOR39770 FH2930 FCOR14680 FHPWGROUP 32AORPWGROUP 32EPRE 57304R 545140-02-01 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-0110950 FCOR32850 FH7600 FCOR22800 FHGEGROUP 33AORGEGROUP 33BNOTE:THISTASKISANALTERNATIVETOTASK545140-01-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025 FOR A/CTHAT HAVE ALREADY BEEN INSPECTED THROUGH AOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALI INTERVAL(7600 FC OR 22800 FH)GROUP33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 52TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 545140-02-02 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-01-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALIINTERVAL (7100 FC OR 21310 FH)11720 FCOR35180 FH7100 FCOR21310 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304R 545140-02-03 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERAL8290 FC 5630 FCPW,PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-01-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS REVISED ALIINTERVAL (5630 FC OR 16900 FH)OR24870 FHOR16900 FHGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 53TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 545140-02-06 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-01-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL(7290 FC OR 36450 FH)10500 FCOR52500 FH7290 FCOR36450 FHGEGROUP 32AORGEGROUP 32EPRE 57304R 545140-02-07 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-0711250 FCOR56250 FH6810 FCOR34080 FHRRGROUP 32AORRRGROUP 32ENOTE:THISTASKISANALTERNATIVETOTASK545140-01-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL(6810 FC OR 34080 FH)GROUP32EPRE 57304R 545140-02-08 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545140-01-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTED THROUGHAOT A330-54A3025, NEXT DUE IS WITHIN THIS ALI INTERVAL(5400 FC OR 27030 FH)7950 FCOR39770 FH5400 FCOR27030 FHPWGROUP 32AORPWGROUP 32EPRE 57304N 545140-02-09 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.10900 FCOR32800 FH7600 FCOR22800 FHGEGROUP 33EPOST 57304ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 54TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 545140-02-10 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.11700 FCOR35100 FH7100 FCOR21300 FHRRGROUP 33EPOST 57304N 545140-02-11 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.8250 FCOR24800 FH5600 FCOR16900 FHPWGROUP 33EPOST 57304N 545140-02-12 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.10500 FCOR52500 FH7250 FCOR36400 FHGEGROUP 32EPOST 57304N 545140-02-13 FASTENERSSPECIAL DETAILED INSPECTION OFPYLON, LATERAL11200 FC 6800 FCRR,PANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.OR56200 FHOR34000 FHGROUP 32EPOST 57304N 545140-02-14 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.7950 FCOR39700 FH5400 FCOR27000 FHPWGROUP 32EPOST 57304N 545140-02-15 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.7950 FC 5400 FCPWA330-200FN 545140-02-16 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.11200 FC 6800 FCRRA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 55TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545142-02-01 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.9700 FCOR29200 FH9700 FCOR29200 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33D545142-02-02 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.8000 FCOR24100 FH8000 FCOR24100 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545142-02-05 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.14900 FCOR44800 FH14900 FCOR44800 FHGEGROUP 33EORPWGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 56TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545142-02-06 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.11200 FCOR33500 FH11200 FCOR33500 FHRRGROUP 33E545142-02-07 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.13900 FCOR69300 FH13900 FCOR69300 FHGEGROUP 32EORPWGROUP 32E545142-02-08 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.10400 FCOR51700 FH10400 FCOR51700 FHRRGROUP 32E545142-02-09 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 139300 FCOR46500 FH9300 FCOR46500 FHGEGROUP 32AORAND RIB 14.PWGROUP 32A545142-02-10 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.7650 FCOR38400 FH7650 FCOR38400 FHRRGROUP 32AN 545142-02-11 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.11700 FCOR35200 FH11700 FCOR35200 FHPWA330-200FN 545142-02-12 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS MATING SURFACE ANDINTERNAL AREA 30 MM AROUND CUTOUT BETWEEN RIB 13AND RIB 14.14000 FCOR42100 FH14000 FCOR42100 FHRRA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 57TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545143-02-04 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-03-01.22600 FCOR67900 FH3700 FCOR11200 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545143-02-09 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-03-04.29000 FCOR87000 FH5100 FCOR15300 FHRRGROUP 33E545143-02-10 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-03-05.25300 FCOR126000 FH4450 FCOR22300 FHRRGROUP 32E545143-02-13 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS, EDGEOF ACCESS DOOR CUTOUTS AND MATING SURFACEBETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-03-1321400 FCOR107000 FH3500 FCOR17600 FHRRGROUP 32A545143-03-01 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-02-04.22600 FCOR67900 FH9900 FCOR29700 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 58TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545143-03-04 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-02-09.29000 FCOR87000 FH13200 FCOR39700 FHRRGROUP 33E545143-03-05 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-02-10.25300 FCOR126000 FH11500 FCOR57700 FHRRGROUP 32E545143-03-13 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.21400 FCOR107000 FH9350 FCOR46800 FHRRGROUP 32ANOTE: THIS TASK IS ANALTERNATIVE TOTASK545143-02-13545146-03-01 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-01.20900 FCOR62700 FH11300 FCOR33800 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 59TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545146-03-02 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-02.16200 FCOR48700 FH8000 FCOR24100 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545146-03-03 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION28500 FCOR85500 FH12400 FCOR37300 FHGEGROUP 33EORPWGROUP 33E- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-03.545146-03-04 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-04.20500 FCOR61500 FH8800 FCOR26500 FHRRGROUP 33E545146-03-05 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-05.26500 FCOR132000 FH11500 FCOR57600 FHGEGROUP 32EORPWGROUP 32E545146-03-06 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-06.19100 FCOR95300 FH8200 FCOR41000 FHRRGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 60TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545146-03-07 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-0719900 FCOR99800 FH10700 FCOR50000 FHGEGROUP 32AORPWGROUP 32A545146-03-08 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 545146-04-0815500 FCOR77600 FH7650 FCOR38300 FHRRGROUP 32A545146-04-01 452AL 453BL 453BR462AL 463BL 463BRSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.20900 FCOR6600 FCORGEGROUP 33APRE-COOLERRODS, AIR DUCT,NOTES :- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-01.62700 FH 19800 FH ORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 61TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545146-04-02 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-02.16200 FCOR48700 FH4500 FCOR13600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545146-04-03 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE28500 FCOR85500 FH6750 FCOR20200 FHGEGROUP 33EORPWGROUP 33E- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-03.545146-04-04 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-04.20500 FCOR61500 FH4450 FCOR13300 FHRRGROUP 33E545146-04-05 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-05.26500 FCOR132000 FH6250 FCOR31300 FHGEGROUP 32EORPWGROUP 32E545146-04-06 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-06.19100 FCOR95300 FH4130 FCOR20600 FHRRGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 62TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545146-04-07 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES :- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-0719900 FCOR99800 FH6300 FCOR31500 FHGEGROUP 32AORPWGROUP 32A545146-04-08 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWER SPARAND LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 7.NOTES:- INSPECTION THROUGH FLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TOTASK 545146-03-0815500 FCOR77600 FH4300 FCOR21600 FHRRGROUP 32A545150-02-01 452AL 462ALPRE-COOLERDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.27900 FCOR9000 FCORGEGROUP 33ARODSAIR DUCT,83600 FH 27100 FH ORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 63TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545150-02-02 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.23000 FCOR69100 FH6500 FCOR19400 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33D545150-02-06 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.31000 FCOR93000 FH11700 FCOR35100 FHPWGROUP 33E545150-02-07 452AL 462ALDETAILEDINSPECTION OF PYLON, UPPER SPAR AND30300 FC 11400 FC PWPRE-COOLERRODSAIR DUCT,LATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.OR150000 FHOR57100 FHGROUP 32E545150-02-10 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.26600 FCOR133000 FH8650 FCOR43200 FHGEGROUP 32AORRRGROUP 32A545150-02-11 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.22000 FCOR110000 FH6200 FCOR31000 FHPWGROUP 32AN 545150-02-13 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8.19400 FC 6900 FCPWA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 64TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545166-02-05 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.35000 FCOR105100 FH8100 FCOR24300 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33D545166-02-06 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.21400 FCOR64100 FH4600 FCOR13800 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545166-02-08 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.20500 FCOR61500 FH4440 FCOR13300 FHRRGROUP 33E545166-02-09 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.30100 FCOR150000 FH7000 FCOR34800 FHGEGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 65TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545166-02-10 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.18400 FCOR91900 FH3960 FCOR19800 FHRRGROUP 32E545166-02-13 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.30600 FCOR150000 FH7050 FCOR35400 FHGEGROUP 32AORPWGROUP 32A545166-02-14 454BL 454BR 464BL464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTINGS AT RIB 12.18700 FCOR93500 FH4000 FCOR20100 FHRRGROUP 32A545168-02-05 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON).35000 FCOR105100 FH8100 FCOR24300 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 66TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545168-02-06 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON).21400 FCOR64100 FH4600 FCOR13800 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33D545168-02-08 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON).20500 FCOR61500 FH4440 FCOR13300 FHRRGROUP 33E545168-02-09 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON).30100 FCOR7000 FCORGEGROUP 32E( )150000 FH 34800 FH545168-02-10 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON).18400 FCOR91900 FH3960 FCOR19800 FHRRGROUP 32E545168-02-13 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)30600 FCOR150000 FH7050 FCOR35400 FHGEGROUP 32AORPWGROUP 32A545168-02-14 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)18700 FCOR93500 FH4000 FCOR20100 FHRRGROUP 32AN 545168-02-15 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)17000 FC 7900 FCPWA330-200FN 545168-02-16 452CL 452CR 462CL 462CR454BL 454BR 464BL 464BRDETAILED INSPECTION OF PYLON TO WING ATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)17000 FC 4400 FCRRA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 67TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545174-02-03 PRE 43271:454DL 454DR 454FL 454FR464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR464KL 464KR 464ML 464MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A.38500 FCOR115400 FH10700 FCOR32000 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33D545174-02-06 PRE 43271:454DL 454DR 454FL 454FR464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A.38600 FCOR115700 FH7700 FCOR23200 FHRRGROUP 33AORRRGROUP 33B464KL 464KR 464ML 464MRORRRGROUP 33CORRRGROUP 33D545174-02-07 PRE 43271:454DL 454DR 454FL 454FR464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR464KL 464KR 464ML 464MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A38000 FCOR150000 FH7600 FCOR38100 FHRRGROUP 32A545174-02-09 PRE 43271:454DL 454DR 454FL 454FR464DL 464DR 464FL 464FRPOST 43271:454KL 454KR 454ML 454MR464KL 464KR 464ML 464MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A37800 FCOR150000 FH10500 FCOR50000 FHPWGROUP 32AN 545174-02-10 454KL 454KR 454ML 454MR464KL 464KR 464ML 464MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A17000 FC 10300 FC31100 FHPWA330-200FN 545174-02-11 454KL 454KR 454ML 454MR464KL 464KR 464ML 464MRDETAILED INSPECTION OF PYLON TO WING ATTACHEMENTFITTING AND LINKS AT RIB 18A17000 FC 13300 FC39900 FHRRA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 68TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330545180-04-04 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON).18100 FCOR50000 FH18100 FCOR50000 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D545180-04-05 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON).17000 FCOR50000 FH17000 FCOR50000 FHGROUP 33E545180-04-06 ENGINELINKSSLEEVESAFT SECONDARYSPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON).16000 FCOR80000 FH16000 FCOR80000 FHGROUP 32ESTRUCTURE545180-04-07 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON)17800 FCOR50000 FH17800 FCOR50000 FHGROUP 32AN545180-04-09 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON)17000 FC 12900 FC PWA330-200FN 545180-04-10 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB 18A (3PLACES PER PYLON)17000 FC 17000 FC RRA330-200FN 551008-01-04 312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZER CENTERBOX TOP SKIN SPANWISE SPLICES BETWEEN FUSELAGEFAIRING LINES.27200 FCOR81600 FH4900 FCOR14700 FHA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 69TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330551016-01-02 313ALSPECIAL DETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN REAR UPPER FLANGE JUSTOUTBOARD OF RIB 3, LH/RH.33100 FCOR96400 FH20000 FCOR60000 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DN 551024-01-04 331 / 341BT, AT333 / 343AT, ABGENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZERLATERAL BOX FRONT SPAR FORWARD FACE BETWEEN RIB 3AND 4.16600 FCOR50000 FH16600 FCOR50000 FHA330-200F571102-01-01 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.15000 FCOR75400 FH5000 FCOR25100 FHGROUP 32APRE 49202PRE 52094ORPOST 50755PRE 52094571102-01-02 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.21500 FCOR107900 FH5000 FCOR25100 FHGROUP 32APOST 49202PRE 50755ORPRE 49202POST 52094ORPOST 50755POST 52094571102-01-03 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.17200 FCOR51600 FH6000 FCOR18100 FHGROUP 33APOST 44360PRE 52094ORGROUP 33BPOST 44360PRE 52094571102-01-04 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.16500 FCOR49700 FH5400 FCOR16200 FHGROUP 33CPRE 49202PRE 52094ORGROUP 33DPRE 49202PRE 52094ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 70TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571102-01-05 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.24200 FCOR72700 FH5550 FCOR16600 FHGROUP 33E571102-01-06 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.22400 FCOR112000 FH5140 FCOR25700 FHGROUP 32E571102-01-07 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.23700 FCOR71100 FH5400 FCOR16200 FHGROUP 33CPOST 49202ORPRE 49202POST 52094ORGROUP 33DPOST 49202ORPRE 49202POST 52094571102-01-08 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.24400 FCOR73200 FH6000 FCOR18100 FHGROUP 33APOST 44360POST 52094ORGROUP 33BPOST 44360POST 52094N 571102-01-09 821NOTE 1LININGAIR CONDITIONING DUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTING ATSTRINGER 38 LEVEL, LH/RH.16300 FC 4600 FC A330-200F571103-01-03 191HB 192HB 821NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-02-03.15600 FCOR46900 FH6600 FCOR20000 FHGROUP 33APOST 44360PRE 50745ORGROUP 33BPOST 44360PRE 50745ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 71TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571103-01-04 191HB 192HB 821NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-02-04.14400 FCOR72000 FH6000 FCOR30200 FHGROUP 32APRE 49202PRE 50745571103-01-05 191HB 192HB 821NOTE 1LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-02-0515600 FCOR46800 FH6400 FCOR19300 FHGROUP 33DPRE 49202PRE 50745R 571103-01-06 191HB 192HB 821NOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OF15800 FCOR6500 FCORGROUP 33CPRE 49202LININGAIR CONDITIONING DUCTSFASTENER (2 POSITIONS),FASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-02-06.47500 FH 19500 FH PRE 50745571103-02-03 821NOTE 1LININGAIR CONDITIONING DUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-01-0315600 FCOR46900 FH1450 FCOR4350 FHGROUP 33APOST 44360PRE 50745ORGROUP 33BPOST 44360PRE 50745571103-02-04 821NOTE 1LININGAIR CONDITIONING DUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-01-04.14400 FCOR72000 FH930 FCOR4650 FHGROUP 32APRE 49202PRE 50745ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 72TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571103-02-05 821NOTE 1LININGAIR CONDITIONING DUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-01-0515600 FCOR46800 FH990 FCOR2950 FHGROUP 33DPRE 49202PRE 50745R 571103-02-06 821NOTE 1LININGAIR CONDITIONING DUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGE IN AREA OFFASTENERS BETWEEN STR. 39 AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TOTASK 571103-01-06.15800 FCOR47500 FH1000 FCOR3000 FHGROUP 33CPRE 49202PRE 50745571104-01-01 191KB 192PBFASTENER TO BE REMOVEDSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OF28100 FCOR7100 FCORGROUP 33APRE 44360821131CX 131DX 132CX 132DX,FASTENER BETWEEN STR 38 AND STR 39, LH/RH.84500 FH 21300 FH POST 52094ORGROUP 33BPRE 44360POST 52094571104-01-02 191KB 192PBFASTENER TO BE REMOVED821131CX 131DX 132CX 132DXSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR38 AND STR 39, LH/RH.16500 FCOR49600 FH7100 FCOR21300 FHGROUP 33APRE 44360PRE 52094ORGROUP 33BPRE 44360PRE 52094571104-01-03 191KB 192PBFASTENER TO BE REMOVED821131CX 131DX 132CX 132DXSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR38 AND STR 39, LH/RH.26100 FCOR78400 FH7100 FCOR21300 FHGROUP 33APOST 44360PRE 52094ORGROUP 33BPOST 44360PRE 52094ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 73TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571104-01-04 191KB 192PBFASTENER TO BE REMOVED821131CX 131DX 132CX 132DXSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR38 AND STR 39, LH/RH.19500 FCOR97800 FH5600 FCOR28000 FHGROUP 32APRE 49202PRE 52094ORPOST 50755PRE 52094571104-01-05 191KB 192PBFASTENER TO BE REMOVED821131CX 131DX 132CX 132DXSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 REAR FITTING WEB IN AREA OFFASTENER BETWEEN STR38 AND STR 39, LH/RH.23200 FCOR69600 FH6300 FCOR19000 FHGROUP 33CPRE 49202PRE 52094ORGROUP 33DPRE 49202PRE 52094571107-01-01 191QB 192QBSPECIAL DETAILEDINSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y=2427 BETWEEN31900 FCOR5300 FCORGROUP 32A,STRINGERS 20 & 21, LH/RH.159600 FH 26700 FH571107-01-03 191QB 192QBSPECIAL DETAILEDINSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y=2427 BETWEENSTRINGERS 20 & 21, LH/RH.36800 FCOR110700 FH5900 FCOR17700 FHGROUP 33CORGROUP 33D571107-01-04 191QB 192QBSPECIAL DETAILEDINSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y=2427 BETWEENSTRINGERS 20 & 21, LH/RH.28500 FCOR85600 FH6200 FCOR18600 FHGROUP 33AORGROUP 33B571107-01-05 191QB 192QBSPECIAL DETAILEDINSPECTION OF CENTER WING BOXLOWER PANEL, DRAIN HOLES AT Y=2427 BETWEENSTRINGERS 20 & 21, LH/RH.31500 FCOR157000 FH5100 FCOR25500 FHGROUP 32E571108-01-04 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.40300 FCOR121100 FH8300 FCOR25100 FHGROUP 33C571108-01-05 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.36700 FCOR110300 FH8400 FCOR25200 FHGROUP 33AORGROUP 33B571108-01-06 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.34500 FCOR172500 FH7400 FCOR37300 FHGROUP 32A571108-01-07 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX INTERNALSTRUCTURE, LOWER SKIN PANEL AND STIFFENERS.39100 FCOR117500 FH8150 FCOR24500 FHGROUP 33DISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 74TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571110-01-01 821NOTE 1LININGAIR CONDITIONING DUCTSSPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 40 FRONT FITTING FLANGEREINFORCING STRAP, 4 FASTENER HOLES AT STR. 38 LEVEL,LH/RH.25000 FCOR75000 FH790 FCOR2380 FHGROUP 33APRE 44360POST 45899POST 53239ORGROUP 33BPRE 44360POST 45899POST 53239571114-01-05 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.31100 FCOR93300 FH13000 FCOR39000 FHGROUP 33AORGROUP 33B571114-01-06 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.23300 FCOR116700 FH10900 FCOR54500 FHGROUP 32A571114-01-07 147AZ 148AZ734SPECIAL DETAILED INSPECTION OF CENTER WING BOX 26500 FC 11900 FC GROUP 33D744INTERNAL STRUCTURE, DRAIN HOLES AT STIFFENERS 27AND 28.OR79500 FHOR35800 FHORGROUP 33C571116-01-02 193DBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 & 22, AT Y =-567.531900 FCOR159600 FH5350 FCOR26700 FHGROUP 32A571116-01-03 193DBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 & 22, AT Y =-567.536800 FCOR110700 FH5900 FCOR17700 FHGROUP 33CORGROUP 33D571116-01-04 193DBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 & 22, AT Y =-567.5.28500 FCOR85600 FH6200 FCOR18600 FHGROUP 33AORGROUP 33B571116-01-05 193DBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, FUEL LEVEL MAGNETIC INDICATOR AREABETWEEN STRINGERS 21 & 22, AT Y =-567.5.31500 FCOR157000 FH5100 FCOR25500 FHGROUP 32E571118-01-06 FAIRING PANELS BETWEENFR.44 AND FR.47SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEENSTRINGERS 27 & 28.31900 FCOR159600 FH5350 FCOR26700 FHGROUP 32A571118-01-07 FAIRING PANELS BETWEENFR.44 AND FR.47SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEENSTRINGERS 27 & 28.28500 FCOR85600 FH6200 FCOR18600 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 75TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571118-01-08 FAIRING PANELS BETWEENFR.44 AND FR.47SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEENSTRINGERS 27 & 28.36800 FCOR110700 FH5900 FCOR17700 FHGROUP 33CORGROUP 33D571118-01-09 FAIRING PANELS BETWEENFR.44 AND FR.4SPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, HYDRAULIC CONNECTORS AREA AT Y=-2230BETWEEN STRINGERS 25 & 26, AND AT Y=180 BETWEENSTRINGERS 27 & 28.31500 FCOR150000 FH5100 FCOR25500 FHGROUP 32E571122-01-04 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOXEXTERNAL STRUCTURE, FASTENERS AREA AT REAR SPARLOWER CHORD (L FITTING) AND LOWER SKIN JUNCTION,FROM Y=953 TO Y=1959, LH/RH.36800 FCOR110400 FH4900 FCOR14700 FHGROUP 33AORGROUP 33BN 571123-01-01 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAMEFROM FR 40.3 TO FR 45, LH/RH.28400 FCOR85400 FH13400 FCOR40300 FHGROUP 33APOST 49404ORGROUP 33BPOST 49404N 571123-01-02 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAMEFROM FR 40.3 TO FR 45, LH/RH.26300 FCOR78900 FH11800 FCOR35400 FHGROUP 33CPOST 49404ORGROUP 33DPOST 49404N 571123-01-03 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME FOOT JUNCTION WITH LATERAL FRAMEFROM FR 40.3 TO FR 45, LH/RH.19800 FCOR99000 FH8200 FCOR41100 FHGROUP 32APOST 49404571125-01-03 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX REARSPAR AFT FACE, FASTENERS AREA BETWEENY=2219 ANDFRAME 47 LOWER CORNER FITTING, LH/RH.26800 FCOR80600 FH6150 FCOR18500 FHGROUP 33AORGROUP 33B571125-01-04 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX REARSPAR AFT FACE, FASTENERS AREA BETWEENY=2219 ANDFRAME 47 LOWER CORNER FITTING, LH/RH.21200 FCOR106100 FH4000 FCOR20000 FHGROUP 32A571125-01-05 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX REARSPAR AFT FACE, FASTENERS AREA BETWEENY=2219 ANDFRAME 47 LOWER CORNER FITTING, LH/RH.24500 FCOR73600 FH4400 FCOR13300 FHGROUP 33CORGROUP 33D571126-01-03 734SPECIAL DETAILED INSPECTIONOF CENT WING BOX, REARSPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDELOWER CORNER.31900 FCOR95700 FH13600 FCOR41000 FHGROUP 33AORGROUP 33B571126-01-04 734SPECIAL DETAILED INSPECTIONOF CENT WING BOX, REARSPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDE25900 FCOR10800 FCORGROUP 32ALOWER CORNER.129800 FH 54200 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 76TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571126-01-05 734SPECIAL DETAILED INSPECTIONOF CENT WING BOX, REARSPAR WEB AT APU FUEL PUMP APERTURE IN THE LEFT SIDELOWER CORNER.29400 FCOR88300 FH11900 FCOR35700 FHGROUP 33CORGROUP 33D571129-01-04 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX, CENTERSPAR, 30MM AROUND ACCESS CUT-OUTS (2 PLACES).32500 FCOR97700 FH11500 FCOR34600 FHGROUP 33AORGROUP 33B571130-01-03 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WING BOX,REAR SPAR, 30 MM AROUND MANHOLE CUT-OUTS (2PLACES).32500 FCOR97700 FH6900 FCOR20700 FHGROUP 33AORGROUP 33B571144-01-01 191HB 191QB 192HB192QBSPECIAL DETAILED INSPECTION OF CENTER WING BOX,LOWER SPLICE AT RIB 1, FIRST FASTENER ROWS ON EACHSIDE OF RIB 1 DATUM AT STR.16, STR.20, STR.21 AND STR.25TO 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.37400 FCOR112300 FH9600 FCOR28800 FHGROUP 33APRE 41652ORGROUP 33BPRE 41652571145-01-01 147AZ 148AZ 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX 31300 FC 7600 FC GROUP 33ASEALANT TO BE REMOVED INTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.OR94100 FHOR22900 FHPRE 41652ORGROUP 33BPRE 41652571145-01-03 147AZ 148AZ 734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.30700 FCOR153900 FH8150 FCOR40700 FHGROUP 32A571145-01-04 147AZ 148AZ 734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.32400 FCOR97100 FH8900 FCOR26800 FHGROUP 33E571145-01-05 147AZ 148AZ 734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.27000 FCOR135000 FH7800 FCOR39200 FHGROUP 32E571145-01-06 147AZ 148AZ 734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.33900 FCOR101800 FH9000 FCOR27200 FHGROUP 33CORGROUP 33DN 571145-01-07 147AZ 148AZ 734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING INBOARDFLANGE, FASTENERS IN RADIUSAREA AT STR.16, STR.20,STR.21 AND STR.25 TO 29, LH/RH.32000 FC 9100 FC A330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 77TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571146-02-04 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.32500 FCOR97500 FH9600 FCOR28800 FHGROUP 33AORGROUP 33B571146-02-05 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.27400 FCOR136900 FH7900 FCOR39400 FHGROUP 32A571146-02-06 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.30800 FCOR92500 FH8300 FCOR25000 FHGROUP 33E571146-02-07 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.26500 FCOR133000 FH7400 FCOR37000 FHGROUP 32E,571146-02-08 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.31100 FCOR93200 FH8650 FCOR25900 FHGROUP 33CORGROUP 33DN 571146-02-09 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WING BOXLOWER PANEL, LOWER SURFACE, FIRST FASTENER ROW ONEACH SIDE OF RIB1 BUTT STRAP EDGE, AT STR16, STR20,STR21 AND STR25 TO STR29, LH/RH.30600 FC 8600 FC A330-200F571152-01-02 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, CENTERSPAR FITTING FLANGE,RADIUS AREA AT FASTENERS 3 TO 4 LEVEL AND FLANGE ATFASTENERS 3 TO 12, LH/RH.20000 FCOR60100 FH6600 FCOR19800 FHGROUP 33APRE 41652ORGROUP 33B571153-01-01 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.21900 FCOR65800 FH15200 FCOR45600 FHGROUP 33E571153-01-02 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.18600 FCOR93300 FH12900 FCOR64600 FHGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 78TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571153-01-03 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.12500 FCOR37600 FH9000 FCOR27100 FHGROUP 33APOST 43577ORGROUP 33BPOST44440S13324571153-01-04 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.18500 FCOR55700 FH15700 FCOR47100 FHGROUP 33CORGROUP 33D571153-01-05 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.19100 FCOR57400 FH15900 FCOR47600 FHGROUP 33APRE 43577ORGROUP 33BPOST,44440S13276ORPOST44440S13090ORPOST 44360571153-01-06 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.15600 FCOR78300 FH13800 FCOR69300 FHGROUP 32AN 571153-01-07 147AZ 148AZ734 744SEALANT TO BE REMOVEDSPECIAL DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, STIFFENING RIB AND RADIUS OFGUSSET INSTALLED ON LOWER L FITTING AT CROSSINGAREA WITH KEEL BEAM FITTING AT FR.40, AND LOWER LFITTING RADIUS ON EACH SIDE OF GUSSET, LH/RH.11100 FC 11100 FC A330-200F571159-01-03 CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WING BOXPORTAL BEAMS AT CONNECTION WITH FRONT SPARVERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).25100 FCOR75400 FH8350 FCOR25000 FHGROUP 33AORGROUP 33B571159-01-04 CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WING BOXPORTAL BEAMS AT CONNECTION WITH FRONT SPARVERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).26800 FCOR134000 FH8850 FCOR44400 FHGROUP 32AISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 79TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330571159-01-05 CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WING BOXPORTAL BEAMS AT CONNECTION WITH FRONT SPARVERTICAL STIFFENERS FROM Y=-1959 TO Y=1959 (9 BEAMS).29000 FCOR87100 FH9450 FCOR28300 FHGROUP 33CORGROUP 33DR 571162-01-01 191HB 192HBSPECIAL DETAILEDINSPECTION OF KEEL BEAM FITTING,TWO FASTENERS HOLES IN CONNECTION OF KEEL BEAMFITTING TO CWB BOTTOM PANEL AT STR.1 LEVEL, LH/RH.12900 FCOR38800 FH7400 FCOR22400 FHGROUP 33APRE 41652POST 54459571163-01-01 191HB 192HBSPECIAL DETAILEDINSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.12000 FCOR36000 FH4000 FCOR12100 FHGROUP 33APOST 41652PRE 44360POST 56467ORGROUP 33BPOST 41652PRE 44360POST 56467N 571164-01-01 191HB 192HBDETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, KEEL BEAM FITTINGANGLE AND DOUBLER ATFR 40, LH/RH.19600 FC 7400 FC A330-200F571165-01-03 734 744SPECIAL DETAILED INSPECTION OF CENTER WING BOX REARSPAR, FILET RADIUS FROM Y=1959 TO Y=2219 AND FROM Z=-1859.6 TO Z=-2073, LH/RH.11600 FCOR34900 FH6900 FCOR20700 FHGROUP 33APRE 43865ORGROUP 33BPRE 43865572001-02-01 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREACOVERED BY PYLON FAIRING AND PYLON REINFORCING.28300 FCOR128700 FH5100 FCOR23400 FHGROUP 32APRE 48437572001-02-03 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREACOVERED BY PYLON FAIRING AND PYLON REINFORCING.31000 FCOR91700 FH5600 FCOR16700 FHGROUP 33CPRE 48437572001-02-04 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 1 & 8 AND RIB 9 & 12, EXCLUDING AREACOVERED BY PYLON FAIRING AND PYLON REINFORCING.29600 FCOR87500 FH5400 FCOR15900 FHGROUP 33DPRE 48437572003-01-04 454BL 454BR 454CL454CR 464BL 464BR464CL 464CRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE VISIBLE PORTION OF PYLON REINFORCINGPLATE28300 FCOR128700 FH6200 FCOR28100 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 80TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572003-01-06 454BL 454BR 454CL454CR 464BL 464BR464CL 464CRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE VISIBLE PORTION OF PYLON REINFORCINGPLATE31000 FCOR91700 FH6700 FCOR20000 FHGROUP 33CPRE 48437572003-01-07 454BL 454BR 454CL454CR 464BL 464BR464CL 464CRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE VISIBLE PORTION OF PYLON REINFORCINGPLATE29600 FCOR87500 FH6400 FCOR19100 FHGROUP 33DPRE 48437572004-02-01 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BYMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING.17000 FCOR77400 FH4800 FCOR22100 FHGROUP 32APRE 48437572004-02-03 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BYMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING.37000 FCOR109300 FH8100 FCOR24000 FHGROUP 33AORGROUP 33B572004-02-04 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BYMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING.18900 FCOR55800 FH5400 FCOR15900 FHGROUP 33CPRE 48437572004-02-05 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREAS COVERED BYMAIN LANDING GEAR REINFORCING PLATE, FLAP TRACK 2FAIRING AND PYLON FAIRING.17500 FCOR51700 FH3900 FCOR11600 FHGROUP 33DPRE 48437572005-01-08 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAINLANDING GEAR REINFORCING PLATE INCLUDINGATTACHMENT TO REAR SPAR.39900 FCOR118000 FH9700 FCOR28700 FHGROUP 33APRE 41114ORGROUP 33BPRE 41114572005-01-09 541CB 641CBSPECIAL DETAILEDINSPECTION OF OUTER WING BOTTOMSKIN FORWARD OF REAR SPAR IN AREA MASKED BY MAINLANDING GEAR REINFORCING PLATE INCLUDINGATTACHMENT TO REAR SPAR.39900 FCOR118000 FH9700 FCOR28700 FHGROUP 33APOST 41114ORGROUP 33BPOST 41114572006-01-01 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.12800 FCOR58400 FH4300 FCOR19500 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 81TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572006-01-02 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.13300 FCOR39500 FH4400 FCOR13200 FHGROUP 33CPRE 48437572006-01-03 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.11900 FCOR35200 FH3800 FCOR11400 FHGROUP 33DPRE 48437572006-02-04 N/ADETAILED INSPECTIONOF OUTER WING BOTTOM SKINLOWER SURFACE MAIN LANDING GEAR REINFORCING PLATE.17300 FCOR51200 FH5400 FCOR15900 FHGROUP 33AORGROUP 33B572007-01-04 454GL 454GR 464GL464GR 531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING.17000 FCOR77400 FH8000 FCOR36500 FHGROUP 32APRE 48437572007-01-05 454GL 454GR 464GL464GR 531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING.37000 FCOR109300 FH13800 FCOR40800 FHGROUP 33AORGROUP 33B572007-01-06 454GL 454GR 464GL464GR 531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING.18900 FCOR55800 FH8900 FCOR26300 FHGROUP 33CPRE 48437572007-01-08 454GL 454GR 464GL464GR 531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRING AND PYLON FAIRING.17500 FCOR51700 FH6400 FCOR19100 FHGROUP 33DPRE 48437572008-01-04 531AB 631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE FORWARD OF REAR SPAR IN AREACOVERED BY FLAP TRACK 2 FAIRING.39900 FCOR118000 FH6900 FCOR20500 FHGROUP 33AORGROUP 33B572010-02-04 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10AND 11-12.36500 FCOR165900 FH6400 FCOR29100 FHGROUP 32APRE 48437572010-02-06 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10AND 11-12.39500 FCOR116700 FH6900 FCOR20500 FHGROUP 33CPRE 48437572010-02-07 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUT-OUTS IN RIB BAYS 2-3, 4-5, 6-7, 8-9, 9-10AND 11-12.38500 FCOR113800 FH6700 FCOR20000 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 82TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572012-02-01 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEENRIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAREXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLONREINFORCING PLATE.25900 FCOR117600 FH4700 FCOR21400 FHGROUP 32APRE 48437572012-02-02 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEENRIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAREXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLONREINFORCING PLATE.28500 FCOR84300 FH6300 FCOR18800 FHGROUP 33AORGROUP 33B572012-02-03 FUEL PUMP FAIRINGS DETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEENRIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAREXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLONREINFORCING PLATE.27900 FCOR82400 FH5100 FCOR15000 FHGROUP 33CPRE 48437572012-02-04 FUEL PUMP FAIRINGS DETAILED INSPECTIONOF OUTER WING BOTTOM SKIN 26600 FC 4800 FC GROUP 33DLOWER SURFACE BETWEEN RIB 1 AND RIB 3 AND BETWEENRIB 10 AND RIB 12 FROM FRONT SPAR TO REAR SPAREXCLUDING AREAS COVERED BY PYLON FAIRING AND PYLONREINFORCING PLATE.OR78600 FHOR14300 FHPRE 48437572013-03-01 454BL 454BR 454CL454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY PYLON FAIRING,EXCLUDING AREA COVERED BY PYLON REINFORCING PLATEAND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.30900 FCOR140200 FH6400 FCOR29300 FHGROUP 32APRE 48437572013-03-02 454BL 454BR 454CL454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY PYLON FAIRING,EXCLUDING AREA COVERED BY PYLON REINFORCING PLATEAND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.26600 FCOR78500 FH6300 FCOR18700 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 83TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572013-03-03 454BL 454BR 454CL454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY PYLON FAIRING,EXCLUDING AREA COVERED BY PYLON REINFORCING PLATEAND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.34100 FCOR100900 FH7100 FCOR21100 FHGROUP 33CPRE 48437572013-03-04 454BL 454BR 454CL454CR 454DL 454DR454FL 454FR 454GL454GR 454HL 454HR464BL 464BR 464CL464CR 464DL 464DR464FL 464FR 464GL464GR 464HL 464HRDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREA COVERED BY PYLON FAIRING,EXCLUDING AREA COVERED BY PYLON REINFORCING PLATEAND AFT ATTACHMENT FITTING SKIN REINFORCING PLATE.31800 FCOR94000 FH6600 FCOR19600 FHGROUP 33DPRE 48437572014-02-02 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINTS AT SRINGER 13AND STRINGER 20 BETWEEN RIB 1 AND RIB 12 EXCLUDINGAREAS COVERED BY FAIRINGS.38000 FCOR112300 FH7900 FCOR23300 FHGROUP 33AORGROUP 33B572015-02-01 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1AND 12.26000 FCOR118100 FH6800 FCOR31200 FHGROUP 32APRE 48437572015-02-02 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1AND 12.32100 FCOR95000 FH6600 FCOR19600 FHGROUP 33AORGROUP 33B572015-02-03 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1AND 12.30600 FCOR90400 FH8100 FCOR23900 FHGROUP 33CPRE 48437572015-02-04 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE MLI HOLES AND DRAIN HOLES AFT OFFRONT SPAR AND FORWARD OF REAR SPAR, BETWEEN RIB 1AND 12.27000 FCOR79900 FH6900 FCOR20500 FHGROUP 33DPRE 48437572016-02-04 FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.23600 FCOR107100 FH3100 FCOR14200 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 84TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572016-02-05 FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.28300 FCOR83600 FH4600 FCOR13600 FHGROUP 33AORGROUP 33B572016-02-06 FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.26500 FCOR78300 FH3500 FCOR10400 FHGROUP 33CPRE 48437572016-02-07 FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.24100 FCOR71400 FH3200 FCOR9500 FHGROUP 33DPRE 48437N 572016-02-12 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN VISIBLE SURFACES OF FUEL PUMP APERTURESBETWEEN RIB 2 AND RIB 4.26900 FCOR80900 FH17000 FCOR50000 FHA330-200F572018-01-05 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.27100 FCOR123300 FH7100 FCOR32300 FHGROUP 32APRE 48437641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572018-01-06 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.29800 FCOR88200 FH7300 FCOR21700 FHGROUP 33AORGROUP 33B572018-01-07 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.39000 FCOR110800 FH10900 FCOR31000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572018-01-08 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.28700 FCOR81600 FH10900 FCOR31000 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 85TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572018-01-09 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.24400 FCOR109100 FH9300 FCOR41600 FHGROUP 32E572018-01-10 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.32900 FCOR148400 FH9200 FCOR41600 FHGROUP 32APOST 48437572018-01-11 541AB 541AZ 541BB541BZ 541CB 541CZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDING27900 FCOR7300 FCORGROUP 33DPRE 48437541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ,STRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.82300 FH 21600 FH572018-01-12 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 1 AND RIB 9, EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13 &20.29300 FCOR86500 FH7700 FCOR22700 FHGROUP 33CPRE 48437572019-01-05 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.27100 FCOR123300 FH5400 FCOR24900 FHGROUP 32APRE 48437572019-01-06 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.29800 FCOR88200 FH7300 FCOR21700 FHGROUP 33AORGROUP 33B572019-01-07 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.31600 FCOR89800 FH8100 FCOR23200 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 86TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572019-01-08 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.31600 FCOR89800 FH8200 FCOR23200 FHGROUP 33E572019-01-09 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.26800 FCOR120200 FH6900 FCOR31100 FHGROUP 32E572019-01-10 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.26700 FCOR120300 FH6900 FCOR31100 FHGROUP 32APOST 48437572019-01-11 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.27900 FCOR82300 FH5600 FCOR16600 FHGROUP 33DPRE 48437572019-01-12 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS 13 &20.29300 FCOR86500 FH5900 FCOR17500 FHGROUP 33CPRE 48437572021-03-02 454FL 454FR 454GL454GR 464FL 464FR464GL 464GR 531AB631ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13AND STRINGER 20 IN AREAS COVERED BY PYLON FAIRINGAND FLAP TRACK 2 FAIRING.37800 FCOR111600 FH10200 FCOR30300 FHGROUP 33AORGROUP 33BD 572022-01-04TASK DELETED IN ISSUE 17D 572022-01-05TASK DELETED IN ISSUE 17D 572022-01-06TASK DELETED IN ISSUE 17D 572022-01-07TASK DELETED IN ISSUE 17572023-02-03 N/ADETAILED INSPECTION OFOUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDINGGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.27100 FCOR123300 FH3600 FCOR16500 FHGROUP 32APRE 48437572023-02-04 N/ADETAILED INSPECTION OFOUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDINGGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.28500 FCOR84300 FH4000 FCOR12000 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 87TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572023-02-05 N/ADETAILED INSPECTION OFOUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDINGGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.29300 FCOR86500 FH3900 FCOR11600 FHGROUP 33CPRE 48437572023-02-06 N/ADETAILED INSPECTION OFOUTER WING BOTTOM SKIN ATSTRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB 10 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREAS COVEREDBY PYLON FAIRING AND REINFORCING PLATE, MAIN LANDINGGEAR REINFORCING PLATE AND FLAP TRACK 2 FAIRING.27900 FCOR82300 FH3700 FCOR11000 FHGROUP 33DPRE 48437572027-01-5 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEENRIB 1 AND RIB 9.36900 FCOR167600 FH6200 FCOR28300 FHGROUP 32APRE 48437541FZ641AB641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZ572027-01-06 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEENRIB 1 AND RIB 9.37200 FCOR110000 FH8600 FCOR25600 FHGROUP 33AORGROUP 33B572027-01-10 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEENRIB 1 AND RIB 9.38400 FCOR113600 FH6500 FCOR19200 FHGROUP 33DPRE 48437572029-01-03 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1AND RIB 12.18000 FCOR81600 FH12700 FCOR57700 FHGROUP 32APRE 48437572029-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1AND RIB 1222800 FCOR67700 FH16400 FCOR48900 FHGROUP 33AORGROUP 33BANDRIB12.67700FH48900FHGROUP33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 88TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572029-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1AND RIB 12.20000 FCOR59400 FH14100 FCOR42000 FHGROUP 33CPRE 48437572029-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR BETWEEN RIB 1AND RIB 12.19500 FCOR58000 FH13800 FCOR41000 FHGROUP 33DPRE 48437572030-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9AND RIB 11.21700 FCOR98500 FH14600 FCOR66200 FHGROUP 32APRE 48437572030-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9AND RIB 11.15600 FCOR46400 FH15600 FCOR46400 FHGROUP 33APRE 42550572030-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9AND RIB 11.18500 FCOR54900 FH16400 FCOR48900 FHGROUP 33APOST 42550ORGROUP 33B572030-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9AND RIB 11.23400 FCOR69700 FH15700 FCOR46800 FHGROUP 33CPRE 48437572030-01-08 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 9AND RIB 11.21300 FCOR63300 FH14300 FCOR42500 FHGROUP 33DPRE 48437R 572032-01-04 N/ADETAILEDINSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.33000 FCOR149400 FH11800 FCOR50000 FHGROUP 32APRE 48437572032-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.15900 FCOR47300 FH12000 FCOR35700 FHGROUP 33APOST 46110ORGROUP 33BPOST 46110572032-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.26400 FCOR78600 FH9500 FCOR28200 FHGROUP 33CPRE 48437572032-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.28600 FCOR81300 FH10000 FCOR28500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572032-01-08 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 128600 FCOR10000 FCORGROUP 33EAND RIB 7.81300 FH 28500 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 89TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572032-01-09 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.23700 FCOR104200 FH8300 FCOR36600 FHGROUP 32E572032-01-10 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.23600 FCOR104200 FH8300 FCOR36600 FHGROUP 32APOST 48437572032-01-11 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR BETWEEN RIB 1AND RIB 7.24000 FCOR71300 FH8600 FCOR25600 FHGROUP 33DPRE 48437572033-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TOREAR SPAR.38200 FCOR173300 FH6600 FCOR30100 FHGROUP 32APRE 48437572033-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TOREAR SPAR.27700 FCOR82400 FH8600 FCOR25500 FHGROUP 33AORGROUP 33B572033-01-06 N/ADETAILED INSPECTIONOF OUTER WING TOP SKIN UPPER 38200 FC 6600 FC GROUP 33CSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TOREAR SPAR.OR113400 FHOR19700 FHPRE 48437572033-01-07 N/A DETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 1 AND RIB 12 FROM FRONT SPAR TOREAR SPAR.34600 FCOR102900 FH6000 FCOR17800 FHGROUP 33DPRE 48437572034-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENRIB 1 AND RIB 18, EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11AND 13.16300 FCOR74000 FH10900 FCOR49700 FHGROUP 32APRE 48437572034-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENRIB 1 AND RIB 18, EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11AND 13.13600 FCOR40400 FH9100 FCOR27100 FHGROUP 33AORGROUP 33B572034-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENRIB 1 AND RIB 18, EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 11AND 13.17000 FCOR50700 FH11400 FCOR34000 FHGROUP 33CPRE 48437572034-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINTS AT STRINGERS 12 AND 19 BETWEENRIB 1 AND RIB 18, EXCLUDING STRINGERS 12 AND 19BETWEEN RIBS 4 AND 8 AND STRINGER 19 BETWEEN RIBS 1115400 FCOR46000 FH10400 FCOR30900 FHGROUP 33DPRE 48437AND 13.ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 90TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572035-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB8.14900 FCOR67500 FH12300 FCOR55900 FHGROUP 32APRE 48437572035-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB8.13700 FCOR40700 FH10900 FCOR32600 FHGROUP 33AORGROUP 33B572035-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB8.14600 FCOR43500 FH12100 FCOR36100 FHGROUP 33CPRE 48437572035-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE FROM STRINGER 12 TO 19 AND FROM RIB 4 TO RIB8.13300 FCOR39500 FH11000 FCOR32700 FHGROUP 33DPRE 48437572036-01-04 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERCROWN FITTINGS AT ROOT JOINT FROM FRONT TO REARSPARS.22100 FCOR100100 FH8800 FCOR40100 FHGROUP 32APRE 48437572036-01-05 541AB 541AZ 541BZ DETAILED INSPECTION OF OUTER WING TOP SKIN STRINGER 26500 FC 12700 FC GROUP 33A641AB 641AZ 641BZ CROWN FITTINGS AT ROOT JOINT FROM FRONT TO REARSPARS.OR78700 FHOR37700 FHORGROUP 33B572036-01-06 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERCROWN FITTINGS AT ROOT JOINT FROM FRONT TO REARSPARS.23500 FCOR69800 FH9400 FCOR27900 FHGROUP 33CPRE 48437572036-01-07 541AB 541AZ 541BZ641AB 641AZ 641BZDETAILED INSPECTION OF OUTER WING TOP SKIN STRINGERCROWN FITTINGS AT ROOT JOINT FROM FRONT TO REARSPARS.21300 FCOR63300 FH8300 FCOR24700 FHGROUP 33DPRE 48437R 572039-01-04 N/A DETAILEDINSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9AND FROM RIB 11 TO 12.33400 FCOR151300 FH14600 FCOR50000 FHGROUP 32APRE 48437572039-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9AND FROM RIB 11 TO 12.36300 FCOR108000 FH16400 FCOR48900 FHGROUP 33AORGROUP 33B572039-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9AND FROM RIB 11 TO 12.37200 FCOR110500 FH16300 FCOR48500 FHGROUP 33CPRE 48437572039-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO REAR SPAR, FROM RIB 7 TO 9AND FROM RIB 11 TO 12.33700 FCOR100300 FH14800 FCOR44000 FHGROUP 33DPRE 48437R 572040-01-04 N/ADETAILEDINSPECTION OF OUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 ANDRIB 13.28600 FCOR129400 FH13500 FCOR50000 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 91TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572040-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 ANDRIB 13.30200 FCOR89700 FH11000 FCOR32900 FHGROUP 33AORGROUP 33B572040-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 ANDRIB 13.33800 FCOR100600 FH16100 FCOR47800 FHGROUP 33CPRE 48437572040-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE SKIN JOINT AT STRINGER 19 BETWEEN RIB 11 ANDRIB 13.31800 FCOR94500 FH15100 FCOR44900 FHGROUP 33DPRE 48437572043-01-04 573FB 673FBDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 9.31500 FCOR145000 FH10300 FCOR47600 FHGROUP 32APRE 48437572043-01-05 573FB 673FBDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 9.24800 FCOR79400 FH5800 FCOR18500 FHGROUP 33AORGROUP 33B572043-01-06 573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPAR AFT 33900 FC 11100 FC GROUP 33CFACE SPAR JOINT PLATE AT RIB 9.OR108500 FHOR35600 FHPRE 48437572043-01-07 573FB 673FBDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 9.28600 FCOR91400 FH9400 FCOR30000 FHGROUP 33DPRE 48437572046-01-04 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.22900 FCOR105500 FH5400 FCOR24900 FHGROUP 32APRE 48437572046-01-05 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.16900 FCOR54000 FH9900 FCOR31800 FCGROUP 33APOST 46111572046-01-06 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.19600 FCOR62700 FH9600 FCOR30600 FHGROUP 33B572046-01-07 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.26400 FCOR82700 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 92TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572046-01-08 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.26400 FCOR82700 FH8000 FCOR25100 FHGROUP 33E572046-01-09 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.22700 FCOR133400 FH6900 FCOR40600 FHGROUP 32E572046-01-10 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.22700 FCOR133600 FH18400 FCOR108200 FHGROUP 32APOST 48437572046-01-11 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.20100 FCOR64400 FH4700 FCOR15200 FHGROUP 33DPRE 48437572046-01-12 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.23900 FCOR76500 FH5600 FCOR18100 FHGROUP 33CPRE 48437N 572046-01-13 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11 INCLUDING TOPAND BOTTOM FLANGE.22200 FCOR66800 FH10400 FCOR31400 FHA330-200F572047-01-03 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.18400 FCOR84900 FH18400 FCOR84900 FHGROUP 32APRE 48437572047-01-04 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.22600 FCOR72400 FH20000 FCOR50000 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 93TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572047-01-05 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.19200 FCOR61300 FH19200 FCOR61300 FHGROUP 33CPRE 48437572047-01-06 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.30400 FCOR95200 FH12000 FCOR37700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572047-01-07 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKET32600 FCOR102200 FH12000 FCOR37300 FHGROUP 33ESEALANT REMOVAL ASPER NTM.)BETWEEN RIB 1 AND RIB 7.R 572047-01-08 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.28000 FCOR164900 FH10300 FCOR50000 FHGROUP 32ER 572047-01-09 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.26200 FCOR153700 FH10300 FCOR50000 FHGROUP 32APOST 48437572047-01-10 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE AT MLG FITTINGS (GEAR RIB 6, FORWARDPINTLE FITTING, RETRACTION JACK FITTING AND SIDESTAYFITTING) BOLTING AREAS AND TOP ANGLE BRACKETBETWEEN RIB 1 AND RIB 7.18300 FCOR58700 FH18300 FCOR58700 FHGROUP 33DPRE 48437R 572048-01-01 541DB 541EB641DB 641EBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.31500 FCOR145000 FH10300 FCOR47600 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 94TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 572048-01-02 541DB 541EB641DB 641EBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.24800 FCOR79400 FH5800 FCOR18500 FHGROUP 33AORGROUP 33BR 572048-01-03 541DB 541EB641DB 641EBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.33900 FCOR108500 FH11100 FCOR35600 FHGROUP 33CPRE 48437R 572048-01-04 541DB 541EB641DB 641EBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE SPAR JOINT BOLTING AREA OF RIB 9.28600 FCOR91400 FH9400 FCOR30000 FHGROUP 33DPRE 48437R 572049-01-04 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARUPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.31500 FCOR145000 FH15500 FCOR50000 FHGROUP 32APRE 48437572049-01-05 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARUPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.24800 FCOR79400 FH8700 FCOR27800 FHGROUP 33AORGROUP 33BR 572049-01-06 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPAR 33900 FC 16700 FC GROUP 33CUPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.OR108500 FHOR50000 FHPRE 48437572049-01-07 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARUPPER AND LOWER FLANGE JOINT STRAPS AT RIB 9.28600 FCOR91400 FH14100 FCOR45000 FHGROUP 33DPRE 48437572050-01-04 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 ANDLOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.20900 FCOR96500 FH6300 FCOR29100 FHGROUP 32APRE 48437572050-01-05 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 ANDLOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.16000 FCOR51200 FH7200 FCOR23200 FHGROUP 33APRE 48437572050-01-06 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 ANDLOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.25100 FCOR80200 FH7200 FCOR23200 FHGROUP 33BPRE 48437572050-01-07 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 ANDLOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.23200 FCOR74300 FH7000 FCOR22400 FHGROUP 33CPRE 48437572050-01-08 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPAR AFTFACE UPPER ATTACHMENT ANGLE FROM RIB 4 TO RIB 7 ANDLOWER ATTACHMENT ANGLE FROM RIB 1 TO RIB 7.22900 FCOR73200 FH6900 FCOR22100 FHGROUP 33DPRE 48437572051-01-05 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT BUILD SLOT BETWEEN RIBS 1 & 2.17200 FCOR79300 FH5300 FCOR24600 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 95TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572051-01-06 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT BUILD SLOT BETWEEN RIBS 1 & 2.32600 FCOR104200 FH5200 FCOR16600 FHGROUP 33APOST 46241ORGROUP 33BPOST 46241572051-01-07 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT BUILD SLOT BETWEEN RIBS 1 & 2.15800 FCOR50400 FH5200 FCOR16600 FHGROUP 33APOST 42547ORGROUP 33BPOST 42547572051-01-08 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT BUILD SLOT BETWEEN RIBS 1 & 2.17800 FCOR57000 FH5500 FCOR17700 FHGROUP 33CPRE 48437572051-01-09 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAT BUILD SLOT BETWEEN RIBS 1 & 2.16900 FCOR54000 FH5200 FCOR16800 FHGROUP 33DPRE 48437572052-03-01 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.20900 FCOR96500 FH9500 FCOR43700 FHGROUP 32APRE 48437572052-03-02 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.16000 FCOR51200 FH7700 FCOR24600 FHGROUP 33APOST 46110ORGROUP 33BPRE 43503POST 46110572052-03-04 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.25100 FCOR80200 FH7700 FCOR24600 FHGROUP 33BPOST 43503572052-03-05 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.22900 FCOR73200 FH10300 FCOR33200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572052-03-06 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.23600 FCOR73900 FH9200 FCOR28700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 96TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572052-03-07 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.23600 FCOR73900 FH9200 FCOR28700 FHGROUP 33E572052-03-08 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.20300 FCOR119200 FH7900 FCOR46400 FHGROUP 32E572052-03-09 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.20300 FCOR119300 FH7900 FCOR46400 FHGROUP 32APOST 48437N 572052-03-10 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 1 AND RIB 7 INCLUDING TOPAND BOTTOM FLANGE.27500 FCOR82500 FH17000 FCOR50000 FHA330-200F572054-01-05 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.20900 FCOR96400 FH5000 FCOR23300 FHGROUP 32APRE 48437572054-01-06 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.14700 FCOR47000 FH4400 FCOR14100 FHGROUP 33APRE 43503PRE 46141ORGROUP 33BPRE 43503PRE 46141572054-01-08 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.28200 FCOR88400 FH8600 FCOR27000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572054-01-09 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.28200 FCOR88400 FH8600 FCOR27000 FHGROUP 33E572054-01-10 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.24300 FCOR142700 FH7400 FCOR43600 FHGROUP 32E572054-01-11 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.14800 FCOR47200 FH3500 FCOR11400 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 97TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572054-01-12 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.24300 FCOR142800 FH7400 FCOR43600 FHGROUP 32APOST 48437572054-01-13 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.30400 FCOR97100 FH4400 FCOR14100 FHGROUP 33APOST 46141ORGROUP 33BPOST 46141572054-01-14 DEPLOY FLAPSSPECIALDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.17500 FCOR56100 FH4200 FCOR13500 FHGROUP 33CPRE 48437N 572054-01-15 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SYSTEMS HOLE BETWEEN RIBS 4 & 5.26800 FCOR80400 FH8300 FCOR25100 FHA330-200F572063-01-05 541AB 541BB 541CB541DB 541EB 541FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND34700 FCOR5500 FCORGROUP 32APRE 48437641AB 641BB 641CB641DB 641EB 641FB12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.159900 FH 25600 FH572063-01-06 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.27000 FCOR86400 FH6600 FCOR21300 FHGROUP 33AORGROUP 33B572063-01-07 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.38600 FCOR123500 FH6100 FCOR19700 FHGROUP 33CPRE 48437572063-01-08 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.36000 FCOR115100 FH5700 FCOR18400 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 98TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572063-01-10 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.32600 FCOR191500 FH7300 FCOR43000 FHGROUP 32APOST 48437572063-01-11 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 1 AND RIB 8 AND BETWEEN RIB 10 AND12 INCLUDING TOP AND BOTTOM FLANGES, BOLTING OFFORWARD PYLON ATTACHMENT FITTINGS IN REGION OF RIBBAY 10-10A AND SPAR JOINT BOLTING INBOARD OF RIB 12.37800 FCOR118500 FH8500 FCOR26600 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572064-01-05 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.25200 FCOR116000 FH6900 FCOR31700 FHGROUP 32APRE 48437572064-01-06 541EB 641EBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFT 13300 FC 6600 FC GROUP 33AFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.OR42700 FHOR21300 FHORGROUP 33B572064-01-07 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.30500 FCOR95600 FH8500 FCOR26000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572064-01-08 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.30500 FCOR95600 FH10000 FCOR31300 FHGROUP 33E572064-01-09 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.26200 FCOR154100 FH8600 FCOR43400 FHGROUP 32E572064-01-10 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.26300 FCOR154400 FH7300 FCOR43000 FHGROUP 32APOST 48437572064-01-11 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.19700 FCOR63100 FH5400 FCOR17300 FHGROUP 33DPRE 48437572064-01-12 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP ANDBOTTOM FLANGES.23400 FCOR74900 FH6400 FCOR20500 FHGROUP 33CPRE 48437N 572064-01-13 541EB 641EBDETAILED INSPECTIONOF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOP AND24800 FCOR7300 FCORA330-200FBOTTOM FLANGES.74500 FH 22100 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 99TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572065-01-04 522DB 522EB 622DB622EBDETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE AND SPAR JOINT PLATE AT RIB 12.34100 FCOR109100 FH14600 FCOR46800 FHGROUP 33AORGROUP 33B572066-01-05 N/ASPECIAL DETAILED INSPECTION OF OUTER WING FRONTSPAR UPPER AND LOWER FLANGE JOINT STRAPS AT RIB 12.32100 FCOR102800 FH14600 FCOR46800 FHGROUP 33AORGROUP 33B572067-01-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6 FORWARD ANDAFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDINGCLEATS, SPAR ATTACHMENTS, REGION OF STRINGERCUTOUTS AND ACCESS CUTOUT SURROUNDS.37800 FCOR107500 FH8100 FCOR23000 FHGROUP 33APRE 41114R 572067-01-06 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6 FORWARD ANDAFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDINGCLEATS, SPAR ATTACHMENTS, REGION OF STRINGERCUTOUTS AND ACCESS CUTOUT SURROUNDS.21100 FCOR60000 FH6200 FCOR17600 FHGROUP 33APOST 41114PRE 54219PRE 53883ORGROUP 33BPRE 54219PRE 53883N 572067-01-15 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6 FORWARD ANDAFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDINGCLEATS, SPAR ATTACHMENTS, REGION OF STRINGERCUTOUTS AND ACCESS CUTOUT SURROUNDS.21100 FCOR60000 FH4900 FCOR13900 FHGROUP 33APOST 41114POST 54219ORPOST 53883ORGROUP 33BPOST 54219ORPOST 53883572068-01-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7 FORWARD ANDAFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDINGCLEATS, SPAR ATTACHMENTS, REGION OF STRINGERCUTOUTS AND ACCESS CUTOUT SURROUNDS.9100 FCOR26000 FH6800 FCOR19400 FHGROUP 33A572068-01-06 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7 FORWARD ANDAFT OF CENTER SPAR AT SKIN ATTACHMENTS INCLUDINGCLEATS, SPAR ATTACHMENTS, REGION OF STRINGERCUTOUTS AND ACCESS CUTOUT SURROUNDS.18000 FCOR51100 FH5000 FCOR14300 FHGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 100TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572069-01-04 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.39400 FCOR175300 FH20000 FCOR50000 FHGROUP 32APRE 48437572069-01-05 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.29700 FCOR84500 FH6700 FCOR19000 FHGROUP 33A572069-01-06 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.29700 FCOR84500 FH6100 FCOR17400 FHGROUP 33B572069-01-08 541DB 541FZ 641DB DETAILED INSPECTION OF OUTER WING RIBS 8 AND 934200 FC 20000 FC GROUP 33D641FZFORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.OR97100 FHOR50000 FHPRE 48437R 572069-01-11 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.38300 FCOR120100 FH17100 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437R 572069-01-12 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS AND ACCESS CUTOUTSURROUNDS.33000 FCOR194000 FH14700 FCOR50000 FHGROUP 32APOST 48437572071-01-06 541AB 541AZ 541BB541BZ 541CZ 541DZ541EZ 641AB 641AZ641BB 641BZ 641CZ641DZ 641EZDETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKINATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS, ACCESS CUTOUTSURROUNDS AND AREA OF MANHOLE BOLTING.32000 FCOR91100 FH20000 FCOR50000 FHGROUP 33CPRE 48437572071-01-07 541AB 541AZ 541BB541BZ 541CZ 541DZ541EZ 641AB 641AZ641BB 641BZ 641CZ641DZ 641EZDETAILED INSPECTION OF OUTER WING RIBS, RIBS 2,3,4 AND5 (FORWARD AND AFT OF CENTER SPAR) AND RIB 2A AT SKINATTACHMENTS (INCLUDING CLEATS), SPAR ATTACHMENTS,REGION OF STRINGER CUTOUTS, ACCESS CUTOUTSURROUNDS AND AREA OF MANHOLE BOLTING.33900 FCOR96200 FH20000 FCOR50000 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 101TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572073-01-05 541FB 541GB 641FB641GBDETAILED INSPECTION OF OUTER WING RIBS, RIB 10 AFT, RIB11 FORWARD AND AFT, AND RIB 12 AT SKIN ATTACHMENTS(INCLUDING CLEATS), SPAR ATTACHMENTS, REGION OFSTRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.32900 FCOR93600 FH6400 FCOR18200 FHGROUP 33AORGROUP 33B572081-01-05 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.21300 FCOR98300 FH10300 FCOR47700 FHGROUP 32APRE 48437POST 43021572081-01-06 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.17600 FCOR56400 FH6900 FCOR22200 FHGROUP 33APOST 43272572081-01-07 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.20900 FCOR67000 FH6900 FCOR22200 FHGROUP 33APOST 43021ORGROUP 33BPOST 43021572081-01-08 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.22400 FCOR71700 FH10900 FCOR34800 FHGROUP 33CPRE 48437POST 43021572081-01-10 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.21500 FCOR68900 FH10400 FCOR33500 FHGROUP 33DPRE 48437572081-01-14 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.34400 FCOR202200 FH7100 FCOR41800 FHGROUP 32APOST 48437N 572081-01-15 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB 2.30100 FCOR90400 FH17000 FCOR50000 FHA330-200F572082-01-05 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.22400 FCOR103200 FH5100 FCOR23700 FHGROUP 32APRE 48437POST 42550ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 102TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572082-01-06 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.29400 FCOR94000 FH8400 FCOR26900 FHGROUP 33APOST 40366POST 42275572082-01-07 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.28400 FCOR90800 FH8400 FCOR26900 FHGROUP 33BPOST 42550572082-01-08 541AB 541AZ 541BB541CB 541DB 541DZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES28100 FCOR20000 FCORGROUP 33CPOST 48437541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.88000 FH 50000 FH ORGROUP 33DPOST 48437R 572082-01-09 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.28100 FCOR88000 FH17000 FCOR50000 FHGROUP 33ER 572082-01-10 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.24100 FCOR142000 FH17000 FCOR50000 FHGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 103TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572082-01-11 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.24200 FCOR142100 FH20000 FCOR50000 FHGROUP 32APOST 48437572082-01-12 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.17900 FCOR57300 FH4100 FCOR12400 FHGROUP 33DPRE 48437572082-01-13 541AB 541AZ 541BB541CB 541DB 541DZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACES21200 FCOR4900 FCORGROUP 33CPRE 48437541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.67900 FH 15600 FH POST 42550N 572082-01-14 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS, AREAAROUND ACCESS HOLES, DRAIN AND VENT HOLES ANDCONDUIT HOLES.19100 FCOR57400 FH4900 FCOR14700 FHA330-200F572084-01-01 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR.11, STR. 14, STR. 18 TO 20AND AT STR. 23 TO 28 LH/RH.30700 FCOR89000 FH9900 FCOR29700 FHGROUP 33APRE 41652ORGROUP 33BPRE 41652572084-01-03 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR.11, STR. 14, STR. 18 TO 20AND AT STR. 23 TO 28 LH/RH.22700 FCOR100000 FH11400 FCOR56100 FHGROUP 32AORGROUP 33C572084-01-04 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR.11, STR. 14, STR. 18 TO 2024700 FCOR74100 FH12500 FCOR37500 FHGROUP 33EAND AT STR. 23 TO 28 LH/RH.ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 104TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572084-01-05 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR.11, STR. 14, STR. 18 TO 20AND AT STR. 23 TO 28 LH/RH.20600 FCOR103000 FH11000 FCOR54900 FHGROUP 32E572084-01-06 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA AT STR.11, STR. 14, STR. 18 TO 20AND AT STR. 23 TO 28 LH/RH.22000 FCOR97200 FH11200 FCOR54900 FHGROUP 33DN 572084-01-07 541 AB, 641 AB,SEALANT REMOVAL AS PERNTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTING OUTBOARDFLANGE IN RADIUS AREA ATSTR.11, STR.14, STR.18 TO 20AND AT STR.23 TO 28, LH/RH.24500 FC 12600 FC A330-200F572090-01-01 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.28300 FCOR128700 FH5200 FCOR23600 FHGROUP 32APRE 48437NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-02-01572090-01-03 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-02-0331000 FCOR91700 FH5700 FCOR16800 FHGROUP 33CPRE 48437572090-01-04 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-02-0429600 FCOR87500 FH5400 FCOR16100 FHGROUP 33DPRE 48437R 572090-02-01 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-01-0128300 FCOR128700 FH12800 FCOR50000 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 105TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572090-02-03 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-01-0331000 FCOR91700 FH14000 FCOR41500 FHGROUP 33CPRE 48437572090-02-04 N/ASPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE AT ATTACHMENT TO FRONT SPARBETWEEN RIB 8 AND RIB 9.NOTE: THIS TASK IS ANALTERNATIVE TOTASK572090-01-0429600 FCOR87500 FH13400 FCOR39600 FHGROUP 33DPRE 48437572093-01-06 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME29100 FCOR132200 FH5900 FCOR26800 FHGROUP 32APRE 48437AS TASK 572093-02-06.572093-01-07 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-02-0739200 FCOR116000 FH6300 FCOR18800 FHGROUP 33AORGROUP 33B572093-01-09 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-02-09.32400 FCOR85700 FH6500 FCOR19400 FHGROUP 33CPRE 48437572093-01-10 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-02-10.30200 FCOR89400 FH6100 FCOR18100 FHGROUP 33DPRE 48437572093-01-13 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-02-1338600 FCOR109800 FH8000 FCOR22700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 106TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572093-01-14 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKIN JOINTOF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-02-1432600 FCOR147000 FH6700 FCOR30300 FHGROUP 32APOST 48437572093-02-06 541FB 641FBSEALANT REMOVAL AS PERNTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-06.29100 FCOR132200 FH5900 FCOR26800 FHGROUP 32APRE 48437572093-02-07 541FB 641FBSEALANT REMOVAL AS PERNTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-0739200 FCOR116000 FH6300 FCOR18800 FHGROUP 33AORGROUP 33B572093-02-09 541FB 641FBSPECIAL DETAILED INSPECTIONOF OUTER WING BOTTOM 32400 FC 6500 FC GROUP 33CSEALANT REMOVAL AS PERNTMSKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-09.OR95700 FHOR19400 FHPRE 48437572093-02-10 541FB 641FBSEALANT REMOVAL AS PERNTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-10.30200 FCOR89400 FH6100 FCOR18100 FHGROUP 33DPRE 48437572093-02-13 541FB 641FBSEALANT REMOVAL AS PERNTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-1438600 FCOR109800 FH8000 FCOR22700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572093-02-14 541FB 641FBSEALANT REMOVAL AS PERNTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN JOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572093-01-1332600 FCOR147000 FH6700 FCOR30300 FHGROUP 32APOST 48437572094-01-05 541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEENRIB 9 AND RIB 12.36900 FCOR167600 FH6200 FCOR28300 FHGROUP 32APRE 48437572094-01-06 541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEEN32700 FCOR8600 FCORGROUP 33AORRIB 9 AND RIB 12.96600 FH 25600 FH GROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 107TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572094-01-10 541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 & STRINGER 20 BETWEENRIB 9 AND RIB 12.38400 FCOR113600 FH6500 FCOR19200 FHGROUP 33DPRE 48437572095-01-05 541BB 541CB 641BB641CB.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.27100 FCOR123300 FH6900 FCOR31500 FHGROUP 32APRE 48437572095-01-06 541BB 541CB 641BB641CB.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.29800 FCOR88200 FH7300 FCOR21700 FHGROUP 33AORGROUP 33B572095-01-07 541BB 541CB 641BB641CB.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.29300 FCOR86500 FH7500 FCOR22100 FHGROUP 33CPRE 48437572095-01-08 541BB 541CB 641BB641CB.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 BETWEEN RIB 5 AND RIB 7.27900 FCOR82300 FH7100 FCOR21100 FHGROUP 33DPRE 48437572101-01-04 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKIN 32400 FC 5600 FC GROUP 32ALOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.OR147400 FHOR25500 FHPRE 48437572101-01-06 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.36900 FCOR108900 FH6300 FCOR18800 FHGROUP 33CPRE 48437572101-01-07 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 12 AND RIB 26, EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.33400 FCOR98600 FH5500 FCOR16300 FHGROUP 33DPRE 48437572104-01-04 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREASCOVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS ATRIB 27 AND RIB 39.32400 FCOR147400 FH5600 FCOR25500 FHGROUP 32APRE 48437572104-01-05 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREASCOVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS ATRIB 27 AND RIB 39.32600 FCOR96400 FH6800 FCOR20200 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 108TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572104-01-06 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREASCOVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS ATRIB 27 AND RIB 39.36900 FCOR108900 FH6300 FCOR18800 FHGROUP 33CPRE 48437572104-01-07 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO FRONT SPAR ANDREAR SPAR BETWEEN RIB 26 AND RIB 39, EXCLUDING AREASCOVERED BY FLAP TRACK 5 FAIRING AND SKIN JOINTS ATRIB 27 AND RIB 39.33400 FCOR98600 FH5500 FCOR16300 FHGROUP 33DPRE 48437572108-02-04 532AB 533AB 534AB541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND27.36500 FCOR165900 FH6600 FCOR30000 FHGROUP 32APRE 48437632AB 633AB 634AB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572108-02-06 532AB 533AB 534AB541GB 541HB 541JB541KB 541MB 541NB541PB 541QB 541RB541SB 542AB 542BB542CB 542DB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND27.39500 FCOR116700 FH7100 FCOR21100 FHGROUP 33CPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 109TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572108-02-07 532AB 533AB 534AB541GB 541HB 541JB541KB 541MB 541NB541PB 541QB 541RB541SB 542AB 542BB542CB 542DB 632AB633AB 634AB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER MATING SURFACES AROUNDACCESS DOOR CUTOUTS IN ALL BAYS BETWEEN RIBS 12 AND27.38500 FCOR113800 FH6900 FCOR20600 FHGROUP 33DPRE 48437572109-02-05 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN UPPER AND LOWER SURFACES AROUND ACCESS DOORCUTOUTS, INCLUDING NACA DUCT, IN ALL BAYS BETWEENRIBS 27 AND 39.32800 FCOR96800 FH10200 FCOR30300 FHGROUP 33AORGROUP 33B642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FB572110-01-04 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONTSPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRINGS 3, 4 AND 5.22200 FCOR101000 FH9400 FCOR43000 FHGROUP 32APRE 48437572110-01-05 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONTSPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRINGS 3, 4 AND 5.22300 FCOR66000 FH10000 FCOR29700 FHGROUP 33AORGROUP 33B572110-01-06 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONTSPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRINGS 3, 4 AND 5.25000 FCOR74000 FH10600 FCOR31500 FHGROUP 33CPRE 48437572110-01-07 N/ADETAILEDINSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROM FRONTSPAR TO REAR SPAR EXCLUDING AREAS COVERED BY FLAPTRACK FAIRINGS 3, 4 AND 5.23200 FCOR68500 FH9800 FCOR29100 FHGROUP 33DPRE 48437572111-01-04 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4 AND 5.22200 FCOR101000 FH8200 FCOR37400 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 110TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572111-01-05 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4 AND 5.22300 FCOR66000 FH10000 FCOR29700 FHGROUP 33AORGROUP 33B572111-01-06 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4 AND 5.25000 FCOR74000 FH9200 FCOR27400 FHGROUP 33CPRE 48437572111-01-07 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4 AND 5.23200 FCOR68500 FH8600 FCOR25300 FHGROUP 33DPRE 48437572116-02-02 N/AGENERAL VISUAL INSPECTION OF OUTER WING BOTTOMSKIN LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER13 AND STRINGER 20 BETWEEN RIB 12 AND RIB 27EXCLUDING AREAS COVERED BY FLAP TRACK FAIRINGS 3, 437800 FCOR111600 FH7200 FCOR21400 FHGROUP 33AORGROUP 33B,& 5.572117-01-05 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBFAIRING ATTMT BRACKET.DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINT AT STRINGER 13AND STRINGER 20 COVERED BY FLAP TRACK FAIRINGS 3, 4AND 5.37800 FCOR111600 FH8400 FCOR25000 FHGROUP 33AORGROUP 33BN 572119-02-10 N/A DETAILED INSPECTIONOF OUTER WING BOTTOM SKINLOWER SURFACE AT DRAIN HOLES FOR SLAT CANS, MLIHOLES AND DRAIN HOLES AFT OF FRONT SPAR ANDFORWARD OF REAR SPAR, BETWEEN RIBS 12 AND 23.27300 FCOR81900 FH13200 FCOR39600 FHA330-200F572121-01-04 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.21900 FCOR99700 FH4800 FCOR22000 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 111TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572121-01-05 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.22800 FCOR67600 FH4600 FCOR13800 FHGROUP 33AORGROUP 33B572121-01-06 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.35400 FCOR100600 FH8300 FCOR23600 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572121-01-07 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.21800 FCOR64400 FH4800 FCOR14200 FHGROUP 33DPRE 48437572121-01-08 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.29900 FCOR134700 FH7000 FCOR31600 FHGROUP 32APOST 48437572121-01-09 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 12 AND RIB 23 EXCLUDINGSTRINGERS 15 AND 18 AND BUTTSTRAPS AT STRINGERS 13AND 20.24600 FCOR72900 FH5400 FCOR16100 FHGROUP 33CPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 112TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572122-01-04 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY26-28 AND STRINGERS 15 & 18.21900 FCOR99700 FH4700 FCOR21600 FHGROUP 32APRE 48437572122-01-05 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650ABDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY26-28 AND STRINGERS 15 & 18.22800 FCOR67600 FH6900 FCOR20400 FHGROUP 33AORGROUP 33B650BB 650CB 650DB650EB 650FB572122-01-06 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY26-28 AND STRINGERS 15 & 18.24600 FCOR72900 FH5300 FCOR15800 FHGROUP 33CPRE 48437572122-01-07 542AB 542BB 542CB542FB 542GB 542HB542JB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642FB 642GB642HB 642JB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 EXCLUDING RIB BAY26-28 AND STRINGERS 15 & 18.22900 FCOR67700 FH4900 FCOR14600 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 113TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572125-01-06 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDINGJOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-02-04.27600 FCOR125600 FH9900 FCOR45200 FHGROUP 32APRE 48437572125-01-07 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDINGJOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-02-05.34700 FCOR102700 FH13000 FCOR38500 FHGROUP 33AORGROUP 33B572125-01-08 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDINGJOINTS ON STRINGERS 15 AND 18.31300 FCOR92500 FH11200 FCOR33200 FHGROUP 33CPRE 48437NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-02-06.572125-01-09 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28 EXCLUDINGJOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-02-07.28300 FCOR83700 FH10200 FCOR30100 FHGROUP 33DPRE 48437572125-02-04 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-01-06.27600 FCOR125600 FH9900 FCOR45200 FHGROUP 32APRE 48437572125-02-05 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-01-07.34700 FCOR102700 FH13000 FCOR38500 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 114TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572125-02-06 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-01-08.31300 FCOR92500 FH11200 FCOR33200 FHGROUP 33CPRE 48437572125-02-07 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572125-01-09.28300 FCOR83700 FH10200 FCOR30100 FHGROUP 33DPRE 48437572129-01-03 541SB 641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIME22800 FCOR67600 FH5600 FCOR16600 FHGROUP 33APRE 44245ORGROUP 33BAS TASK 572129-02-03.PRE 44245572129-02-03 541SB 641SBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572129-01-03.22800 FCOR67600 FH5600 FCOR16600 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245572130-01-03 542AB 642AB DETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572130-02-03.22800 FCOR67600 FH6900 FCOR20400 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245572130-02-03 542AB 642ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 19 JOINT BETWEEN RIB 23 AND RIB 24.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572130-01-03.22800 FCOR67600 FH6900 FCOR20400 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245R 572131-01-04 N/ADETAILEDINSPECTION OF OUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPARBETWEEN RIB 12 AND RIB 27.29600 FCOR134300 FH13600 FCOR50000 FHGROUP 32APRE 48437572131-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPARBETWEEN RIB 12 AND RIB 27.33000 FCOR98000 FH16400 FCOR48900 FHGROUP 33AORGROUP 33B572131-01-06 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR34500 FCOR15800 FCORGROUP 33CPRE 48437BETWEEN RIB 12 AND RIB 27.102700 FH 47100 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 115TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572131-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPARBETWEEN RIB 12 AND RIB 27.32700 FCOR97300 FH15000 FCOR44600 FHGROUP 33DPRE 48437572133-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.35000 FCOR158400 FH5800 FCOR26300 FHGROUP 32APRE 48437572133-01-05 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.34800 FCOR103400 FH8900 FCOR26600 FHGROUP 33AORGROUP 33B572133-01-07 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN UPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONT SPARTO REAR SPAR.37600 FCOR111600 FH6200 FCOR18500 FHGROUP 33DPRE 48437572138-01-05 N/AGENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKINJOINT AREA.31200 FCOR92600 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B572138-01-07 N/AGENERAL VISUAL INSPECTION OF OUTER WING TOP SKIN 34700 FC 20000 FC GROUP 33DUPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKINJOINT AREA.OR103200 FHOR50000 FHPRE 48437572138-01-09 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKINJOINT AREA.31700 FCOR143700 FH20000 FCOR50000 FHGROUP 32APRE 48437572138-01-10 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE IN REGION OF RIB 27 CHORDWISE SKINJOINT AREA.37600 FCOR111700 FH20000 FCOR50000 FHGROUP 33CPRE 48437572139-01-05 N/A GENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.31200 FCOR92600 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B572139-01-07 N/AGENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.34700 FCOR103200 FH20000 FCOR50000 FHGROUP 33DPRE 48437572139-01-09 N/AGENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.31700 FCOR143700 FH20000 FCOR50000 FHGROUP 32APRE 48437572139-01-10 N/AGENERAL VISUAL INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT RIB 39 CHORDWISE SKIN JOINT AREA.37600 FCOR111700 FH20000 FCOR50000 FHGROUP 33CPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 116TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572140-01-04 541EB 541FB 541GB541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDINGBUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.36900 FCOR167000 FH8700 FCOR39600 FHGROUP 32APRE 48437572140-01-05 541EB 541FB 541GB541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDINGBUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.36900 FCOR109800 FH8900 FCOR26400 FHGROUP 33AORGROUP 33B641NB 641PB 641QB641RB 641SBN 572140-01-10 541EB 541FB 541GB541HB 541JB 541KB541LB 541MB 541NB541PB 541QB 541RB541SB 641EB 641FB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 9 AND RIB 23 INCLUDINGBUTTSTRAPS AT STR 12 AND 19 AND ALL STRINGER JOINTS.30200 FCOR90800 FH17000 FCOR50000 FHA330-200F572141-01-04 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUTIN RIB BAY 23-24.36000 FCOR163200 FH10000 FCOR45300 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 117TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572141-01-05 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EB550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUTIN RIB BAY 23-24.33600 FCOR99800 FH12600 FCOR37600 FHGROUP 33AORGROUP 33B572141-01-08 542AB 542BB 542CB542DB 542EB 542FB542GB 542HB 542JB542KB 550AB 550BB550CB 550DB 550EBDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGERS BETWEEN RIB 23 AND RIB 39 INCLUDINGBUTTSTRAPS AT STR 12, STR 19 AND BUTTSTRAPS RUNOUTIN RIB BAY 23-24.39700 FCOR118100 FH11000 FCOR32600 FHGROUP 33DPRE 48437550FB 642AB 642BB642CB 642DB 642EB642FB 642GB 642HB642JB 642KB 650AB650BB 650CB 650DB650EB 650FB572144-01-05 542EB 642EBDETAILED INSPECTIONOF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.31200 FCOR92600 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B572144-01-07 542EB 642EBDETAILED INSPECTIONOF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.34700 FCOR103200 FH20000 FCOR50000 FHGROUP 33DPRE 48437572144-01-09 542EB 642EBDETAILED INSPECTIONOF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.31700 FCOR143700 FH20000 FCOR50000 FHGROUP 32APRE 48437572144-01-10 542EB 642EBDETAILED INSPECTIONOF OUTER WING TOP SKIN LOWERSURFACE AT CHORDWISE JOINT AT RIB 27.37600 FCOR111700 FH20000 FCOR50000 FHGROUP 33CPRE 48437572148-01-04 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.27600 FCOR125600 FH9900 FCOR45200 FHGROUP 32APRE 48437572148-01-05 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.34700 FCOR102700 FH13000 FCOR38500 FHGROUP 33AORGROUP 33BPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 118TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572148-01-06 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.31300 FCOR92500 FH11200 FCOR33300 FHGROUP 33CPRE 48437572148-01-07 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS IN RIB BAYS 26 TO 28, INCLUDING BUTTSTRAPS.28300 FCOR83700 FH10200 FCOR30100 FHGROUP 33DPRE 48437572153-01-04 574AT 674ATDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 27.31500 FCOR145000 FH10300 FCOR47600 FHGROUP 32APRE 48437572153-01-05 574AT 674ATDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 27.24800 FCOR79400 FH5800 FCOR18500 FHGROUP 33AORGROUP 33B572153-01-06 574AT 674ATDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 27.33900 FCOR108500 FH11100 FCOR35600 FHGROUP 33CPRE 48437572153-01-08 574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPAR AFT 28600 FC 9400 FC GROUP 33DFACE SPAR JOINT PLATE AT RIB 27.OR91400 FHOR30000 FHPRE 48437R 572153-01-12 574AT 674ATDETAILED INSPECTIONOF OUTER WING REAR SPAR AFTFACE SPAR JOINT PLATE AT RIB 27.36900 FCOR216400 FH8600 FCOR50000 FHGROUP 32APOST 48437572154-01-04 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.27700 FCOR127700 FH9400 FCOR43300 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 119TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572154-01-05 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.29800 FCOR95200 FH7800 FCOR24900 FHGROUP 33AORGROUP 33BR 572154-01-06 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.28600 FCOR89600 FH17200 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBR 572154-01-07 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.28600 FCOR89600 FH17000 FCOR50000 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 120TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 572154-01-08 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.24600 FCOR144500 FH17000 FCOR50000 FHGROUP 32E572154-01-09 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.24700 FCOR144800 FH14800 FCOR87300 FHGROUP 32APOST 48437542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB572154-01-10 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.28800 FCOR92000 FH9700 FCOR31200 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 121TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572154-01-11 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CB542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.30300 FCOR97000 FH10300 FCOR32900 FHGROUP 33CPRE 48437N 572154-01-13 541FB 541GB 541HB541JB 541KB 541LB541MB 541NB 541PB541QB 541RB 541SB542AB 542BB 542CBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 11 AND RIB 30 INCLUDINGTOP AND BOTTOM FLANGES AND SPAR JOINT BOLTING ATRIB 27.32800 FCOR98400 FH8000 FCOR24000 FHA330-200F542DB 641FB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SB 642AB 642BB642CB 642DB572158-01-05 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12AND RIB 23.36900 FCOR167600 FH5300 FCOR24300 FHGROUP 32APRE 48437572158-01-06 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12AND RIB 23.32700 FCOR96600 FH6900 FCOR20500 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 122TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572158-01-10 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINBUTTSTRAPS AT STRINGERS 13 AND 20 BETWEEN RIB 12AND RIB 23.38400 FCOR113600 FH5500 FCOR16500 FHGROUP 33DPRE 48437572159-01-04 542AB 542BB 542CB642AB 642BB 642CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 BETWEEN RIB 23 AND RIB26.36900 FCOR167600 FH5700 FCOR26100 FHGROUP 32APRE 48437572159-01-05 542AB 542BB 542CB642AB 642BB 642CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 BETWEEN RIB 23 AND RIB26.32700 FCOR96600 FH8100 FCOR23900 FHGROUP 33AORGROUP 33B572159-01-09 542AB 542BB 542CB642AB 642BB 642CBSPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN BUTTSTRAP AT STRINGER13 BETWEEN RIB 23 AND RIB38400 FCOR6000 FCORGROUP 33DPRE 4843726.113600 FH 17700 FH572162-01-05 523CB 623CBDETAILED INSPECTION OF OUTER WING FRONT SPARFORWARD FACE SPAR JOINT PLATE AT RIB 27.34100 FCOR109100 FH14600 FCOR46800 FHGROUP 33AORGROUP 33B572164-01-05 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.27000 FCOR124500 FH7500 FCOR34900 FHGROUP 32APRE 48437572164-01-06 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.27000 FCOR86400 FH6900 FCOR22300 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 123TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572164-01-07 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.29600 FCOR94700 FH8300 FCOR26500 FHGROUP 33CPRE 48437572164-01-09 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.29000 FCOR92700 FH8100 FCOR25900 FHGROUP 33DPRE 48437641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DB572164-01-11 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.30200 FCOR177300 FH7500 FCOR44300 FHGROUP 32APOST 48437572164-01-12 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 542AB542BB 542CB 542DB641GB 641HB 641JB641KB 641LB 641MB641NB 641PB 641QB641RB 641SB 642AB642BB 642CB 642DBDETAILED INSPECTION OF OUTER WING FRONT SPAR AFTFACE BETWEEN RIB 12 AND RIB 27 INCLUDING TOP ANDBOTTOM FLANGES.35000 FCOR109800 FH8700 FCOR27400 FHGROUP 33DPOST 48437ORGROUP 33DPOST 48437D 572166-01-05TASK DELETED IN ISSUE 17ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 124TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572180-01-04 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.21600 FCOR98300 FH9200 FCOR41900 FHGROUP 32APRE 48437572180-01-05 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.22100 FCOR65500 FH7100 FCOR21100 FHGROUP 33AORGROUP 33B572180-01-06 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.24300 FCOR71900 FH10300 FCOR30600 FHGROUP 33CPRE 48437572180-01-07 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.24600 FCOR70000 FH8400 FCOR24000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572180-01-08 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.24600 FCOR70000 FH8400 FCOR24000 FHGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 125TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572180-01-09 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.20900 FCOR93700 FH7100 FCOR32100 FHGROUP 32E572180-01-10 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.20800 FCOR93700 FH7100 FCOR32200 FHGROUP 32APOST 48437572180-01-11 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.22600 FCOR66800 FH9600 FCOR28500 FHGROUP 33DPRE 48437N 572180-01-12 541GB 541HB 541JB541KB 541LB 541MB541NB 541PB 541QB541RB 541SB 641GB641HB 641JB 641KB641LB 641MB 641NB641PB 641QB 641RB641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 12 AND RIB 23.28600 FCOR85900 FH7600 FCOR22900 FHA330-200F572181-01-04 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.21600 FCOR98300 FH9200 FCOR41900 FHGROUP 32APRE 48437572181-01-05 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.22100 FCOR65500 FH7100 FCOR21100 FHGROUP 33AORGROUP 33B572181-01-06 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.24300 FCOR10300 FCORGROUP 33CPRE 4843771900 FH 30600 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 126TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572181-01-07 542AB 542BB 542CB642AB 642BB 642CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIB 23 AND RIB 26.22600 FCOR66800 FH9600 FCOR28500 FHGROUP 33DPRE 48437572184-01-04 541QB 641QBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-02-04.21900 FCOR99700 FH5000 FCOR22700 FHGROUP 32APRE 48437572184-01-05 541QB 641QBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-02-05.22800 FCOR67600 FH5600 FCOR16600 FHGROUP 33AORGROUP 33B572184-01-06 541QB 641QBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.24600 FCOR72900 FH5600 FCOR16600 FHGROUP 33CPRE 48437NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-02-06.572184-01-07 541QB 641QBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-02-07.22900 FCOR67700 FH5200 FCOR15400 FHGROUP 33DPRE 48437572184-02-04 541QB 641QBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-01-04.21900 FCOR99700 FH5000 FCOR22700 FHGROUP 32APRE 48437572184-02-05 541QB 641QBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-01-05.22800 FCOR67600 FH5600 FCOR16600 FHGROUP 33AORGROUP 33B572184-02-06 541QB 641QBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-01-06.24600 FCOR72900 FH5600 FCOR16600 FHGROUP 33CPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 127TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330572184-02-07 541QB 641QBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOTTOMSKIN STRINGER 20 JOINT BETWEEN RIB 20 AND RIB 21.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 572184-01-07.22900 FCOR67700 FH5200 FCOR15400 FHGROUP 33DPRE 48437572185-01-01 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN MANUALREFUELLING APERTURE IN RIB BAY 22-2337700 FCOR166000 FH20000 FCOR50000 FHGROUP 32APOST 48437572185-01-02 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN MANUALREFUELLING APERTURE IN RIB BAY 22-2345500 FCOR129400 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572185-01-03 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN MANUALREFUELLING APERTURE IN RIB BAY 22-23.32600 FCOR92700 FH32600 FCOR92700 FHGROUP 33E572185-01-04 N/ADETAILED INSPECTION OFOUTER WING TOP SKIN MANUALREFUELLING APERTURE IN RIB BAY 22-23.27000 FCOR118200 FH27000 FCOR118200 FHGROUP 32E572606-01-03 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK-UP, ASSEMBLY.16200 FC 16200 FC GROUP 32APOST 48437ORGROUP 33CPOST 48437ORGROUP 33EORGROUP 32EORGROUP 33DPOST 48437N 572606-01-07 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 3, 4AND 5 AFT PICK-UP, ASSEMBLY.20100 FCOR60300 FH20100 FCOR60300 FHA330-200FN 572607-01-06 531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS 2, 3, 4AND 5 FORWARD PICK-UP LUGS FITTINGS.22100 FCOR66400 FH17000 FCOR50000 FHA330-200FISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 128TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330573001-01-05 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINTAT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT ANDREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.26000 FCOR119900 FH5300 FCOR24400 FHGROUP 32APRE 48437573001-01-07 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINTAT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT ANDREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.30000 FCOR96000 FH5600 FCOR18000 FHGROUP 33APOST 41460ORGROUP 33B573001-01-08 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINTAT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT ANDREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.28700 FCOR91700 FH5800 FCOR18700 FHGROUP 33CPRE 48437573001-01-10 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOX JOINTAT RIB 39 INCLUDING TOP AND BOTTOM SKINS, FRONT ANDREAR SPARS AND ALL FITTINGS AND BUTTSTRAPS.28200 FCOR90100 FH5700 FCOR18300 FHGROUP 33DPRE 48437573002-01-05 N/ADETAILED INSPECTION OFWINGTIP BOX TOP SKIN UPPERSURFACE AND BOTTOM SKIN LOWER SURFACE.26000 FCOR119900 FH5300 FCOR24400 FHGROUP 32APRE 48437573002-01-07 N/ADETAILED INSPECTION OFWINGTIP BOX TOP SKIN UPPERSURFACE AND BOTTOM SKIN LOWER SURFACE.30000 FCOR96000 FH5600 FCOR18000 FHGROUP 33APOST 41460ORGROUP 33B573002-01-08 N/ADETAILED INSPECTION OFWINGTIP BOX TOP SKIN UPPERSURFACE AND BOTTOM SKIN LOWER SURFACE.28700 FCOR91700 FH5800 FCOR18700 FHGROUP 33CPRE 48437573002-01-09 N/ADETAILED INSPECTION OFWINGTIP BOX TOP SKIN UPPERSURFACE AND BOTTOM SKIN LOWER SURFACE.28200 FCOR90100 FH5700 FCOR18300 FHGROUP 33DPRE 48437573003-02-04 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).31700 FCOR146000 FH4700 FCOR21900 FHGROUP 32APRE 48437573003-02-05 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).35300 FCOR113000 FH6800 FCOR21800 FHGROUP 33AORGROUP 33B573003-02-06 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).32900 FCOR103000 FH8200 FCOR25800 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 129TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 573003-02-07 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).19700 FCOR61800 FH17000 FCOR50000 FHGROUP 33ER 573003-02-08 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).16900 FCOR99700 FH14900 FCOR50000 FHGROUP 32E573003-02-09 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).28300 FCOR166400 FH7100 FCOR41600 FHGROUP 32APOST 48437573003-02-10 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).34300 FCOR109700 FH5100 FCOR16500 FHGROUP 33DPRE 48437N 573003-02-12 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TO WINGLETFORWARD AND AFT LUGS (BOTH ON WINGTIP AND WINGLET).16400 FCOR49200 FH8100 FCOR24400 FHA330-200F574106-01-04 521BB 521CB 521DB DETAILED INSPECTION OFOUTER WING FIXED LEADING 26700 FC 20000 FC GROUP 32A521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.OR122900 FHOR50000 FHPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 130TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574106-01-05 521BB 521CB 521DB521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.25600 FCOR81800 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB574106-01-06 521BB 521CB 521DB521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.28100 FCOR89900 FH20000 FCOR50000 FHGROUP 33CPRE 48437623FBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 131TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574106-01-08 521BB 521CB 521DB521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.26700 FCOR85200 FH20000 FCOR50000 FHGROUP 33DPRE 48437622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FB574106-01-11 521BB 521CB 521DB521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.33100 FCOR194500 FH20000 FCOR50000 FHGROUP 32APOST 48437623FBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 132TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574106-01-12 521BB 521CB 521DB521EB 521FB 521GB521HB 521JB 522AB522BB 522CB 522DB522EB 522FB 522GB522HB 522JB 522KB522LB 522MB 522NB522PB 522QB 522RB522SB 523CB 523DB523EB 523FB 621BB621CB 621DB 621EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SUB-SPAR JOINTSTRAPS ON TRACK RIB 1 TOTRACK RIB 16.38500 FCOR120500 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBR 574107-02-04 521FB 521GB 521HB521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522KB 522LB522MB 522NB 522PB522QB 522RB 522SB523CB 523DB 523EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINTSTRAPS AT TRACK RIB 3 TO TRACK RIB 12.37400 FCOR172200 FH14100 FCOR50000 FHGROUP 32APRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 133TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574107-02-05 521FB 521GB 521HB521JB 522AB 522BB522CB 522DB 522EB522FB 522GB 522HB522JB 522KB 522LB522MB 522NB 522PB522QB 522RB 522SB523CB 523DB 523EB621FB 621GB 621HB621JB 622AB 622BB622CB 622DB 622EB622FB 622GB 622HB622JB 622KB 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EBSPECIAL DETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE TOP SPREADER PLATE AND SUB-SPAR JOINTSTRAPS AT TRACK RIB 3 TO TRACK RIB 12.34000 FCOR108700 FH12500 FCOR40000 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 134TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-01 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.17100 FCOR79100 FH6800 FCOR31500 FHGROUP 32APRE 48437622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 135TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-02 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.17000 FCOR54300 FH5800 FCOR18500 FHGROUP 33AORGROUP 33B622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 136TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-03 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.21700 FCOR67900 FH8600 FCOR27100 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 137TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-04 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.21700 FCOR67900 FH8600 FCOR27100 FHGROUP 33E622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 138TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-05 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.18600 FCOR109500 FH7400 FCOR43700 FHGROUP 32E622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 139TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-06 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.18700 FCOR109600 FH7400 FCOR43800 FHGROUP 32APOST 48437622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 140TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-07 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.18800 FCOR60200 FH7500 FCOR24000 FHGROUP 33DPRE 48437622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 141TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574109-02-08 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.19100 FCOR61000 FH7600 FCOR24300 FHGROUP 33CPRE 48437622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 142TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 574109-02-09 521AB 521BB 521CB521DB 521EB 521FB521GB 521HB 521JB522AB 522BB 522CB522DB 522EB 522FB522GB 522HB 522JB522KB 522LB 522MB522NB 522PB 522QB522RB 522SB 523CB523DB 523EB 523FB523GB 523HB 523JB523KB 523LB 523MB523NB 523PB 621AB621BB 621CB 621DB621EB 621FB 621GB621HB 621JB 622ABDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM JOINT SPREADER PLATES AND SUB-SPARJOINT STRAPS ON ALL INTERMEDIATE RIBS (INCLUDINGCLOSING RIBS AND TELESCOPE RIBS) AND SLAT HOLD DOWNRIBS.18300 FCOR55000 FH18300 FCOR55000 FHA330-200F622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBR 574114-03-01 N/ADETAILEDINSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.28000 FCOR127000 FH12400 FCOR50000 FHGROUP 32APRE 48437574114-03-02 N/ADETAILED INSPECTION OFOUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.39700 FCOR117300 FH5500 FCOR16400 FHGROUP 33AORGROUP 33B574114-03-03 N/ADETAILED INSPECTION OFOUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.31100 FCOR92100 FH13900 FCOR41000 FHGROUP 33CPRE 48437574114-03-04 N/ADETAILED INSPECTION OFOUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG LOWER SURFACEFORWARD OF FRONT SPAR FROM RIB 11 TO RIB 39.28800 FCOR85000 FH12700 FCOR37500 FHGROUP 33DPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 143TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330574115-02-01 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARDOF FRONT SPAR BETWEEN RIBS 9 AND 11.16500 FCOR75700 FH6900 FCOR31500 FHGROUP 32APRE 48437574115-02-02 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARDOF FRONT SPAR BETWEEN RIBS 9 AND 11.19000 FCOR56300 FH2500 FCOR7500 FHGROUP 33AORGROUP 33B574115-02-03 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARDOF FRONT SPAR BETWEEN RIBS 9 AND 11.18300 FCOR54200 FH7600 FCOR22600 FHGROUP 33CPRE 48437574115-02-05 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXED LEADINGEDGE BOTTOM SKIN OVERHANG UPPER SURFACE FORWARDOF FRONT SPAR BETWEEN RIBS 9 AND 11.17300 FCOR51100 FH7100 FCOR21100 FHGROUP 33DPRE 48437R 575011-01-04 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.33400 FCOR151200 FH17300 FCOR50000 FHGROUP 32APRE 48437575011-01-05 N/ADETAILED INSPECTION OF OUTER WING TRAILING EDGE TOP 16800 FC 7000 FC GROUP 33ASKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.OR49900 FHOR20900 FHORGROUP 33BR 575011-01-06 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.37400 FCOR111000 FH19400 FCOR50000 FHGROUP 33CPRE 48437575011-01-07 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.30600 FCOR87100 FH10500 FCOR30000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575011-01-08 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.30600 FCOR87000 FH10000 FCOR28500 FHGROUP 33E575011-01-09 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.25400 FCOR111600 FH8300 FCOR36500 FHGROUP 32E575011-01-10 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.25300 FCOR111700 FH8700 FCOR38400 FHGROUP 32APOST 48437R 575011-01-11 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 1AND RIB 14.36700 FCOR109000 FH19000 FCOR50000 FHGROUP 33DPRE 48437N 575011-01-12 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGE TOPSKIN UPPER SURFACE AFT OF REAR SPAR BETWEEN RIB 128600 FCOR9100 FCORA330-200FAND RIB 14.85800 FH 27300 FHISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 144TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575012-01-10 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.35900 FCOR102100 FH8000 FCOR22900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575012-01-11 N/ADETAILED INSPECTION OFOUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 9 EXCLUDING AREA COVERED BYFLAP TRACK 2 FAIRING AND CURVED SKIN EDGE AFT OFREAR SPAR JUST INBOARD OF GEAR SUPPORT RIB 6.30300 FCOR136800 FH6800 FCOR30600 FHGROUP 32APOST 48437575016-01-04 531AB 631ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDERFLAP TRACK 2 FAIRING.36000 FCOR163400 FH8300 FCOR37700 FHGROUP 32APRE 48437575016-01-06 531AB 631ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDERFLAP TRACK 2 FAIRING.39700 FCOR117300 FH8000 FCOR23700 FHGROUP 33CPRE 48437575016-01-08 531AB 631ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR UNDERFLAP TRACK 2 FAIRING.37700 FCOR111300 FH7600 FCOR22500 FHGROUP 33DPRE 48437575017-01-04 573DB 673DBSPECIAL DETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT,INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUSTOUTBOARD OF GEAR RIB 6.36000 FCOR163400 FH5000 FCOR22800 FHGROUP 32APRE 48437575017-01-06 573DB 673DBSPECIAL DETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT,INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUSTOUTBOARD OF GEAR RIB 6.39700 FCOR117300 FH5500 FCOR16300 FHGROUP 33CPRE 48437575017-01-07 573DB 673DBSPECIAL DETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN 50 MM AROUND MANHOLE CUTOUT,INTERNAL AND EXTERNAL, AFT OF REAR SPAR JUSTOUTBOARD OF GEAR RIB 6.37700 FCOR111300 FH5200 FCOR15500 FHGROUP 33DPRE 48437575018-01-03 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.24200 FCOR109900 FH20000 FCOR50000 FHGROUP 32APRE 48437575018-01-04 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.23600 FCOR69900 FH8300 FCOR24600 FHGROUP 33AORGROUP 33B575018-01-05 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.26900FCOR79600 FH20000 FCOR50000 FHGROUP 33CPRE 48437ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 145TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575018-01-06 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.29800 FCOR84700 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437R 575018-01-07 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.20800 FCOR65200 FH17000 FCOR50000 FHGROUP 33ER 575018-01-08 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.17900 FCOR105300 FH17000 FCOR50000 FHGROUP 32E575018-01-09 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.25200 FCOR113500 FH17200 FCOR77400 FHGROUP 32APOST 48437575018-01-10 147AT 148AT 191CT192CTDETAILED INSPECTION OF OUTER WING TRAILING EDGEATTACHMENT OF SHROUD BOX.26300 FCOR20000 FCORGROUP 33DPRE 48437DEPLOY FLAPS77600 FH 50000 FH575022-01-01 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.13000 FCOR59800 FH6400 FCOR29500 FHGROUP 32APRE 48437575022-01-02 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.15400 FCOR48200 FH12200 FCOR38400 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575022-01-03 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.15400 FC 12200 FC GROUP 33EORGROUP 32EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 146TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575022-01-04 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.13200 FCOR77900 FH10500 FCOR62000 FHGROUP 32APOST 48437575022-01-05 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.13500 FCOR43100 FH6600 FCOR21200 FHGROUP 33AORGROUP 33B575022-01-06 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TO15500 FCOR7600 FCORGROUP 33CPRE 48437,REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.49500 FH 24400 FH575022-01-07 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILING EDGEINBOARD AILERON HINGES, 1-3 AT LUG AND ATTACHMENT TOREAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTAND ATTACHMENT OF HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL AND EXTERNAL.14700 FCOR47000 FH7200 FCOR23100 FHGROUP 33DPRE 48437575023-01-07 575CB 575DB 675CB 675DB DETAILED INSPECTION OF OUTER WING TRAILING EDGEOUTBOARD AILERON, HINGES 1-3 AT LUG AND ATTACHMENTTO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,HINGES 4 AND 5 AT LUG AND ATTACHMENT TO HINGEPOSTTO REAR SPAR AND TOP AND BOTTOM SKIN OVERHANGS,INTERNAL AND EXTERNAL.38900 FCOR136800 FH7300 FCOR42800 FHGROUP 32APOST 48437575025-01-04 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.34600 FCOR157200 FH7300 FCOR33300 FHGROUP 32APRE 48437575025-01-05 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.25600 FCOR75800 FH6600 FCOR19700 FHGROUP 33AORGROUP 33BISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 147TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575025-01-06 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.38400 FCOR113400 FH8100 FCOR24000 FHGROUP 33CPRE 48437575025-01-07 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.30000 FCOR85200 FH8400 FCOR23900 FHGROUP 33E575025-01-08 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.25500 FCOR96900 FH7100 FCOR32000 FHGROUP 32E575025-01-09 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILING EDGEBOTTOM SKIN LOWER SURFACE AFT OF REAR SPAR FROMRIB 8 TO RIB 12.36200 FCOR107100 FH7600 FCOR22700 FHGROUP 33DPRE 48437575051-01-01 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPERFLANGES RADII OF ROLLER TRACKS.16000 FC 8000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D575051-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK BEAM NO 1, UPPERFLANGES RADII OF ROLLER TRACKS.18000 FC 8000 FC GROUP 32EORGROUP 33E575053-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO 1, DRIVE LINK,DRIVE LEVER, DRIVE STRUT AND CARRIAGE.16000 FC 6500 FC GROUP 32APRE 45326ORGROUP 33APRE 45326ORGROUP 33BPRE 45326ORGROUP 33CPRE 45326ORGROUP 33DPRE 45326ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 148TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575054-01-01 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOXSUPPORT, FORK ASSY, DRIVE STRUT AND CARRIAGE.16000 FC 8000 FC GROUP 32APOST 45326ORGROUP 33APOST 45326ORGROUP 33BPOST 45326ORGROUP 33CPOST 45326ORGROUP 33DPOST 45326575054-01-02 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK NO 1, GEAR BOXSUPPORT, FORK ASSY, DRIVE STRUT AND CARRIAGE.18000 FC 8000 FC GROUP 32EOR, ,GROUP 33E575055-01-02 734 744DETAILEDINSPECTION OF FLAP TRACK NO 1, ATTACHMENTSTO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDINGSUPPORT STRUTS WITH ATTACHMENT FITTING.16000 FC 8000 FC GROUP 32APRE 45326ORGROUP 33APRE 45326ORGROUP 33BPRE 45326ORGROUP 33CPRE 45326ORGROUP 33DPRE 45326575055-01-03 734 744DETAILEDINSPECTION OF FLAP TRACK NO 1, ATTACHMENTSTO FUSELAGE (SWINGING LINKS WITH LUGS), INCLUDINGSUPPORT STRUTS WITH ATTACHMENT FITTING.18000 FC 8000 FC GROUP 32EORGROUP 33ER575057-01-02FLAPS EXTENDEDAFT TRACK FAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND5, UPPER FLANGES RADII.20000 FC 14500 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 149TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R575059-01-02FLAPS EXTENDEDAFT FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO 2, 3, 4 AND 5,DRIVE ARMS, DRIVE STRUTS, GUIDE ARMS WITH TRACKSIDEATTACHMENT FITTINGS AND AFT SUPPORT LINK ANDTRAVELLING BEAM AT TRACK NO 4.20000 FC 14500 FC A330-200ORA330-300575061-01-02FLAPS EXTENDEDFAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5,CARRIAGE ASSEMBLIES.20000 FC 7500 FC GROUP 32APOST 43303ORGROUP 33APOST 43303ORGROUP 33BPOST 43303ORGROUP 33CPOST 43303ORGROUP 33DPOST 43303575061-01-03FLAPS EXTENDEDFAIRINGSDETAILED INSPECTION OF FLAP TRACKS NO 2,3,4 AND 5,CARRIAGE ASSEMBLIES.20000 FC 8000 FC GROUP 32EORGROUP 33ER 575063-01-01 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2, 3, 4 AND5 LOWER FLANGES, STRAP AND ANGLES.20000 FC 15000 FC A330-200ORA330-300575067-01-02 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575067-02-02.24500 FC 8500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D575067-01-03 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575067-02-03.29500 FC 8500 FC GROUP 32EORGROUP 33EISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 150TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575067-02-02 FWD FLAP TRACKFAIRINGSFAIL SAFE BOLTSPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575067-01-02.24500 FC 8500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D575067-02-03 FWD FLAP TRACKFAIRINGSFAIL SAFE BOLTSPECIAL DETAILED INSPECTION OF FLAP TRACK BEAMS NO2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575067-01-03.29500 FC 8500 FC GROUP 32EORGROUP 33E575069-01-02 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND5, AFT ATTACHMENT SPIGOTS.24500 FC 10000 FC GROUP 32AOR,GROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D575069-01-03 FLAP TRACK FAIRING DETAILED INSPECTION OF FLAP TRACK BEAMS NO 2,3,4 AND5, AFT ATTACHMENT SPIGOTS.29500 FC 10000 FC GROUP 32EORGROUP 33ER 575401-01-02 FLAPS EXTENDEDGENERAL VISUAL INSPECTION OF INBOARD FLAP, EXTERNALSURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS ANALTERNATIVE TASK TO575401-02-01.3000 FC 3000 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 151TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575401-02-01 FLAPS EXTENDED DETAILED INSPECTION OF INBOARD FLAP, EXTERNALSURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS ANALTERNATIVE TASK TO575401-01-02.5900 FC 5900 FC GROUP 32APRE 49008ORGROUP 33APRE 49008ORGROUP 33BPRE 49008ORGROUP 33CPRE 49008ORGROUP 33DPRE 49008R 575402-01-01 FLAPS EXTENDEDSPECIAL DETAILED INSPECTION OF INBOARD FLAP, SKIN ANDDOUBLER IN CUT-OUT AREA FOR ATTACHMENT FITTINGS AT18000 FC 8000 FC A330-200ORTRACK 2, LH/RH.A330-300575403-01-02 581AB 681AB 734744DETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 1 AND TRUNNION,EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575403-02-02.20000 FC 10000 FC GROUP 32APRE 45326ORGROUP 33APRE 45326ORGROUP 33BPRE 45326ORGROUP 33CPRE 45326ORGROUP 33DPRE 45326ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 152TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575403-01-03 581AB 681AB 734744DETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 1 AND TRUNNION,EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575403-02-03.20000 FC 12000 FC GROUP 32APOST 45326ORGROUP 33APOST 45326ORGROUP 33BPOST 45326ORGROUP 33CPOST 45326ORGROUP 33DPOST 45326ORGROUP 32EORGROUP 33E575403-02-02 581AB 681AB 734744SPECIAL DETAILED INSPECTION OF INBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION,INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575403-01-02.20000 FC 10000 FC GROUP 32APRE 45326ORGROUP 33APRE 45326ORGROUP 33BPRE 45326ORGROUP 33CPRE 45326ORGROUP 33DPRE 45326ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 153TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330575403-02-03 581AB 681AB 734744SPECIAL DETAILED INSPECTION OF INBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 1 AND TRUNNION,INTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575403-01-03.20000 FC 12000 FC GROUP 32APOST 45326ORGROUP 33APOST 45326ORGROUP 33BPOST 45326ORGROUP 33CPOST 45326ORGROUP 33DPOST 45326ORGROUP 32EORGROUP 33E575405-01-02 531AT 531CB 631AT631CBFLAPS EXTENDEDDETAILED INSPECTION OF INBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 2 AND EXTERNAL DRIVESTRUT BRACKET, CARRIAGEATTACHMENT BRACKET ANDGUIDE ARM ATTACHMENT BRACKET.20000 FC 11000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DR 575503-01-02 532AT 532CB 632AT632CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 3, AND EXTERNAL DRIVESTRUT ATTACHMENT FITTING, SWING LINK TO CARRIAGEWITH ASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575503-02-02.20000 FC 15500 FC A330-200ORA330-300R 575503-02-02 532AT 532CB 632AT632CBFLAPS EXTENDEDSPEED TAPESPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 3.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575503-01-02.20000 FC 15500 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 154TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 575505-01-02 533AT 533CB 633AT633CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 4, AND EXTERNAL FWDSUPPORT LINK AND AFT SUPPORT LINK ATTACH FITTING.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575505-02-02.20000 FC 15500 FC A330-200ORA330-300R 575505-02-02 533AT 533CB 633AT633CBFLAPS EXTENDEDSPEED TAPESPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 4.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575505-01-02.20000 FC 15500 FC A330-200ORA330-300R 575507-01-02 534AT 534CB 634AT634CBFLAPS EXTENDEDDETAILED INSPECTION OF OUTBOARD FLAP, INTERNALSUPPORT FITTING AT TRACK NO 5, AND EXTERNAL DRIVESTRUT ATTACH FITTING, SWING LINK TO CARRIAGE WITHASSOCIATED ATTACH FITTING AND GUIDE ARM ATTACHFITTING.20000 FC 15500 FC A330-200ORA330-300NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575507-02-02.R 575507-02-02 534AT 534CB 634AT634CBFLAPS EXTENDEDSPEED TAPESPECIAL DETAILED INSPECTION OF OUTBOARD FLAP,INTERNAL SUPPORT FITTING AT TRACK NO 5.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575507-01-02.20000 FC 15500 FC A330-200ORA330-300R 575509-01-02 FLAPS EXTENDEDRUBBER SEALDETAILED INSPECTION OF OUTBOARD FLAP, INNER END RIBINCLUDING ROLLER AND INTERCONNECTION STRUTATTACHMENT BRACKET, EXTERNAL.NOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575509-02-02.20000 FC 15500 FC A330-200ORA330-300R 575509-02-02 FLAPS EXTENDEDRUBBER SEALSPEED TAPESPECIAL DETAILED INSPECTION OF OUTBOARD FLAP, INNEREND RIB INCLUDING ROLLERAND INTERCONNECTION STRUTATTACHMENT BRACKET, INTERNALNOTE: THIS TASK MUST BE PERFORMED AT THE SAME TIMEAS TASK 575509-01-02.20000 FC 15500 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 155TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330N 576105-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1.11100 FCOR33500 FH8200 FCOR24700 FHA330-200POST 53074ORA330-300POST 53074ORA330-200FN 576108-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.15400 FCOR92600 FH15400 FCOR92600 FHA330-200POST 53074ORA330-300POST 53074ORA330-200FR 576114-02-01 JACK FAIRINGSSPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWERFLANGE OF OUTER JACK FITTING.28700 FCOR8000 FCORA330-200OR86100 FH 24000 FH A330-300N 576115-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWERFLANGERADIUS AT LUG SIDE OF HINGE1.20400 FCOR61400 FH18400 FCOR55400 FHA330-200POST 53074ORA330-300POST 53074ORA330-200FN 576117-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS, LOWERFLANGE RADIUS AT LUG SIDE OF OUTER JACK FITTING.13100FCOR39400 FH8900 FCOR26700 FHA330-200POST 53074ORA330-300POST 53074ORA330-200FN 576118-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS, UPPERFLANGE RADIUS AT LUG SIDE OF HINGE 3.10700 FCOR53600 FH10700 FCOR53600 FHA330-200POST 53074ORA330-300POST 53074ORA330-200FR 577003-01-02 SPOILERS DEPLOYEDFLAP DEPLOYEDDETAILED INSPECTION OF SPOILER NO 1, HINGE ANDACTUATOR ATTACHMENT FITTINGS (6 PLACES).16000 FC 8000 FC A330-200ORA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 156TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330711141-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF INLET COWL ATTACHMENT(A1 FLANGE).8000 FC 8000 FC GER 711200-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGESAND SURROUNDING STRUCTURE (15 CM AROUND HINGEFITTINGS).8000 FC 8000 FCRRA330-200ORRRA330-300R 711246-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHESAND SURROUNDING STRUCTURE (15 CM AROUND LATCHFITTINGS).8000 FC 8000 FCRRA330-200ORRRA330-300R 711301-02-02 415AL 415BL 416AR416BR 425AL 425BL426AR 426BRGENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWLDOOR HINGES AND SURROUNDING STRUCTURE (15 CMAROUND HINGE FITTINGS).8000 FC 8000 FCPWA330-200ORPWA330-300R 711302-02-02 415AL 415BL 416AR416BR 425AL 425BL426AR 426BRGENERAL VISUAL INSPECTION OF FWD AND AFT FAN COWLDOOR LATCHES AND SURROUNDING STRUCTURE (15 CMAROUND LATCH FITTINGS).8000 FC 8000 FCPWA330-200ORPWA330-300711341-02-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOOR HINGESAND SURROUNDING STRUCTURE (15 CM AROUND HINGEFITTINGS).8000 FC 8000 FCGE711343-02-01 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOOR LATCHESAND SURROUNDING STRUCTURE (15 CM AROUND LATCHFITTINGS).8000 FC 8000 FCGE711345-02-01 414AL 414AR 424AL424ARGENERAL VISUAL INSPECTION OF CORE COWL DOORHINGES AND SURROUNDING STRUCTURE (15 CM AROUNDHINGE FITTINGS).8000 FC 8000 FCGE711347-01-01 414AL 414AR 424AL424ARGENERAL VISUAL INSPECTION OF CORE COWL DOORLATCHES AND SURROUNDING STRUCTURE (15 CM AROUNDLATCH FITTINGS).8000 FC 8000 FCGE712102-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF CF6-80E1 FORWARD ENGINEMOUNT EXCLUDING THE PLATFORM.4000 FCOR12000 FH4000 FCOR12000 FHGE712103-01-01 ENGINEFORWARD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT PLATFORM.6300 FCOR65800 FH4100 FCOR42400 FHCF6-80E1A2PRE 43462ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 157TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330712103-01-02 ENGINEFORWARD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT PLATFORM.6600 FCOR68300 FH6600 FCOR68300 FHCF6-80E1A2POST 43462ORCF6-80E1A3ORCF6-80E1A4712104-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF FORWARD ENGINE MOUNT REARTRUNNION CLEARANCE HOLE.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOADPATH.2520 FCOR7560 FH2520 FCOR7560 FHRR712105-01-01 ENGINEFWD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT THRUST TRUNNION.8000 FCOR24000 FH8000 FCOR24000 FHRR712106-01-01 ENGINEFORWARD ENGINE MOUNTSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT.8000 FCOR8000 FCORPWDISASSEMBLED24000 FH 24000 FH712202-01-01 414AL 414AR 424AL424ARDETAILED INSPECTION OF AFT ENGINE MOUNT EXCLUDINGTHE UPPER BEAM.8000 FCOR56700 FH8000 FCOR56700 FHGE712204-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFELINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOADPATH.4130 FCOR12390 FH4130 FCOR12390 FHRR712204-02-01 417AL 418AR 427AL428ARENGINEENGINE MOUNTDETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFELINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOADPATH.8000 FCOR24000 FH8000 FCOR24000 FHPWISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 158TASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYAIRWORTHINESS LIMITATION SECTIONA330R 783200-01-02 417DL 417EL 418DR418ER 427DL 427EL428DR 428ERGENERAL VISUAL INSPECTION OF THRUST RESERVERHINGES, SLEEVES, PINS ANDSURROUNDING STRUCTURE (15CM AROUND HINGE FITTINGS).2000 FC 2000 FCRRA330-200POST 46879ORRRA330-300POST 46879ORRRA330-200POST 47358ORRRA330-300POST 47358783201-03-01 415BL 416BR 417AL GENERAL VISUAL INSPECTION OF THRUST REVERSER8000 FC 8000 FCGE418AR 425BL 426BR427AL 428ARHINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15CM AROUND HINGE ATTACHMENTS).R 783201-04-01 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARGENERAL VISUAL INSPECTION OF THRUST REVERSERHINGES, ATTACHMENTS AND SURROUNDING STRUCTURE (15CM AROUND HINGE ATTACHMENTS).8000 FC 8000 FCPWA330-200ORPWA330-300783202-01-02 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARLATCH ACCESS DOORGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE(15 CM AROUND LATCH ATTACHMENTS).8000 FC 8000 FCGER 783202-02-02 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARLATCH ACCESS DOORGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES, ATTACHMENTS AND SURROUNDING STRUCTURE(15 CM AROUND LATCH ATTACHMENTS).8000 FC 8000 FCPWA330-200ORPWA330-300R 783245-02-01 418HR 418JR 428HR428JRGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES AND SURROUNDING STRUCTURE (15 CM AROUNDLATCH FITTINGS).8000 FC 8000 FCRRA330-200ORRRA330-300ISSUE: 28 May 2010© AIRBUS SAS2010. ALL RIGHTS RESERVED.ALI SECTION 2EASA APPROVEDPAGE: 159

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 1

© AIRBUS SAS 2010. All rights reserved. 

# A330

1 SUMMARY OF CHANGES

Section 2 AIRWORTHINESS LIMITATIONS:

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

R 521103-01-02 Applicability updated to exclude A330-200F

R 521201-01-02 Applicability updated to exclude A330-200F

R 521301-01-02 Applicability updated to exclude A330-200F

R 522201-01-02 Applicability updated to exclude A330-200F

N 523104-01-02 New task created

R 523106-01-01 Applicability updated to exclude A330-200F

N 523204-01-02 New task created

R 528203-01-02 Applicability updated to exclude A330-200F

N 528206-01-01 New task created to cover A330-200F

N 531106-01-06 New task created to cover A330-200F

N 531108-01-01 New task created to cover A330-200F

N 531109-01-01 New task created to cover A330-200F

R 531110-02-02 Applicability updated to exclude A330-200F

N 531110-02-03 New task created to cover A330-200F

R 531112-02-01 Applicability updated to exclude A330-200F

N 531112-02-02 New task created to cover A330-200F

R 531118-01-01 Applicability updated to exclude A330-200F

R 531120-01-02 Applicability updated to exclude A330-200F

N 531125-02-01 New task created to cover A330-200F

N 531145-01-01 New task created to cover A330-200F

N 531148-01-01 New task created to cover A330-200F

R 531154-01-03 Applicability extended to A330-200F

N 531155-01-01 New task created to cover A330-200F

N 531160-01-01 New task created to cover A330-200F

N 531163-01-01 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 2

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

N 531164-01-01 New task created to cover A330-200F

N 531169-02-01 New task created to cover A330-200F

N 531177-01-01 New task created to cover A330-200F

N 531178-01-01 New task created to cover A330-200F

N 531179-01-01 New task created to cover A330-200F

N 531184-01-03 New task created

R 531192-01-03 Threshold updated

R 531194-01-03 Threshold updated

R 532101-01-02 Threshold/Interval updated

Applicability updated to exclude A330-200F

N 532101-02-02 New task created as an alternative to 532101-01-02

R 532115-01-02 Applicability updated to exclude A330-200F

R 532117-01-03 Interval updated

Applicability updated to exclude A330-200F

N 532117-02-03 New task created as an alternative to 532117-01-03

R 532128-01-01 Applicability updated to exclude A330-200F

R 532138-01-01 Applicability updated to exclude A330-200F

R 532143-01-02 Applicability updated to exclude A330-200F

R 532144-01-02 Applicability updated to exclude A330-200F

R 532146-01-02 Applicability updated to exclude A330-200F

R 532147-01-02 Applicability updated to exclude A330-200F

R 532148-01-02 Applicability updated to exclude A330-200F

R 532149-01-02 Applicability updated to exclude A330-200F

N 532166-01-03 New task created

N 532166-02-03 New task created

N 532182-01-01 New task created to cover A330-200F

N 532183-01-01 New task created to cover A330-200F

R 533012-01-01 Description updated to remove the information on the

number of fasteners

R 533012-02-01 Description updated to remove the information on the

number of fasteners

N 533113-01-10 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 3

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

N 533115-01-09 New task created to cover A330-200F

R 533125-01-01 Applicability updated to exclude A330-200F

N 533127-03-04 New task created to cover A330-200F

N 533164-01-08 New task created to cover A330-200F

N 533187-01-01 New task created

N 533187-01-02 New task created

N 533187-01-03 New task created

R 533192-01-01 Applicability updated to exclude A330-200F

R 533193-01-01 Applicability updated to exclude A330-200F

N 533196-01-01 New task created to cover A330-200F

R 534124-01-02 Interval reduced

Applicability updated to exclude A330-200F

N 534124-02-02 New task created as an alternative to 534124-01-02

R 534126-01-02 Threshold/Interval updated

Applicability updated to exclude A330-200F

N 534126-02-02 New task created as an alternative to 534126-01-02

R 534135-01-01 Applicability updated to exclude A330-200F

R 534139-01-04 Applicability updated to exclude A330-200F

R 534140-02-02 Applicability updated to exclude A330-200F

R 534146-01-02 Applicability updated to exclude A330-200F

R 534149-01-02 Applicability updated to exclude A330-200F

R 534150-01-02 Applicability updated to exclude A330-200F

N 534150-01-03 New task created to cover A330-200F

R 534154-01-02 Applicability updated to exclude A330-200F

R 534155-01-02 Applicability updated to exclude A330-200F

N 534177-01-03 New task created

N 534177-02-03 New task created

N 534182-01-01 New task created to cover A330-200F

N 534184-01-01 New task created to cover A330-200F

N 545103-02-04 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 4

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

N 545108-04-19 New task created to cover A330-200F

N 545108-04-20 New task created to cover A330-200F

R 545140-01-01 Description note updated

Applicability extended

R 545140-01-02 Description note updated

Applicability extended

R 545140-01-03 Description note updated

Applicability extended

R 545140-01-06 Description note updated

Applicability extended

R 545140-01-07 Description note updated

Applicability extended

R 545140-01-08 Description note updated

Applicability extended

R 545140-02-01 Description note updated

Applicability extended

R 545140-02-02 Description note updated

Applicability extended

R 545140-02-03 Description note updated

Applicability extended

R 545140-02-06 Description note updated

Applicability extended

R 545140-02-07 Description note updated

Applicability extended

R 545140-02-08 Description note updated

Applicability extended

N 545140-02-09 New task created

N 545140-02-10 New task created

N 545140-02-11 New task created

N 545140-02-12 New task created

N 545140-02-13 New task created

N 545140-02-14 New task created

N 545140-02-15 New task created to cover A330-200F

N 545140-02-16 New task created to cover A330-200F

N 545142-02-11 New task created to cover A330-200F

N 545142-02-12 New task created to cover A330-200F

N 545150-02-13 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 5

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

N 545168-02-15 New task created to cover A330-200F

N 545168-02-16 New task created to cover A330-200F

N 545174-02-10 New task created to cover A330-200F

N 545174-02-11 New task created to cover A330-200F

N 545180-04-09 New task created to cover A330-200F

N 545180-04-10 New task created to cover A330-200F

N 551008-01-04 New task created to cover A330-200F

N 551024-01-04 New task created to cover A330-200F

N 571102-01-09 New task created to cover A330-200F

R 571103-01-06 Description updated to correct the note.

R 571103-02-06 Description updated to correct the note.

N 571123-01-01 New task created

N 571123-01-02 New task created

N 571123-01-03 New task created

N 571145-01-07 New task created to cover A330-200F

N 571146-02-09 New task created to cover A330-200F

N 571153-01-07 New task created to cover A330-200F

R 571162-01-01 Description updated

Threshold and Intervals updated

Applicability updated

N 571164-01-01 New task created to cover A330-200F

N 572016-02-12 New task created to cover A330-200F

D 572022-01-04 Task deleted as it is not applicable to A330

D 572022-01-05 Task deleted as it is not applicable to A330

D 572022-01-06 Task deleted as it is not applicable to A330

D 572022-01-07 Task deleted as it is not applicable to A330

R 572032-01-04 FH Interval figure updated

R 572039-01-04 FH Interval figure updated

R 572040-01-04 FH Interval figure updated

N 572046-01-13 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 6

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

R 572047-01-08 FH Interval figure updated

R 572047-01-09 FH Interval figure updated

R 572048-01-01 Inspection level updated

R 572048-01-02 Inspection level updated

R 572048-01-03 Inspection level updated

R 572048-01-04 Inspection level updated

R 572049-01-04 FH Interval figure updated

R 572049-01-06 FH Interval figure updated

N 572052-03-10 New task created to cover A330-200F

N 572054-01-15 New task created to cover A330-200F

N 572064-01-13 New task created to cover A330-200F

R 572067-01-06 Threshold updated

Applicability corrected

N 572067-01-15 New task created

R 572069-01-11 FH Interval figure updated

R 572069-01-12 FH Interval figure updated

N 572081-01-15 New task created to cover A330-200F

R 572082-01-09 Interval updated

R 572082-01-10 Interval updated

N 572082-01-14 New task created to cover A330-200F

N 572084-01-07 New task created to cover A330-200F

R 572090-02-01 FH Interval figure updated

N 572119-02-10 New task created to cover A330-200F

R 572131-01-04 FH Threshold and Interval figures updated

N 572140-01-10 New task created to cover A330-200F

R 572153-01-12 FH Interval figure updated

R 572154-01-06 FH Interval figure updated

R 572154-01-07 Interval updated

R 572154-01-08 Interval updated

N 572154-01-13 New task created to cover A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 7

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

D 572166-01-05 Task deleted

N 572180-01-12 New task created to cover A330-200F

N 572606-01-07 New task created to cover A330-200F

N 572607-01-06 New task created to cover A330-200F

R 573003-02-07 Interval updated

R 573003-02-08 Interval updated

N 573003-02-12 New task created to cover A330-200F

R 574107-02-04 FH Interval figure updated

N 574109-02-09 New task created to cover A330-200F

R 574114-03-01 FH Interval figure updated

R 575011-01-04 FH Interval figure updated

R 575011-01-06 FH Interval figure updated

R 575011-01-11 FH Interval figure updated

N 575011-01-12 New task created to cover A330-200F

R 575018-01-07 Interval updated

R 575018-01-08 Interval updated

R 575057-01-02 Applicability updated to exclude A330-200F

R 575059-01-02 Applicability updated to exclude A330-200F

R 575063-01-01 Applicability updated to exclude A330-200F

R 575401-01-02 Applicability updated to exclude A330-200F

R 575402-01-01 Applicability updated to exclude A330-200F

R 575503-01-02 Applicability updated to exclude A330-200F

R 575503-02-02 Applicability updated to exclude A330-200F

R 575505-01-02 Applicability updated to exclude A330-200F

R 575505-02-02 Applicability updated to exclude A330-200F

R 575507-01-02 Applicability updated to exclude A330-200F

R 575507-02-02 Applicability updated to exclude A330-200F

R 575509-01-02 Applicability updated to exclude A330-200F

R 575509-02-02 Applicability updated to exclude A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 28 MAY 2010 PAGE: APXA- 8

© AIRBUS SAS 2010. All rights reserved. 

# A330

REV

CODE TASK REFERENCE SUMMARY OF CHANGES

N 576105-01-01 New task created

N 576108-01-01 New task created

R 576114-02-01 Applicability updated to exclude A330-200F

N 576115-01-01 New task created

N 576117-01-01 New task created

N 576118-01-01 New task created

R 577003-01-02 Applicability updated to exclude A330-200F

R 711200-01-02 Applicability updated to exclude A330-200F

R 711246-01-02 Applicability updated to exclude A330-200F

R 711301-02-02 Applicability updated to exclude A330-200F

R 711302-02-02 Applicability updated to exclude A330-200F

R 783200-01-02 Applicability updated to exclude A330-200F

R 783201-04-01 Applicability updated to exclude A330-200F

R 783202-02-02 Applicability updated to exclude A330-200F

R 783245-02-01 Applicability updated to exclude A330-200F

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX B - ABBREVIATIONS

ISSUE: 28 MAY 2010 PAGE: APXB - 1

© AIRBUS SAS 2010. All rights reserved. 

# A330

ABBREVIATION MEANING

AD Airworthiness Directive

ALI Airworthiness Limitation Item

ALS Airworthiness Limitations Section

AMM Aircraft Maintenance Manual

ATA Air Transport Association

CPCP Corrosion Prevention and Control Program

D Deleted

EASA European Aviation Safety Agency

FAA Federal Aviation Agency

FC Flight Cycle

FH Flight Hour

FR Frame

HFEC High Frequency Eddy Current (NDT inspection method)

HTP Horizontal Tail Plane

JAR Joint Aviation Requirements

LOV Limit Of Validity

MOD Modification

MPD Maintenance Planning Document

MRBR Maintenance Review Board Report

MSN Manufacturer Serial Number

N New

N/A Not Applicable

NDT Non Destructive Test

NTM Non Destructive Test Manual

R Revised

RAS Repair Design Approval Sheet

ROR Record Of Revisions

SB Service Bulletins

SRM Structural Repair Manual

SSI Structural Significant Item

STC Supplemental Type Certificate

STR Stringer

THS Trimmable Horizontal Stabilizer

TPS Temporary Protection System

TOC Table Of Contents

US UltraSonic (NDT inspection method)

WV Weight Variant

# AIRWORTHINESS LIMITATION ITEMS

APPENDIX C – TERMS AND DEFINITIONS

ISSUE: 28 MAY 2010 PAGE: APXC - 1

© AIRBUS SAS 2010. All rights reserved. 

# A330

TERM DEFINITION

AIRCRAFT

STRUCTURE Consists of all load-carrying members including wings, fuselage, empennage,

engine mountings, landing gear, flight control surfaces, and related points of

attachment. The actuating portions of items such as landing gear, flight controls,

doors, etc. are treated as sy stems components. Attachme nt of the actuators to

the airframe are treated as structure.

CALENDAR TIME

(Cal) In Years (Ye), in Months (Mo), etc... mu st be counted from the date of initial

entry into service, unless otherwise st ated. Storage, maintenance, etc... do not

freeze calendar time accumulation.

CONTINUED

AIRWORTHINESS Is the process of ensuring that the leve l 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 struct ure is intended to ensure that should

serious fatigue, corrosion, or accidental damage occur within the operational life

of the aeroplane, the remaining structur e 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 pr actice. 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 de signed 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 usa ge 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 fr ist 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.