# Customer Services Directorate



# A330 Airworthiness Limitation Items



# A330

Airworthiness Limitation Items

© AIRBUS SAS 2012. All rights reserved. Confidential and proprietary document.

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

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

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

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

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

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

for which it is supplied. 

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

23 March 2012

Issue 19

# A330 Airworthiness Limitation Items

TABLE OF CONTENTS

SUBJECT SECTION

ISSUE: 23 MAR 2012 PAGE: 1-TOC

© AIRBUS SAS 2012. All rights reserved. 

# RECORD OF REVISIONS ROR

INTRODUCTION 1

GENERAL 1-1

Airworthiness Limitations 1-1- A

RULES FOR COMPLIANCE DEMONSTRATION 1-2

General 1-2- A

Conditions for DT ALI inspection 1-2- B

Reporting 1-2- C

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

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

LIMIT OF VALIDITY (LOV) 1-3

APPLICABILITY 1-4



# General 1-4- A

Weight Variant (WV) applicability 1-4- B



# Applicability System 1-4-C

EXPLANATION OF SECTION 2 TABLE FORMAT 1-5

AIRWORTHINESS LIMITATIONS 2

SUMMARY OF CHANGES APPENDIX A



# ABBREVIATIONS APPENDIX B



# TERMS AND DEFINITIONS APPENDIX C

# A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 1-ROR

EASA APPROVED

© AIRBUS SAS 2012. All rights reserved.

Issue Date Reason for revision Approved

by EASA

1 22 Aug 97 Section 2 of CMR documents originally identified

‘Structural Inspections’ These are not CMRs. New

document created.

Target date for inclusion of these requirements in

MRB report extended from 1998 to 1999.

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

Document retitled ‘Airworthiness Limitation Items’.

It was originally called ‘Structural Inspection

Requirements’.

Text of Section 1 modified to refer to A330-200

and to add a new paragraph to justify

acceptability of 1999 target date.

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

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

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

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

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

Text of Section 1 modified to revise target dates

for publication of ALIs.

8 31 Oct 01 Document completely revised to introduce ALIs

following completion of the full scale fatigue test

and teardown analysis.

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

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

025 added for A330-300. Reference to Zonal

Program deleted from paragraph 1.5.

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

052 in new WV GROUP 33E. New DSG added

for GROUP 33E. To provide compatibility with

MRBR and MPD, task numbering changed to 9

digits and applicability amended.

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

engines (A330-300 WV 051) included.

Tasks that were deleted in Issue 10 reintroduced.

# A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 2-ROR

EASA APPROVED

© AIRBUS SAS 2012. All rights reserved.

Issue Date Reason for revision Approved

by EASA

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

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

included.

Requirements of WV GROUP 33E for RR

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

Requirements for enhanced modifications

embodied on non-fully enhanced aircraft

included.

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

A330-303.

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

WV022) included.

Task applicabilities changed due to impact of

product improvement mods for A330 WV000 up

to WV030 series.

New numbering rules (ALI task previously with 9

digits replaced by 10 Digit number system)

included in section 2.

WV053, 054, 055 added for Group 32E.

WV027 added for Group 32A.

WV026, 027 added for Group 33C.

WV053 added for Group 33E.

Confidentiality statement added. Approved by

EASA

under reference

EASA.A.C.01277

on 17 January 2006

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

Task applicabilities changed due to impact of

modifications.

GE requirements updated due to new calculation. Approved by

EASA

under reference

EASA.A.C.07222

on 9 July 2007

16 13 Jun 08 New compliance time requirements introduced in

the Record Of Revisions.

Introduction reworded with :

New Limits Of Validity (LOV)

New information concerning Rules for

Compliance Demonstration (Alternative

inspections, Multiple WV configuration...)

Task requirements updated due to:

Intermediate Service Goal exercise

Fleet survey results

Modifications/In-service experience Approved by

EASA

under reference

EASA.A.C.10414

on 4 Nov 2008

# A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 3-ROR

EASA APPROVED

© AIRBUS SAS 2012. All rights reserved.

Issue Date Reason for revision Approved

by EASA

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

Task applicabilities changed due to impact of

modifications. Approved by

EASA

under reference

10031148

on 29 July 2010

18 1st AUG 2011 Task requirements updated due to:

Fleet survey results

New approach added with 2 sets of figures for the

tasks sensitive to the range

Section 2.2 is created for tasks FH optimized

Modifications/In-service experience

Weight variants added Approved by

EASA

under reference

10038005

on 11 January 2012

19 23 MAR 2012 Correction of errors from Rev 18

Weight Variant 062 added for Group 32E

Weight Variant 055 added for Group 33E Approved by

EASA

under reference

10040023

on 08 June 2012

# A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 4-ROR

EASA APPROVED

AIRBUS SAS 2012. All rights reserved. 

# COMPLIANCE TIME:

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

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

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

defined in th e A330 ALI Document revision 19.

2. From the 11 January 2012 to 11 January 2014, except for those specific task/applicabilities

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

defined in, either:

- The ALI Document at issue 17

or,

- The ALI Document at issue 1 9.

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

table 1 through the following instructions:

- As per issue 1 8 :

This means that no compliance time is granted.

Issue 1 8 is to be applied from 11 January 2012.

- As per issue 17 for 1 year:

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

After this da te, issue 1 8 shall be applied.

- As per Para 2:

This means that there is no specific instruction.

The conditions defined in paragraph 2 above, apply.

TABLE 1

TASK REFERENCE THRESHOLD INTERVAL

532124-02-08 As per Issue 1 8 As per Para 2

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

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

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

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

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

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

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

531130-01-02 As per Para 2 As per Issue 17 for 1 year

# A330 Airworthiness Limitation Items

RECORD OF REVISIONS

ISSUE: 23 MAR 2012 PAGE: 5-ROR

EASA APPROVED

AIRBUS SAS 2012. All rights reserved. 

# TABLE 1

TASK REFERENCE THRESHOLD INTERVAL

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

574115-02-05 As per Para 2 As per Issue 17 for 1 year

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 6

© AIRBUS SAS 2012. All rights reserved. 

# 1 INTRODUCTION

1-1 GENERAL

The data provided has been established with the following rules:

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

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

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

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

1-1-A Section 2 - Airworthiness Limitations

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

evaluation on structural element that could contri bute to catastrophic failure of the aircraft.

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

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

pressurization loads, and whose failure could result in catastrophic failure of the airplane.

Corrosion Level 1 is defined as follows:

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

or - Corrosion occuring between successive inspections that exceeds allowable limit but is local

and can be attributed to an event not typical of Operator usage of other aircraft in the same

fleet (e.g. mercury spill).

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

(SECTION D) of the A330 MRB Report is an acceptable means of compliance.

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

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

damage.

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

maintenance tasks, providing that they are performed with the same inspection level, as

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

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

following Airbus supporting publications:

− Maintenance Planning Document (MPD),

− Aircraft Maintenance Manual (AMM),

− Non-Destructive Testing Manual (NTM)

− Structural Repair Manual (SRM).

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 7

© AIRBUS SAS 2012. All rights reserved. 

# 1-1-B Section 2-1:

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

that could be sensitive to the range or not.

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

the description column:

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

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

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

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

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

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

1-1-C Section 2-2:

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

tolerance that are sensitive to the range.

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

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

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

1-2 RULES FOR COMPLIANCE DEMONSTRATION

1-2-A General

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

(LOV) in FC or FH whichever occurs first.

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

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

maintenance program.

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

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

flight.

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

embodiment, unless otherwise stated.

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

from manufacturer, unless otherwise stated.

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 8

© AIRBUS SAS 2012. All rights reserved. 

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

performed.

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

associated with the inspection method used at last inspection.

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

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

accomplishment and the threshold is greater than the interval.

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

Cycles up to threshold inspection or between two consecutive inspections.

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

inspection or between two consecutive inspections.

1-2-B Conditions for DT ALI inspection

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

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

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

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

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

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

Repair Manual SRM or other documentation acceptable to the relevant Airworthiness

Authority.

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

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

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

the DT ALI maintenance requirement.

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

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

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

must be applied.

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

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

1-2-C Reporting

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

when the corrosion is detected) shall be r eported to Airbus.

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

− DT ALI maintenance requirement reference,

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 9

© AIRBUS SAS 2012. All rights reserved. 

# − Aircraft Manufacturer Serial Number (MSN) affected,

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

the finding,

− Identification of the affected structure,

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

− Circumstance of detection and inspection method used.

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

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

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

Compliance (AMOC).

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

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

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

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

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

any necessary adaptations of the limitations.

1-3 LIMIT OF VALIDITY (LOV)

Aircraft series LOV

Flight Hours Flight Cycles

A330-200 series excl. WV050’s and above or 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 given aircraft series, no combination is

allowed.

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 10

© AIRBUS SAS 2012. All rights reserved. 

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

These aircraft shall be operated within the envelope of:

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

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

1-4 APPLICABILITY

1-4-A General

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

Aircraft series Aircraft models WV

A330-200 A330-201 020, 023, 024, 050, 052,054, 055, 056, 057,

058, 059, 060, 061, 062

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

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

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

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

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

056, 057, 058, 059, 060, 062

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

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

060, 061, 062

A330-200F A330-223F 000, 001, 002

A330-243F 000, 001, 002

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

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

A330-303 050, 052, 054, 055

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

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

A330-323 020, 022, 025, 050, 052, 054, 055

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

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

014, 022, 052, 054, 055

A330-343 020, 022, 024, 050, 052, 054, 055

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 11

© AIRBUS SAS 2012. All rights reserved. 

# 1-4-B Weight Variant (WV) applicability

A/C Series Weight Variants WV Group

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

050, 051, 052, 053, 054, 055, 056, 057, 058, 059,

060, 061, 062 Group 32E

A330-200F 000, 001, 002 -

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

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

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

022 Group 33D

050, 051, 052, 053, 054, 055 Group 33E

Interpretation: Group XYZ

− X: Aircraft Type 3 for A330

− Y: Series (2 for -200, 3 for -300)

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

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

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

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

readability of the applicability column.

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

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

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

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

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

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

confirmed using the weight variant information given in Table 3 of SRM introduction.

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

modifications corresponding to the weight variant change after the aircraft delivery.

It is operator’s responsibility to check the embodiement of the referenced Service Bulletins in

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

(MSN).

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

MTOW have to be applied.

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 12

© AIRBUS SAS 2012. All rights reserved. 

# 1-4-C Applicability system

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

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

Examples are given below:

Applicability Task applicable to

ALL All A330 aircraft.

A330-xxx - xxx series aircraft.

A330-200 A330-200 Pax aircraft

A330-200F A330-200 Freighter aircraft

PRE nnnnn All A330 PRE MOD nnnnn.

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

POST nnnnn All A330 POST MOD nnnnn.

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

POST nnnnn

Sxxxxx All A330 POST MOD nnnnn (at least with Mod Proposal S xxxxx em bodied).

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

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 13

© AIRBUS SAS 2012. All rights reserved. 

# 1-5 EXPLANATION OF SECTION 2 TABLE FORMAT

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

REV CODE

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

compared to previous issue of the document.

<Blank> = No amendment.

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

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

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

TASK REFERENCE

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

follows:

XXXXXX-XX-XX

Applicability index

Sequential number

SSI number

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

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

Detailed or Special Detailed.

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

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

differences e.g. different access panel numbers.

# A330 Airworthiness Limitation Items

INTRODUCTION

ISSUE: 23 MAR 2012 PAGE: 14

© AIRBUS SAS 2012. All rights reserved. 

# ACCESS

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

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

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

TASK DESCRIPTION

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

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

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

added to clarify the inspection area.

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

performed at the same time, are included.

THRESHOLD

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

INTERVAL

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

subsequent times.

APPLICABILITY

This column indicates the applicability of the task.A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 1EASA APPROVED©AIRBUS SAS 2012. All rights reserved.2 AIRWORTHINESS LIMITATIONS2-1 SECTION 2.1REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY521101-01-01TASK DELETED IN ISSUE 18521103-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 1 (FORWARDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.12800 FC 12800 FC A330-200ORA330-300521105-01-01 ESCAPE SLIDEINSULATIONLININGDETAILED INSPECTION OF TOP & BOTTOMCROSSBEAMS T8 & T1 ENDS AT FRAMES FR1 AND FR7IN THEIR UNION TO DOOR STOP ASSEMBLIES, ONFORWARD PASSENGER/CREW DOOR, LH/RH.33900 FC 15500 FC A330-200ORA330-300521201-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.12800 FC 12800 FC A330-200ORA330-300521203-01-01TASK DELETED IN ISSUE 18521203-01-02TASK DELETED IN ISSUE 18521301-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) SKIN, EXTERNAL SURFACE.12800 FC 12800 FC A330-200ORA330-300521303-01-01TASK DELETED IN ISSUE 18521303-01-02TASK DELETED IN ISSUE 18522201-01-02 N/AGENERAL VISUAL INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) SKIN,EXTERNAL SURFACE.12800 FC 12800 FC A330-200ORA330-300522203-01-01TASK DELETED IN ISSUE 18522203-01-02TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 2EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY523104-01-02 132AR 132BR 132CR132DR 132ER 132FR132GR 132HR 132JR132KR 132LRDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR HINGE ASSEMBLIES AT FR 20BTO FR25 (10 PLACES).15800 FC 3300 FC ALL523106-01-01 821CRDOOR LOCKING HANDLEUNLOCKEDDETAILED INSPECTION OF FORWARD CARGOCOMPARTMENT , DOOR FRAME C20B BETWEEN BEAM3 AND 4.10600 FC 2600 FC A330-200PRE 51038PRE 50528ORA330-300PRE 51038PRE 50528523204-01-02 152AR 152BR 152CR152DR 152ER 152FR152GR 152HR 152JR152KR 152LRDETAILED INSPECTION OF AFT CARGOCOMPARTMENT DOOR HINGE ASSEMBLIES AT FR 60TO FR 64A (10 PLACES)15800 FC 3300 FC ALL524101-01-02 N/ADETAILED INSPECTION OF AVIONICS COMPARTMENTLOWER ACCESS DOOR SKIN, EXTERNAL SURFACE.10300 FC 10300 FC ALL524103-01-02 811DOOR FLOOR PANELDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, AVIONICS COMPARTMENT LOWERACCESS DOOR CROSS MEMBERS.31500 FC 14200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D528104-01-02 734 744DETAILED INSPECTION OF MAIN LANDING GEAR, MAINDOOR, CENTER FITTING AND SURROUNDING AREA(300 MM AROUND), LH/RH.8300 FC 8300 FC ALL528203-01-02 713 714DETAILED INSPECTION OF NOSE LANDING GEAR,FORWARD DOOR, HINGES (NO 1, NO 2, NO 3)INCLUDING FITTINGS ON FUSELAGE, LH/RH.9600 FC 9600 FC A330-200ORA330-300528206-01-01 713 714 715 716 DETAILED INSPECTION OF NOSE LANDING GEARDOORS, HINGES (NO 1, NO 2, NO 3, NO 4, NO5)INCLUDING FITTINGS ON FUSELAGE, LH/RH.12000 FC 12000 FC A330-200F531106-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.9 AND FR.10A AT COCKPIT LATERAL WINDOWLOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.21000 FC 10100 FC GROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 3EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531106-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.9 AND FR.10A AT COCKPIT LATERAL WINDOWLOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.32600 FC 10000 FC GROUP 33BORGROUP 32AORGROUP 33CORGROUP 33D531106-01-06 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR.9 AND FR.10A AT COCKPIT LATERAL WINDOWLOWER CORNER AREA, EXTERNAL SURFACE, LH/RH.24000 FC 7900 FC A330-200F531108-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OFCIRCUMFERENTIAL JOINT AT FRAME 18 BETWEENSTRINGER 3 AND STRINGER 7, BUTT JOINT AND REARPANEL, LH.17400 FC 11900 FC A330-200F531109-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OFCIRCUMFERENTIAL JOINT AT FRAME 18 BETWEENSTRINGER 11 AND STRINGER 13, BUTT JOINT ANDREAR PANEL, RH .28700 FC 19700 FC A330-200F531110-02-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR 10 AND FR 13 FROM FLOOR LEVEL TO STR 9 FWD,EXTERNAL SURFACE, LH/RH.18500 FC 18500 FC A330-200ORA330-300531110-02-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR 10 AND FR 13 FROM FLOOR LEVEL TO STR 9 FWD,EXTERNAL SURFACE, LH/RH.10100 FC 10100 FC A330-200F531112-02-01 N/ADETAILED INSPECTION OF FUSELAGE STRUCTUREAROUND DOOR 1 (FORWARD PASSAGER / CREWDOOR), EXTERNAL SURFACE, BETWEEN FR 13 AND FR18 FROM LATERAL LONGITUDINAL LAP JOINT TO STR 9AFT, LH/RH.8900 FC 8900 FC A330-200ORA330-300531112-02-02 N/ADETAILED INSPECTION OF FUSELAGE STRUCTUREAROUND DOOR 1 (FORWARD PASSAGER / CREWDOOR), EXTERNAL SURFACE, BETWEEN FR 13 AND FR18 FROM LATERAL LONGITUDINAL LAP JOINT TO STR 9AFT, LH/RH.8700 FC 8700 FC A330-200F531118-01-01 121AL 121EL713 714GENERAL VISUAL INSPECTION OF GROUND SERVICESCONNECTION ACCESS DOORS CUTOUTS AND NOSELANDING GEAR CUTOUT, BETWEEN FR 4 AND FR 19 ONLOWER FUSELAGE.3700 FC 3700 FC A330-200ORA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 4EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531120-01-02 713 714GENERAL VISUAL INSPECTION OF NLG BAY INTERNALSTRUCTURE, NOSE LANDING GEAR WELL PANELS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED1300 FCOR3900 FH1300 FCOR3900 FHA330-200ORA330-300531124-01-03TASK DELETED IN ISSUE 18531124-01-04 713 714DETAILED INSPECTION OF NLG BAY SIDE PANEL TOPINNER RADIUS FROM NLG BAY FORWARD PANEL TONLG BAY AFT PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28500 FCOR82000 FH10100 FCOR30400 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531124-01-05TASK DELETED IN ISSUE 18531125-01-03 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FRAME 17ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48TO 51, LH/RH.39500 FC 4800 FC GROUP 33AORGROUP 33B531125-01-04 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FRAME 17ATTACHMENT TO BOTTOM SKIN FROM STRINGER 48TO 51, LH/RH.21400 FC 5750 FC GROUP 32AORGROUP 33CORGROUP 33D531125-02-01 811 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 LANDINGGEAR ACTUATOR FITTING.32900 FC 4750 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 5EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531130-01-02 NOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 16A AT CABIN FLOORLEVEL, LH/RH.21900 FC 4350 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258531131-01-02 NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 16A, JOINT AREA BETWEENSTRINGERS 28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 531131-02-02.18500 FC 9800 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258531131-02-02 NOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 16A, JOINT AREABETWEEN STRINGERS 28 AND 30, LH/RH.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 531131-01-02.18500 FC 9800 FC GROUP 33APRE 44258ORGROUP 33BPRE 44258531132-01-02 NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 14 JOINT BETWEEN STRINGERS28 AND 30 LEVEL, LH/RH.35100 FC 12900 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531133-01-03TASK DELETED IN ISSUE 18531134-01-01TASK DELETED IN ISSUE 18531134-01-02TASK DELETED IN ISSUE 18531134-01-03 AVIONICS COMPT DOOROPENEDSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, BOOMERANG FRAMES 11A TO16A ATTACHMENT TO SKIN, BETWEEN STRINGERS 46AND 47, LH/RH.39000 FC 3700 FC GROUP 32AORGROUP 33CORGROUP 33D531135-01-02 N/ASPECIAL DETAILED INSPECTION OF REAR LOWERCORNER OF THE COCKPIT LATERAL WINDOW FRAME,FORWARD OF FR.10, EXTERNAL SURFACE, LH/RH.4850 FC 4850 FC ALLA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 6EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531136-01-02 CEILING PANELSNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 12 AND 13 DOUBLER AREA ATCROWN CENTRELINE.17500 FC 10100 FC GROUP 33APRE 42481ORGROUP 33BPRE 42481531138-01-02 RADOME OPENEDINSULATION PANELSDETAILED INSPECTION OF FORWARD PRESSUREBULKHEAD FORWARD FACE STRINGERS AND SKIN,FROM Y=-50 TO Y=50 ABOVE COCKPIT FLOOR LEVEL.34700 FC 9150 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531139-01-02 811NOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FORWARD PRESSURE BULKHEAD AFTFACE VERTICAL BEAMS AND UPPER SHEET AT Y=-330,Y=0 AND Y=330, ABOVE COCKPIT FLOOR LEVEL.34700 FC 9150 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531140-01-01 831LININGNOTE 1GALLEYS AND TOILETSIF INSTALLEDSPECIAL DETAILED INSPECTION OF LATERAL FRAME10 AT FLOOR LEVEL ATTACHMENT, ABOVE COCKPITFLOOR, 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,INTERNAL STRUCTURE, LH/RH.17500 FC 9000 FC GROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 7EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531142-01-02 CEILINGNOTE 1DETAILED INSPECTION OF FRAME 10 UPPER CURVEDMEMBER BETWEEN CROWN CENTRELINE AND UPPERLATERAL SPLICING, SPLICE EXCLUDED, INTERNALSTRUCTURE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-02-02.34900 FC 5200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531142-02-02 CEILINGNOTE 1SPECIAL DETAILED INSPECTION OF FRAME 10 UPPERCURVED MEMBER BETWEEN CROWN CENTRELINEAND UPPER LATERAL SPLICING, SPLICE EXCLUDED,INTERNAL STRUCTURE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 531142-01-02.34900 FC 7800 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531143-01-02 NOTE 1AIR DUCTSVACUUM PIPESDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FLOOR BEAM AND CRUCIFORM FITTINGAT FR.14, LH/RH.16600 FC 3900 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531144-01-02 NOTE 1LININGTOILETSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, JUNCTION AREA BETWEENFRAME 14 AND CRUCIFORM FITTING, LH/RH.16600 FC 7000 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 8EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYR 531144-01-03 LININGNOTE 1TOILETSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNALSTRUCTURE, JUNCTION AREA BETWEEN FRAME 14ANDCRUCIFORM FITTING, LH/RH.29000 FC 7000 FC GROUP 32EORGROUP 33E531145-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OFCIRCUMFERENTIAL JOINT AT FRAME19 BETWEENSTRINGER 45 AND STRINGER 47, BUTT JOINT ANDREAR PANEL, RH.24400 FC 23700 FC A330-200F531146-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, LATERAL AND AFT WINDOW FRAMESJUNCTION WITH FRAME 7 UPPER MEMBER, LH/RH.37100 FC 8750 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531148-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OFCIRCUMFERENTIAL JOINT AT FRAME18 BETWEENSTRINGER 30 AND STRINGER 32, BUTT JOINT ANDREAR PANEL, LH.27700 FC 23700 FC A330-200F531149-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, ANGLE GUSSET ABOVE FRONTWINDSHIELD PANELS, INCLUDING TOP 3 NUTS ONCENTRE POST.35300 FC 8500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 9EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531154-01-02 LININGSSLIDING WINDOWSOPENEDNOTE 1DETAILED INSPECTION OF LOWER SURFACE OFUPPER CLOSING PANEL BETWEEN FR 7 AND FRONTWINDSHIELD SIDE POST, INTERNAL STRUCTURE,LH/RH.15800 FC 8100 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531154-01-03 LININGSSLIDING WINDOWSOPENEDNOTE 1DETAILED INSPECTION OF LOWER SURFACE OFUPPER CLOSING PANEL BETWEEN FR 7 AND FRONTWINDSHIELD SIDE POST, INTERNAL STRUCTURE,LH/RH.31300 FC 8100 FC GROUP 32EORGROUP 33EORA330-200F531155-01-01 LININGNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 14C, FROMSTRINGER 9 TO STRINGER 12, LH/RH.17500 FC 9100 FC A330-200F531157-01-02 LININGNOTE 1DETAILED INSPECTION OF PASSENGER / CREW DOORUPPER KEEL FITTINGS AT FRAME 17 AND AT STGR.12LEVEL, INTERNAL STRUCTURE, LH/RH.31300 FC 6700 FC GROUP 33A531158-01-01 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN AFT WINDOWFRAME AND FRAMES 8 AND 9 UPPER MEMBERS,LH/RH.35300 FC 15500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531160-01-01 811 821AVIONICS BAY FLOORPANELSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, RADIUS OF LUGS ON UPPERCORNER OF PORTAL FRAME 15A, LH/RH.9900 FC 6300 FC A330-200F531161-01-02TASK DELETED IN ISSUE 18531163-01-01 713 714NLGSPECIAL DETAILED INSPECTION OF NOSE LANDINGGEAR MAIN ATTACHEMENT BEARING BORE, LH/RH.13800 FC 13800 FC A330-200F531164-01-01 713 714SPECIAL DETAILED INSPECTION OF NOSE LANDINGGEAR BAY LATERAL PANELS, JUNCTION TO LOWERFRAME 17 FITTING, LH/RH.7000 FC 7000 FC A330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 10EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531169-02-01 125AL 125BL 125CL126BR 126CR713 714DETAILED INSPECTION OF NOSE FUSELAGE LOWERSKIN AND FAIRING SUBSTRUCTURE, AREA COVEREDBY NOSE FAIRING BETWEEN FR10 AND FR17INCLUDING NLG BAY LATERAL PANEL EXTERNALSURFACE, FLAT PANEL, FR16A AND FORWARD FACEOF LOWER FR17 FITTING, LH/RH.15600 FC 15600 FC A330-200F531175-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE AT JUNCTION BETWEEN FR.17 ANDMACHINED STIFFENERS AT STGR.14/18/22/24, LH/RH.22700 FC 7900 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D531177-01-01 125AL 125BL 125CL126BR 126CR713 714SPECIAL DETAILED INSPECTION OF LONGITUDINALJUNCTION CENTRAL AND LATERAL PANELS ATSTRINGER 46, EXTERNAL SURFACE BETWEEN FR11 TOFR12A, LH/RH.17400 FC 17400 FC A330-200F531178-01-01 125AL 125BL 125CL126BR 126CR713 714DETAILED INSPECTION OF Y750 AFT FITTING, TOPRADIUS, LH/RH.23100 FC 13000 FC A330-200F531179-01-01 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 TO BEREMOVEDSPECIAL 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 TO BEREMOVEDSPECIAL 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 55534531184-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, RIVET LINES AT UPPERLONGITUDINAL LAP JOINT (STGR.9 AFT LEVEL) FROMFR.13 TO FR.13A AND FROM FR.14 TO FR.16A, LH/RH.21100 FC 16900 FC A330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 11EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531185-01-02TASK DELETED IN ISSUE 18R 531186-01-02 TOILETS & CRRLININGSNOTE 1TITANIUM RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERSOF FORWARD UPPER PANEL ABOVE STRINGER 9FORWARD, LH/RH.31500 FC 10400 FC GROUP 33APRE 40347PRE 49411531186-01-03 TOILETS & CRRLININGSNOTE 1TITANIUM RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 13, 8 FASTENERSOF FORWARD UPPER PANEL ABOVE STRINGER 9FORWARD, LH/RH.28700 FC 9600 FC GROUP 33APOST 40347PRE 49411ORGROUP 32APRE49411ORGROUP 33BPRE 49411ORGROUP 33CPRE 49411ORGROUP 33DPRE 49411531188-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OFFRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5ROWS AT STGR.9 FWD LEVEL, LH/RH.31500 FC 7600 FC GROUP 33APRE 40347PRE 53102A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 12EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531188-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT, RIVET ROWS FORWARD OFFRAME 13 FROM STR.9 AFT TO STR.26, EXCLUDING 5ROWS AT 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 53102531189-01-02 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FORWARD PAX/CREW DOOR CUT-OUT,FORWARD UPPER LONGERONAT STRINGER 12 LEVEL,BETWEEN FR. 13A AND FR.13B, LH/RH.29300 FC 8850 FC GROUP 32APRE 49194ORGROUP 33AORGROUP 33BORGROUP 33CPRE 49194ORGROUP 33DPRE 49194531192-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, JUNCTION AREA BETWEEN FR. 13FORWARD FACE AND STRINGER 9 FORWARD AND FR.13 AFT FACE AND STRINGER 12, LH/RH.21800 FC 8100 FC ALLA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 13EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY531194-01-03 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, MACHINED STIFFENERS 14 AND 22BETWEEN FR. 17 AND FR.18, LH/RH.21800 FC 8100 FC ALL531198-01-02 LININGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE BELOW CABIN FLOOR LEVEL, TORSIONBOX INTERNAL PANEL BETWEEN FRAMES 13A AND 14,AND 16A AND 17, LH/RH.29300 FC 8850 FC GROUP 32APRE 49194ORGROUP 33AORGROUP 33BORGROUP 33CPRE 49194ORGROUP 33DPRE 49194532101-01-02 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 18 AND FR 38FROM STR 26 TO BOTTOM CENTER LINE, INCLUDINGSKIN SPLICES AND LAP JOINTS, EXCLUDING AREASUNDERNEATH BELLY FAIRING LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-02-022250 FC 2250 FC A330-200ORA330-300532101-02-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 26 TOBOTTOM CENTER LINE, INCLUDING SKIN SPLICES ANDLAP JOINTS, EXCLUDING AREAS UNDERNEATH BELLYFAIRING LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532101-01-026900 FC 6900 FC A330-200ORA330-300532114-01-02TASK DELETED IN ISSUE 18532114-01-03TASK DELETED IN ISSUE 18532114-01-04TASK DELETED IN ISSUE 18532114-01-05TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 14EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532115-01-02 821GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR CUTOUT, VISIBLE PART OFLATERAL FRAMES (FR 20A AND FR 25A).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17300 FCOR52100 FH17300 FCOR52100 FHA330-200ORA330-300532117-01-03TASK DELETED IN ISSUE 18532117-02-03TASK DELETED IN ISSUE 18532124-02-04 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FC 8800 FC GROUP 32A532124-02-05 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.19300 FC 3700 FC GROUP 33APRE 45293PRE 41856ORGROUP 33BPRE 45293PRE 41856532124-02-06 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.22600 FC 10000 FC GROUP 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 FC 5500 FC GROUP 33APOST 41856ORGROUP 33BPOST 41856532124-02-08 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.21300 FC 4400 FC GROUP 33CORGROUP 33D532124-02-09 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FC 4500 FC GROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 15EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532124-02-10 832 842SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 2 (MIDPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH SCUFF PLATE, LH/RH.26000 FC 7300 FC GROUP 32E532125-01-04 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.8800 FC 8800 FC GROUP 32A532125-01-05 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.3600 FC 3600 FC GROUP 33APRE 45293PRE 41856ORGROUP 33BPRE 45293PRE 41856532125-01-06 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.9700 FC 9700 FC GROUP 33APOST 45293PRE 41856ORGROUP 33BPOST 45293PRE 41856532125-01-07 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.5400 FC 5400 FC GROUP 33APOST 41856ORGROUP 33BPOST 41856532125-01-08 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.4200 FC 4200 FC GROUP 33CORGROUP 33D532125-01-09 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.4400 FC 4400 FC GROUP 33E532125-01-10 832 842SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 2 (MID PASSENGER/CREW DOOR) CUT-OUTUPPER CORNERS.7300 FC 7300 FC GROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 16EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532126-01-01 832 842DOOR FRAME LININGINSULATIONDETAILED INSPECTION OF DOOR 2, COVER PLATE OFTORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR12 AND STR 13, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20700 FCOR62100 FH11700 FC GROUP 33APRE 45223ORGROUP 33BPRE 45223532127-01-01 832 842DOOR FRAME LININGNOTE 1DETAILED INSPECTION OF DOOR NO 2, FR 33,BETWEEN STR 13 AND STR 15, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19000 FCOR62100 FH6300 FC GROUP 33APRE 44147ORGROUP 33BPRE 44147532128-01-01TASK DELETED IN ISSUE 18532129-01-02TASK DELETED IN ISSUE 18532129-01-03TASK DELETED IN ISSUE 18532130-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AND VISIBLE PORTION OF WINDOWFORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR36 AND FR 38 FROM STR 18 TO STR 22, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20400 FC 8500 FCOR26100 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532130-01-03TASK DELETED IN ISSUE 18532130-01-04TASK DELETED IN ISSUE 18532138-01-01 131AG 821DRAINMASTDETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AT DRAIN MAST CUT-OUT, BETWEEN FR 37AND FR 37.1, FROM STR 53 TO STR 54, LH ONLY.26500 FC 10000 FC A330-200ORA330-300532139-01-01 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AT CLOSED DRAIN MAST CUT-OUTBETWEEN FR 28 AND FR 29, FROM STR 46 TO STR 47,RH.NOTE: THIS TASK IS APPLICABLE ONLY IF THE CUTOUT IS EMBODIED IN THE SKIN.22100 FC 8500 FC GROUP 33APOST 41367ORGROUP 33BPOST 41367532143-01-02TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 17EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532144-01-02 832 842CEILING PANELSNOTE 1DETAILED INSPECTION OF FRAMES AND STRINGERCOUPLING AREA, BETWEEN FR 32 AND FR 34, FROMSTR 9 TO STR 13 LH/RH, INTERNAL STRUCTURE.20000 FC 10000 FC A330-200ORA330-300532146-01-02TASK DELETED IN ISSUE 18532147-01-02 821CARGO COMPARTMENTFLOOR PANELSLININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS OF CARGO FLOOR ATTACHMENTS FITTINGSFROM FR 20 TO FR 38 LH, FROM FR 26 TO FR 38 RH,BETWEEN STR 34 AND STR 43.20600 FC 10000 FC A330-200ORA330-300532148-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREA AT FR 31 FROM STR 9 TO STR 15 LH/RH,EXTERNAL SURFACE.23200 FC 15900 FC A330-200ORA330-300532149-01-02TASK DELETED IN ISSUE 18532150-01-02TASK DELETED IN ISSUE 18532150-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31AND FR 37.1.35400 FC 3400 FC GROUP 33APRE 46636ORGROUP 33BPRE 46636ORGROUP 33CPRE 46636ORGROUP 33DPRE 46636532150-01-04TASK DELETED IN ISSUE 18532151-01-01 N/ASPECIAL DETAILED INSPECTION OF EXTERNAL SKINOF LONGITUDINAL LAP JOINT AT STR 22, BETWEEN FR37.1 AND FR 38.23100 FC 2900 FC GROUP 33APRE 45226ORGROUP 33BPRE 45226R 532152-01-01 N/ADETAILED INSPECTION OF FUSELAGE SKIN AT SHEARTIE ATTACHMENT BETWEEN FR 26 AND FR 37.1 FROMSTR 13 TO STR 31 LH/RH, EXTERNAL SURFACE.22600 FC 7800 FC A330-200ORA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 18EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532153-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEOUTFLOW VALVE DOUBLER EXTERNAL SURFACE,BETWEEN FR 32 AND FR 33, FROM STR 45 TO STR 49,LH ONLY.13900 FC 7400 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532153-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEOUTFLOW VALVE DOUBLER EXTERNAL SURFACE,BETWEEN FR 32 AND FR 33, FROM STR 45 TO STR 49,LH ONLY.31600 FC 30000 FC GROUP 32EORGROUP 33E532154-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AT SPOT LIGHT CUT-OUT, BETWEEN- FR 27 AND FR 28 AND BETWEEN- FR 30 AND FR 31,- FROM STR 24 TO STR 26, LH/RH25900 FC 5500 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532155-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN ANDDOUBLER AT PRESSURE RELIEF VALVE CUTOUT,BETWEEN FR 24 AND FR 25, FROM STR 26 TO STR 30,LH ONLY.17100 FC 5300 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532156-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39700 FCOR118900 FH4000 FCOR12000 FHGROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 19EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532156-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39700 FCOR118900 FH3800 FCOR11500 FHGROUP 33APRE 46636ORGROUP 33BPRE 46636ORGROUP 33CPRE 46636ORGROUP 33DPRE 46636532156-01-04TASK DELETED IN ISSUE 18532157-01-02 832 842SIDEWALL LININGINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 31, FROM STR 9 TOSTR 15, LH/RH.38800 FC 15900 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532158-01-02 833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39700 FCOR118900 FH4000 FCOR12000 FHGROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532158-01-03TASK DELETED IN ISSUE 18532164-01-01TASK DELETED IN ISSUE 18532165-01-02 831 841CEILING PANELSLININGINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT AT STR 9, BETWEEN FR 31AND FR 37.1.35800 FC 3400 FC GROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532165-01-03TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 20EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY532166-01-03 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 18 AND FR 38FROM STR 6 TO CROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-034500 FC 4500 FC A330-200ORA330-300532166-02-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 18 AND FR 38 FROM STR 6 TOCROWN CENTER LINE, LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-036900 FC 6900 FC A330-200ORA330-300532182-01-01 835LININGNOTE1SPECIAL DETAILED INSPECTION OF FRAME ANDFRAME COUPLING FROM FR 20 TO FR 26/28 AT STR 21RH13900 FC 3200 FC A330-200F532183-01-01 835LININGNOTE1SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAND CIRCUMFERENTIAL SPLICE AT FR 31 BETWEENSTR 5 AND CROWN 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 BELLYFAIRING SEALING LIP ATTACHMENT FROM FRAME 37.1TO 38 AND FROM FRAME 53.6 TO 56.16400 FC 4800 FC ALL533009-01-01 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30700 FCOR92100 FH14700 FCOR44200 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 21EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533009-01-02 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-02NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32800 FCOR115100 FH12100 FCOR42500 FHGROUP 32APRE 49202PRE 52911ORGROUP 32APOST 50755PRE 56001533009-01-03 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-03NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86100 FH10700 FCOR32300 FHGROUP 33DPRE 49202PRE 52911533009-01-04 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-04NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88300 FH10900 FCOR32800 FHGROUP 33CPRE 49202PRE 52911A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 22EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533009-02-01 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30700 FCOR92100 FH4900 FCOR14700 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911533009-02-02 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-02NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32800 FCOR115100 FH4050 FCOR14100 FHGROUP 32APRE 49202PRE 52911ORGROUP 32APOST 50755PRE 56001533009-02-03 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-03NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86100 FH3600 FCOR10700 FHGROUP 33DPRE 49202PRE 52911A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 23EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533009-02-04 251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-04NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88300 FH3650 FCOR10900 FHGROUP 33CPRE 49202PRE 52911533010-01-01 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30700 FCOR92100 FH4150 FCOR12400 FHGROUP 33AORGROUP 33BR 533010-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32800 FCOR115100 FH3400 FCOR12000 FHGROUP 32APRE 49202ORGROUP 32APOST 50755533010-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86100 FH3000 FCOR9100 FHGROUP 33DPRE 49202533010-01-04 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88300 FH3050 FCOR9200 FHGROUP 33CPRE 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 24EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533012-01-01 261CC 262CCOVERHEAD STOWAGEBINSNOTE 1RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROMSTRINGER 4 TO 5, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31400 FCOR94300 FH7850 FCOR23600 FHGROUP 33APRE 52911533012-02-01 261CC 262CCOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROMSTRINGER 4 TO 5, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31400 FCOR94300 FH2450 FCOR7400 FHGROUP 33APRE 52911533013-01-02TASK DELETED IN ISSUE 18533013-01-03TASK DELETED IN ISSUE 18533013-01-04TASK DELETED IN ISSUE 18533014-01-01 734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20FASTENERS AFT OF FRAME 47 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR96000 FH7450 FCOR24300 FHGROUP 33AORGROUP 33BPRE45307S13490533014-01-02 734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20FASTENERS AFT OF FRAME 47 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29500 FCOR96400 FH7500 FCOR24500 FHGROUP 32APRE45307S13490A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 25EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533016-01-01 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31500 FCOR94600 FH4200 FCOR13700 FHGROUP 33C533016-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR92500 FH4100 FCOR13400 FHGROUP 33D533016-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29600 FCOR88800 FH4100 FCOR13400 FHGROUP 33E533018-01-01 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31900 FCOR111900 FH4750 FCOR16700 FHGROUP 32APRE 49202533018-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27800 FCOR83600 FH4200 FCOR12700 FHGROUP 33DPRE 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 26EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533018-01-03 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28500 FCOR85700 FH4250 FCOR12800 FHGROUP 33CPRE 49202533021-01-01 734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED9000 FCOR29540 FH6000 FCOR19600 FHGROUP 33APOST 45307ORGROUP 33BPOST 45307533021-01-02 734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8350 FCOR27500 FH5550 FCOR18300 FHGROUP 32APOST 45307ORGROUP 33CORGROUP 33D533021-01-03 734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8650 FCOR28300 FH5750 FCOR18900 FHGROUP 32EORGROUP 33E533103-02-01 N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, SKIN PANEL RIVETING ON FR.40 FROMSTRINGER 17 TO 19, LH/RH.15100 FC 7330 FC GROUP 33APRE45749S13894A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 27EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533104-01-03 ANTICOLLISION LIGHT:LENS 7LVADF: LENSES 2RP1 &SEAL AND 2RP2 & SEALDETAILED INSPECTION OF FUSELAGE SKIN 50 MMAROUND:- UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 ANDFR.43- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEENFR.48 AND FR.49 AND BETWEEN FR.52 & FR.53,BETWEEN STRINGER 1 LH AND STRINGER 1 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37900 FCOR113900 FH5050 FC GROUP 33AORGROUP 33B533105-01-02TASK DELETED IN ISSUE 18533106-01-02 N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR91100 FH7500 FCOR24500 FHGROUP 33AORGROUP 33B533106-01-03 N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37700 FCOR132100 FH10900 FCOR38400 FHGROUP 32A533107-01-03 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17300 FCOR52100 FH11500 FCOR37600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 28EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533107-01-04 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15600 FCOR54800 FH10200 FCOR36000 FHGROUP 32APRE 49202533107-01-05 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14300 FCOR43100 FH9600 FCOR31400 FHGROUP 33DPRE 49202533107-01-06 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22200 FCOR66700 FH10000 FCOR32900 FHGROUP 33E533107-01-07 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26300 FCOR92200 FH11300 FCOR39800 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 29EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533107-01-08 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14700 FCOR44200 FH9800 FCOR32100 FHGROUP 33CPRE 49202533107-01-09 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26100 FCOR91300 FH10200 FCOR36000 FHGROUP 32APOST 49202533107-01-10 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71700 FH9600 FCOR31400 FHGROUP 33DPOST 49202533107-01-11 LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24500 FCOR73600 FH9800 FCOR32100 FHGROUP 33CPOST 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 30EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533109-01-01 N/ASPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL LAP JOINT AT STRINGER 5 FROMFRAME 38 TO 53.3, AT STRINGER 13 FROM FRAME 38TO 47 AND AT STRINGER 22 FROM FRAME 43 TO 53.3,EXCLUDING 3 RIVET ROWSFORWARD AND AFT FRAME45 LEVEL, LH/RH.33800 FC 10200 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533112-01-01 N/ASPECIAL DETAILED INSPECITON OF FUSELAGEEXTERNAL STRUCTURE, LONGITUDINAL JOINT ATSTRINGER 39 AHEAD OF FRAME 53.2, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38500 FCOR125700 FH1700 FCOR5550 FHGROUP 33APOST 41897ORGROUP 33B533112-01-02 N/ASPECIAL DETAILED INSPECITON OF FUSELAGEEXTERNAL STRUCTURE, LONGITUDINAL JOINT ATSTRINGER 39 AHEAD OF FRAME 53.2, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35700 FCOR116800 FH1600 FCOR5200 FHGROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533113-01-04 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13600 FCOR41000 FH7900 FCOR25800 FHGROUP 33AORGROUP 33B533113-01-05 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED9300 FCOR28000 FH6100 FCOR19900 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 31EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533113-01-06 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11000 FCOR38700 FH6900 FCOR24100 FHGROUP 32E533113-01-07 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12800 FCOR38600 FH7500 FCOR24500 FHGROUP 33D533113-01-08 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14000 FCOR49200 FH8000 FCOR28100 FHGROUP 32A533113-01-09 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13200 FCOR39700 FH7650 FCOR25000 FHGROUP 33C533113-01-10 N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.11900 FC 7770 FC A330-200F533114-01-03 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25400 FCOR76300 FH25400 FCOR76300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 32EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533114-01-04 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18900 FCOR56800 FH18900 FCOR56800 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533114-01-06 251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20600 FCOR72400 FH20600 FCOR72400 FHGROUP 32APRE 49202533115-01-04 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16500 FCOR49700 FH5800 FCOR19000 FHGROUP 33AORGROUP 33B533115-01-05 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13600 FCOR41000 FH4850 FCOR15800 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533115-01-06 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16700 FCOR50100 FH4700 FCOR15500 FHGROUP 33E533115-01-07 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19700 FCOR69200 FH5300 FCOR18700 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 33EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533115-01-08 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14900 FCOR52200 FH5150 FCOR18100 FHGROUP 32APRE 49202533115-01-09 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.13000 FC 8500 FC A330-200F533115-01-10 251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17900 FCOR53800 FH4850 FCOR15800 FHGROUP 32APOST 49202ORGROUP 33CPOST 49202ORGROUP 33DPOST 49202533124-01-02TASK DELETED IN ISSUE 18533125-01-01 734 744GENERAL VISUAL INSPECTION OF FORWARD FACE OFFR 53.2 PRESSURE BULKHEAD INCLUDING THEATTACHMENT AREA OF THE CLG TRUNNION FITTINGS.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.1500 FC 1500 FC A330-200ORA330-300533126-01-03 734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED4050 FCOR13200 FH4050 FCOR13200 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 34EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533126-01-05 734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED4000 FCOR13100 FH4000 FCOR13100 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533126-01-06 734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED5300 FCOR17300 FH5300 FCOR17300 FHGROUP 32EORGROUP 33E533127-03-01 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED4000 FCOR13100 FH4000 FCOR13100 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533127-03-02 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACENOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED4050 FCOR13200 FH4050 FCOR13200 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 35EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533127-03-03 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED5300 FCOR17300 FH5300 FCOR17300 FHGROUP 32EORGROUP 33E533127-03-04 FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.19000 FC 19000 FC A330-200F533137-01-01TASK DELETED IN ISSUE 18533137-01-02TASK DELETED IN ISSUE 18533138-01-02 FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FLOOR BEAM INBOARDFLANGE AT Y=1959, AT FR48 LEVEL LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24600 FCOR80400 FH23900 FCOR78200 FHGROUP 33APOSTMSB 53-3013533145-01-03 197AT 197HB 198AT198HBSPECIAL DETAILED INSPECTION OF FUSELAGELONGITUDINAL BUTT JOINT ATSTRINGER 31 LEVELFROM FRAME 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 ATSTRINGER 31 LEVELFROM FRAME 53.3 TO FRAME 54, LH/RH.24700 FC 6150 FC GROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202R 533151-01-01 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21300 FCOR64100 FH13500 FCOR44300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 36EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYR 533151-01-02 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17600 FCOR52900 FH10500 FCOR34300 FHGROUP 33CORGROUP 33DORGROUP 33ER 533151-01-03 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19200 FCOR67300 FH11900 FCOR41700 FHGROUP 32AORGROUP 32E533152-01-01 151GW152 GWACT IFINSTALLEDSPECIAL DETAILED INSPECTION OF INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31AT FILLET FAIRINGLEVEL, LH/RH29400 FC 7050 FC GROUP 33APRE 40379PRE 46202ORGROUP 33BPRE 40379PRE 46202533152-01-02 151GW152 BXACT IFINSTALLEDLDMCR IFINSTALLEDSPECIAL DETAILED INSPECTION OF INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31AT FILLET FAIRINGLEVEL, LH/RH29400 FC 7050 FC GROUP 33APOST 40379PRE 46202ORGROUP 33BPOST 40379PRE 46202533152-01-03 151HX152 HXLDL IFINSTALLEDSPECIAL DETAILED INSPECTION OF INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT STR31AT FILLET FAIRINGLEVEL, LH/RH29400 FC 7050 FC GROUP 33APOST 46202ORGROUP 33BPOST 46202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 37EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533152-01-04 151GW 152GWACT IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGER 31,INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLETFAIRING LEVEL, LH/RH.24700 FC 6150 FC GROUP 32APRE 40379PRE 46202ORGROUP 33CPRE 40379PRE 46202ORGROUP 33DPRE 40379PRE 46202533152-01-05 151GW 152BXACT IF INSTALLEDLD-MCR IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGER 31,INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLETFAIRING LEVEL, LH/RH.24700 FC 6150 FC GROUP 32APOST 40379PRE 46202ORGROUP 33CPOST 40379PRE 46202ORGROUP 33DPOST 40379PRE 46202R 533152-01-06 151HX 152HXLDL IF INSTALLEDSPECIAL DETAILED INSPECTION OF STRINGER 31,INTERNALFUSELAGE, BETWEEN FR 53.7 AND FR 53.8 AT FILLETFAIRING LEVEL, LH/RH.24700 FC 6150 FC GROUP 32APOST 46202PRE 49202ORGROUP 33CPOST 46202PRE 49202ORGROUP 33DPOST 46202PRE 49202533154-01-04 CABIN FLOOR PANELSGALLEYSTOILETSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO53.1, LH/RH.12100 FC 8050 FC GROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 38EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533154-01-05 CABIN FLOOR PANELSGALLEYSTOILETSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, RIVET ROWS AT SHEAR PANELS ANDLONGITUDINAL BEAMS JUNCTION, FROM FRAME 48 TO53.1, LH/RH.20000 FC 13300 FC GROUP 33BORGROUP 32APRE 49202ORGROUP 32APOST 50755ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533154-01-06TASK DELETED IN ISSUE 18533155-01-01 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36100 FCOR118000 FH12700 FCOR41700 FHGROUP 32APRE 49202533155-01-02 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29000 FCOR94800 FH10400 FCOR33900 FHGROUP 33AORGROUP 33B533155-01-03 251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35600 FCOR116500 FH12600 FCOR41300 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533156-01-01 822LININGNOTE 1LD-MCR IF INSTALLEDPOST 46678: LDLTOILETS ANDFURNISHINGSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONSBETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO54, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30400 FCOR99400 FH6500 FCOR21300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 39EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533156-01-02 822LD-MCR IF INSTALLEDOR POST 46678 LDLTOILETS ANDFURNISHINGSLININGNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNALSTRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEENSTRINGERS32 AND 33 AT FRAMES 53.3 TO 54, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34800 FCOR113900 FH7500 FCOR24500 FHGROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533162-01-02 734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 40FASTENERS FORWARD AND AFT FR. 48 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16300 FCOR53400 FH9900 FCOR32500 FHGROUP 33AORGROUP 33BPRE 43852533164-01-03 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19200 FCOR62900 FH11900 FCOR39100 FHGROUP 32A533164-01-04 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24500 FCOR80200 FH14400 FCOR47200 FHGROUP 32EORGROUP 33E533164-01-06 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25000 FCOR81700 FH14100 FCOR46300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 40EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533164-01-07 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19300 FCOR63100 FH12000 FCOR39200 FHGROUP 33CORGROUP 33D533164-01-08 734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11400 FCOR37500 FH10200 FCOR33300 FHGROUP 33APOST 43904533179-01-02TASK DELETED IN ISSUE 18533180-01-03 N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27300 FCOR96000 FH8400 FCOR29600 FHGROUP 32A533180-01-04 N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20400 FCOR61700 FH4900 FCOR14900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 41EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533180-01-05 N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34600 FCOR104400 FH6100 FCOR18400 FHGROUP 33CORGROUP 33D533181-01-03 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27700 FCOR97300 FH14200 FCOR49800 FHGROUP 32A533181-01-04 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20700 FCOR62400 FH8500 FCOR25800 FHGROUP 33AORGROUP 33B533181-01-05 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35400 FCOR106700 FH9400 FCOR28400 FHGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 42EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYR 533181-01-06 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30100 FCOR90800 FH14000 FCOR42200 FHGROUP 33ER 533181-01-07 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR98800 FH15000 FCOR52500 FHGROUP 32E533187-01-01 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26100 FCOR91500 FH8500 FC GROUP 32AORGROUP 32E533187-01-02 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24800 FCOR74400 FH8000 FC GROUP 33AORGROUP 33B533187-01-03 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20900 FCOR62900 FH7150 FC GROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 43EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533187-01-05 CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19900 FCOR59900 FH7000 FC GROUP 33E533192-01-01TASK DELETED IN ISSUE 18533193-01-01TASK DELETED IN ISSUE 18533194-01-04 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR60200 FH11400 FCOR35700 FHGROUP 33E533194-01-05 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR35800 FH6200 FCOR18500 FHGROUP 33ADOOR TYPE 1ORGROUP 33BDOOR TYPE 1533194-01-06 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR59700 FH15000 FCOR48900 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352533194-01-07 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR60200 FH7600 FCOR25000 FHGROUP 33ADOOR TYPE APOST 42352PRE 41848ORGROUP 33BDOOR TYPE APOST 42352PRE 41848A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 44EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533194-01-08 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26000 FCOR78200 FH7400 FCOR24100 FHGROUP 33ADOOR TYPE APOST 41848ORGROUP 33BDOOR TYPE APOST 41848533194-01-09 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR84100 FH10700 FCOR37500 FHGROUP 32A533194-01-11 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17000 FCOR59700 FH6600 FCOR23100 FHGROUP 32E533194-01-12 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR72200 FH11000 FCOR33000 FHGROUP 33CORGROUP 33DR 533195-02-04 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR72200 FH11500 FCOR37500 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR35800 FH6200 FCOR18500 FHGROUP 33ADOOR TYPE 1ORGROUP 33BDOOR TYPE 1A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 45EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533195-02-06 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR59700 FH15000 FCOR48900 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352533195-02-07 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR60200 FH7600 FCOR25000 FHGROUP 33ADOOR TYPE APOST 42352PRE 41848ORGROUP 33BDOOR TYPE APOST 42352PRE 41848533195-02-08 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26000 FCOR78200 FH7400 FCOR24100 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,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR84100 FH10700 FCOR37500 FHGROUP 32A533195-02-11 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17000 FCOR59500 FH6600 FCOR23100 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 46EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY533195-02-12 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR72200 FH11000 FCOR33000 FHGROUP 33CORGROUP 33D533196-01-01 734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, CATENARIES SKINS AT JUNCTION WITHGANTRIES Y1456, OUTSIDE BOARD, AND Y1959, INSIDEBOARD, BETWEEN FR48 AND FR49 LH/RH.15300 FC 5200 FC A330-200FR 533197-01-01 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKINBETWEEN FR 53.3 AND FR 54 FROM STRINGER 6 LH TOSTRINGER 6 RH, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-02-014500 FC 4500 FC A330-200ORA330-300R 533197-02-01 N/ADETAILED INSPECTION OF FUSELAGE SKIN BETWEENFR 53.3 AND FR 54 FROM STRINGER 6 LH TO STRINGER6 RH, EXTERNAL SURFACE.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 533197-01-016900 FC 6900 FC A330-200ORA330-300534102-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 58 FROM STRINGERS 13 TO CROWNCENTER LINE, EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32100 FCOR96100 FH11600 FCOR34900 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534102-01-04TASK DELETED IN ISSUE 18534102-01-05TASK DELETED IN ISSUE 18534104-01-04TASK DELETED IN ISSUE 18534104-01-05TASK DELETED IN ISSUE 18534104-01-06TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 47EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534104-01-08 833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROMSTRINGERS 4 TO 6, STRINGERS 12 TO 14 ANDSTRINGERS 21 TO 22, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8800 FCOR26500 FH8800 FCOR26500 FHGROUP 33APRE 43996ORGROUP 33BPRE 43996ORGROUP 33CPRE 43996ORGROUP 33DPRE 43996534105-01-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37300 FCOR112400 FH12200 FCOR36800 FHGROUP 33APRE 40556ORGROUP 33BPRE 40556534105-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31700 FCOR95600 FH19000 FCOR57000 FHGROUP 32AORGROUP 33APOST 40556ORGROUP 33BPOST 40556ORGROUP 33CPOST 40556ORGROUP 33DPOST 40556534105-01-05TASK DELETED IN ISSUE 18534105-01-06 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24900 FCOR86900 FH16500 FCOR57700 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 48EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534107-01-02 833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3TO STR 7, AND STR 11 TO STR 13, AT INTERSECTIONOF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR101700 FH16700 FCOR49900 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534107-01-03TASK DELETED IN ISSUE 18534107-01-04 833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3TO STR 7, AND STR 11 TO STR 13, AT INTERSECTIONOF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24900 FCOR86900 FH13800 FCOR48200 FHGROUP 32ER 534108-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS ATFR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31700 FCOR111100 FH25400 FCOR88800 FHA330-200ORA330-300R 534110-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80FROMSTR 6 TO STR 13 LH/RH, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31700 FCOR111100 FH25400 FCOR88800 FHA330-200ORA330-300534120-01-02TASK DELETED IN ISSUE 18534120-01-03TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 49EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534120-01-04 N/ADETAILED INSPECTION OF FUSELAGE SKIN ANDVISIBLE PART OF WINDOW FORGINGS BETWEEN FR53.8 AND FR 73 AND BETWEEN STRINGERS 18 AND 22LH/RH, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19400 FCOR68100 FH19400 FCOR68100 FHGROUP 32E534124-01-02TASK DELETED IN ISSUE 18534124-02-02TASK DELETED IN ISSUE 18534126-01-02 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 54 AND FR 80FROM STR 26 TO BOTTOM CENTER LINE, LH/RH,INCLUDING SKIN SPLICES AND LAP JOINTS ANDINCLUDING THE LOWER, UNCOVERED AREA OF SKINAFT OF THE BELLY FAIRING AND FWD OF FR 54NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-02-022250 FC 2250 FC A330-200ORA330-300534126-02-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 26 TOBOTTOM CENTER LINE, LH/RH, INCLUDING SKINSPLICES AND LAP JOINTS AND INCLUDING THELOWER, UNCOVERED AREA OFSKIN AFT OF THEBELLY FAIRING AND FWD OF FR 54NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534126-01-026900 FC 6900 FC A330-200ORA330-300534131-01-02 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10500 FCOR36900 FH10500 FCOR36900 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 50EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534131-01-03 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10500 FCOR31300 FH10500 FCOR31300 FHGROUP 33E534131-01-04 833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10500 FCOR36900 FH10500 FCOR36900 FHGROUP 32E534132-02-01 833 843SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT, STRUCTUREUNDERNEATH THE SCUFF PLATE LH/RH.22800 FC 10500 FC A330-200ORA330-300534132-02-02TASK DELETED IN ISSUE 18534132-02-03TASK DELETED IN ISSUE 18534135-01-01TASK DELETED IN ISSUE 18534136-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGE SKINOF AFT CARGO COMPARTMENT DOOR CUT-OUT ATUPPER REAR AND LOWER FORWARD CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22800 FCOR68600 FH6000 FCOR18100 FHGROUP 33APRE 41045ORGROUP 33BPRE 41045534137-01-02TASK DELETED IN ISSUE 18534137-01-03TASK DELETED IN ISSUE 18534139-01-04 822GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR 59A AND 65) AS FAR AS VISIBLE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17300 FCOR52100 FH17300 FCOR52100 FHA330-200ORA330-300534140-02-02 822GENERAL VISUAL INSPECTION OF LOCK FITTINGS OFAFT CARGO COMPARTMENT DOOR AT 10 POSITIONSBETWEEN FR 59A AND FR 65.5900 FC 5900 FC A330-200ORA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 51EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534143-01-02 N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED5500 FCOR19200 FH5500 FCOR19200 FHGROUP 32A534143-01-03 N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8000 FCOR24000 FH8000 FCOR24000 FHGROUP 33E534143-01-04 N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8500 FCOR29800 FH8500 FCOR29800 FHGROUP 32E534143-01-06 N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED5300 FCOR16100 FH5300 FCOR16100 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534144-01-02 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT STRUCTUREUNDERNEATH SCUFF PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23400 FCOR70600 FH5300 FCOR16100 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534144-01-03TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 52EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534144-01-04 823SCUFF PLATEDETAILED INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT STRUCTUREUNDERNEATH SCUFF PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28300 FCOR98900 FH8500 FCOR29800 FHGROUP 32E534146-01-02TASK DELETED IN ISSUE 18534148-01-02 ANTENNADETAILED INSPECTION OF SKIN AROUND VHF 3ANTENNA CUT-OUT BETWEEN FR 56 AND FR 57 FROMSTRINGERS 2 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25700 FCOR77000 FH10200 FCOR31000 FHGROUP 33AORGROUP 33B534148-01-03TASK DELETED IN ISSUE 18534148-01-04TASK DELETED IN ISSUE 18534149-01-02 823GENERAL VISUAL INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR 67 AND FR 69) AS FAR ASVISIBLE.3600 FC 3600 FC A330-200ORA330-300534150-01-02TASK DELETED IN ISSUE 18534150-01-03 823LININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS OF CARGO FLOOR ATTACHMENT FITTINGS,FROM FR 58 TO FR 64 LH, BETWEEN STR 39 AND STR45, FROM FR 65 TO FR 69 LH, BETWEEN STR 41 ANDSTR 50.27900 FCOR83800 FH7900 FCOR23700 FHA330-200F534150-01-04TASK DELETED IN ISSUE 18534150-01-05 823LININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS OF CARGO FLOOR ATTACHMENT FITTINGS,FROM FR 54 TO FR 64 LH AND FROM FR 54 TO FR 58RH, BETWEEN STR 39 AND STR 45 FROM FR 65 TO FR69 LH, BETWEEN STR 41 AND STR 50.29400 FC 12700 FC A330-200POST 43984ORA330-300POST 43984A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 53EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534150-01-06 823LININGSNOTE 1DETAILED INSPECTION OF FRAMES AT UPPER RUNOUTS OF CARGO FLOOR ATTACHMENT FITTINGS,FROM FR 54 TO FR 64 LH AND FROM FR 54 TO FR 58RH, BETWEEN STR 39 AND STR 45 FROM FR 65 TO FR69 LH, BETWEEN STR 41 AND STR 50.15500 FC 12700 FC A330-200PRE 43997PRE 43984ORA330-300PRE 43997PRE 43984534151-01-01TASK DELETED IN ISSUE 18534151-01-02TASK DELETED IN ISSUE 18534151-01-03 833 843DOOR FRAME LININGDETAILED INSPECTION OF WEB OF FUSELAGE DOORFRAME 73A, FROM CABIN FLOOR TO STRINGER 11,LH/RH.12600 FC 12600 FC GROUP 33APRE 44204 PRE44975 ORGROUP 33BPRE 44204 PRE44975534152-01-01 833 843SIDEWALL LININGSNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE FROM FR 60 TO FR 66 AND FROM STR 18TO STR 23 RH IN FRAME COUPLING AREA.20000 FC 8000 FC GROUP 33APRE 44203ORGROUP 33BPRE 44203534153-01-01 162ZW 823NOTE 1DETAILED INSPECTION OF WEB OF FR 73A BELOWCABIN FLOOR, BETWEEN STR 26 AND 26X LH/RH.20000 FC 8000 FC GROUP 33APRE 44989PRE 44043ORGROUP 33BPRE 44989PRE 44043534154-01-02TASK DELETED IN ISSUE 18534154-01-03 833 843LININGINSULATIONDETAILED INSPECTION OF INTERNAL STRUCTURE OFTORSION BOX, INCLUDING SKIN AND SPLICE PLATE,BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 ANDFR 76, LH/RH.20000 FC 8000 FC A330-200POST 44680ORA330-300POST 44680534154-01-04 833 843LININGINSULATIONDETAILED INSPECTION OF INTERNAL STRUCTURE OFTORSION BOX, INCLUDING SKIN AND SPLICE PLATE,BETWEEN STR 9 AND STR 11 AND BETWEEN FR 73 ANDFR 76, LH/RH.11800 FC 9700 FC A330-200PRE 44680ORA330-300PRE 44680A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 54EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534155-01-02 833 843LININGINSULATIONSPECIAL DETAILED INSPECTION OF TORSION BOXLONGITUDINAL BEAM ADJACENT TO RUNOUT OFCORNER DOUBLER BETWEEN FR 73A AND FR 74,LH/RH.20000 FC 8000 FC A330-200ORA330-300534156-01-02 822LININGCARGO FLOOR PANELSINSULATIONDETAILED INSPECTION OF INTERNAL STRUCTUREBELOW AFT CARGO COMPARTMENT DOOR CUT-OUTBETWEEN FR 59 AND 67, FROM CARGO FLOOR LEVELTO STR 47 RH.30600 FC 30600 FC GROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534164-01-01TASK DELETED IN ISSUE 18534165-01-01 162ZW 823NOTE 1DETAILED INSPECTION OF WEB OF FR 75A, BELOWCABIN FLOOR, BETWEEN STR 26 AND STR 26X, LH/RH.20000 FC 8000 FC GROUP 33APRE 46866PRE 43517ORGROUP 33BPRE 46866PRE 43517534166-01-02TASK DELETED IN ISSUE 18534166-01-03 ANTENNASPECIAL DETAILED INSPECTION OF SKIN AROUNDVHF2 ANTENNA CUT-OUT BETWEEN FR 54 AND FR 55,FROM STR 51 TO STR 52, LH.22000 FC 18000 FC GROUP 32APOST 46849PRE 48442534177-01-03 N/AGENERAL VISUAL INSPECTION OF FUSELAGE SKINEXTERNAL SURFACE BETWEEN FR 54 AND FR 80FROM STR 6 TO CROWN CENTER LINE, EXLUDINGAREA UNDER VERTICAL STABILIZER FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-034500 FC 4500 FC A330-200ORA330-300534177-02-03 N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE BETWEEN FR 54 AND FR 80 FROM STR 6 TOCROWN CENTER LINE, EXLUDING AREA UNDERVERTICAL STABILIZER FAIRING.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 534177-02-036900 FC 6900 FC A330-200ORA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 55EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY534182-01-01 835LININGNOTE1SPECIAL DETAILED INSPECTION OF FRAME ANDFRAME COUPLING FROM FR 60 TO FR 64 BETWEENSTR 20X AND STR 23, RH.10300 FCOR30900 FH3600 FCOR10800 FHA330-200F534184-01-01 821LININGNOTE1DETAILED INSPECTION OF FRAME AND FRAMECOUPLING AT FR 67, STR 33 RH AND FR 69, STR 33 RH.23200 FCOR69600 FH7900 FCOR23700 FHA330-200F535103-01-02 312ARDETAILED INSPECTION OF REAR PRESSUREBULKHEAD AFT FACE, INCLUDING ATTACHMENT TOSKIN, BETWEEN STR 26 LH/RH AND CROWN CENTERLINE.16500 FC 7500 FC GROUP 32APRE 48980ORGROUP 33APRE 48980ORGROUP 33BPRE 48980ORGROUP 33CPRE 48980ORGROUP 33DPRE 48980535104-02-01 312ARGENERAL VISUAL INSPECTION OF REAR PRESSUREBULKHEAD AFT FACE, INCLUDING ATTACHMENT TOSKIN, BETWEEN STR 26 LH/RH AND BOTTOM CENTERLINE.5100 FC 5100 FC GROUP 32APRE 48980ORGROUP 33APRE 48980ORGROUP 33BPRE 48980ORGROUP 33CPRE 48980ORGROUP 33DPRE 48980545103-02-04 ENGINESPECIAL DETAILED INSPECTION OF PYLON PYRAMID,END OF ARMS AT ENGINE FORWARD MOUNT FITTING.18100 FC 18100 FC A330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 56EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545104-02-03 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13100 FCOR39300 FH1300 FCOR3900 FHGEGROUP 33AORGEGROUP 33B545104-02-04 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13500 FCOR40500 FH1300 FCOR3900 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.(2 FASTENER LOCATIONS/PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11700 FCOR35100 FH1200 FCOR3600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 57EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545104-02-12 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13000 FCOR45500 FH1300 FCOR4500 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13400 FCOR46900 FH1300 FCOR4500 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11600 FCOR40600 FH1200 FCOR4200 FHRRGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 58EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545108-03-01 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED6100 FCOR18600 FH6100 FCOR18600 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 32APRE48298ORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298ORPWGROUP 32APRE48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 59EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545108-03-03 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED5100 FCOR15600 FH5100 FCOR15600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298ORRRGROUP 32APRE48298545108-03-09 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED9300 FCOR27900 FH9300 FCOR27900 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 60EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545108-03-11 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED7200 FCOR21600 FH7200 FCOR21600 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545108-03-12 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED9100 FCOR31800 FH9100 FCOR31800 FHGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32APOST 48298ORPWGROUP 32E545108-03-14 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED7100 FCOR24800 FH7100 FCOR24800 FHRRGROUP 32APOST 48298ORRRGROUP 32E545108-04-19 415AL 416AR 425AL426AR 415BL 416BR425BL 426BRDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.7700 FC 7700 FC PWA330-200F545108-04-20 415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.7700 FC 7700 FC RRA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 61EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545111-02-01 ENGINEAFT ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF PYLON, ENGINEAFT ATTACHMENT UPPER BEAM AT RIB 9C.9500 FCOR98300 FH9500 FCOR98300 FHGE545129-01-03 454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26900 FCOR87900 FH8500 FCOR27700 FHPWGROUP 32AORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 32EORPWGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 62EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545129-01-04 454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26900 FCOR87900 FH8600 FCOR28100 FHRRGROUP 32AORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 32EORRRGROUP 33ER 545129-01-09 454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR100700 FH9600 FCOR31300 FHGEGROUP 32AORGEGROUP 33AORGEGROUP 33BORGEGROUP 32EORGEGROUP 33E545138-01-06TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 63EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545138-01-07 N/ADETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28500 FCOR85500 FH6100 FCOR18300 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545138-01-09TASK DELETED IN ISSUE 18545138-01-10TASK DELETED IN ISSUE 18545138-01-12 N/ADETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-12NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28200 FCOR98700 FH6000 FCOR21000 FHRRGROUP 32APRE 48298545138-02-03 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERALPANELS, AREA OF FASTENERS SECURING SUPPORTTO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-07.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28500 FCOR85500 FH12400 FCOR37200 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE48298545138-02-05TASK DELETED IN ISSUE 18545138-02-06TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 64EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545138-02-12 N/ASPECIAL DETAILED INSPECTION OF PYLON LATERALPANELS, AREA OF FASTENERS SECURING SUPPORTTO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-12NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28200 FCOR98700 FH12300 FCOR43000 FHRRGROUP 32APRE 48298545140-01-01 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (4750 FC OR 14250 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11200 FCOR33600 FH4800 FCOR14400 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 65EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-01-02 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (3770 FC OR 11310 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR36000 FH3800 FCOR11400 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304545140-01-03 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (3060 FC OR 9180 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8400 FCOR25200 FH3100 FCOR9300 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 66EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-01-06 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (4560 FC OR 22800 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11000 FCOR38400 FH4700 FCOR16400 FHGEGROUP 32AORGEGROUP 32EPRE 57304545140-01-07 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (3620 FC OR 18090 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11700 FCOR40900 FH3700 FCOR12900 FHRRGROUP 32AORRRGROUP 32EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 67EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-01-08 N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (2930 FC OR 14680 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8300 FCOR29000 FH3000 FCOR10500 FHPWGROUP 32AORPWGROUP 32EPRE 57304545140-02-01 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (7600 FC OR 22800 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11200 FCOR33600 FH7800 FCOR23400 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 68EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-02-02 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (7100 FC OR 21310 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR36000 FH7200 FCOR21600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304545140-02-03 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (5630 FC OR 16900 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8400 FCOR25200 FH5700 FCOR17100 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 69EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-02-06 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (7290 FC OR 36450 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11000 FCOR38400 FH7600 FCOR26500 FHGEGROUP 32AORGEGROUP 32EPRE 57304545140-02-07 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (6810 FC OR 34080 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11700 FCOR40900 FH7100 FCOR24800 FHRRGROUP 32AORRRGROUP 32EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 70EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-02-08 N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (5400 FC OR 27030 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8300 FCOR29000 FH5600 FCOR19600 FHPWGROUP 32AORPWGROUP 32EPRE 57304545140-02-09 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11200 FCOR33600 FH7800 FCOR23400 FHGEGROUP 33EPOST 57304545140-02-10 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR36000 FH7200 FCOR21600 FHRRGROUP 33EPOST 57304545140-02-11 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8400 FCOR25200 FH5700 FCOR17100 FHPWGROUP 33EPOST 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 71EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545140-02-12 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11000 FCOR38500 FH7600 FCOR26600 FHGEGROUP 32EPOST 57304545140-02-13 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED11700 FCOR40900 FH7100 FCOR24800 FHRRGROUP 32EPOST 57304545140-02-14 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8300 FCOR29000 FH5600 FCOR19600 FHPWGROUP 32EPOST 57304545140-02-15 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.7950 FC 5400 FC PWA330-200F545140-02-16 FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.11200 FC 6800 FC RRA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 72EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545142-02-01 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED7500 FCOR22500 FH7500 FCOR22500 FHGEGROUP 33AORGEGROUP 33BORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545142-02-02 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED6700 FCOR20100 FH6700 FCOR20100 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 73EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545142-02-05 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12400 FCOR37200 FH12400 FCOR37200 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33E545142-02-06 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10400 FCOR31200 FH10400 FCOR31200 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545142-02-07 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12200 FCOR42700 FH12200 FCOR42700 FHGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32APOST 48298ORPWGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 74EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545142-02-08 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10200 FCOR35700 FH10200 FCOR35700 FHRRGROUP32APOST 48298ORRRGROUP 32E545142-02-09 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED7400 FCOR25900 FH7400 FCOR25900 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE48298545142-02-10 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED6600 FCOR23100 FH6600 FCOR23100 FHRRGROUP 32APRE 48298545142-02-11 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.11700 FCOR35200 FH11700 FCOR35200 FHPWA330-200F545142-02-12 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.14000 FCOR42100 FH14000 FCOR42100 FHRRA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 75EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545143-02-04 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86100 FH3100 FCOR9300 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545143-02-09TASK DELETED IN ISSUE 18545143-02-10TASK DELETED IN ISSUE 18545143-02-13 453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-13NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29300 FCOR102500 FH3200 FCOR11200 FHRRGROUP 32APRE 48298545143-03-01 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS ANDMATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86100 FH8300 FCOR24900 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545143-03-04TASK DELETED IN ISSUE 18545143-03-05TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 76EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545143-03-13 453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS ANDMATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-13NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29300 FCOR102500 FH8500 FCOR29700 FHRRGROUP 32APRE 48298545146-03-01 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31200 FCOR93600 FH11100 FCOR33300 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 77EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545146-03-02 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24100 FCOR72300 FH7900 FCOR23700 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545146-03-03TASK DELETED IN ISSUE 18545146-03-04 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR91800 FH8700 FCOR26100 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545146-03-05TASK DELETED IN ISSUE 18545146-03-06 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30200 FCOR105700 FH8600 FCOR30100 FHRRGROUP 32APOST 48298RRGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 78EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545146-03-07 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR107800 FH11000 FCOR38500 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE 48298545146-03-08 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23800 FCOR83300 FH7800 FCOR27300 FHRRGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 79EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545146-04-01 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31200 FCOR93600 FH6500 FCOR19500 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545146-04-02 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24100 FCOR72300 FH4400 FCOR13200 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545146-04-03TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 80EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545146-04-04 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR91800 FH4400 FCOR13200 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545146-04-05TASK DELETED IN ISSUE 18545146-04-06 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30200 FCOR105700 FH4300 FCOR15000 FHRRGROUP 32APOST 48298ORRRGROUP 32E545146-04-07 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR107800 FH6500 FCOR22700 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 81EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545146-04-08 452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23800 FCOR83300 FH4400 FCOR15400 FHRRGROUP 32APRE 48298545150-02-01 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22000 FCOR67200 FH6100 FCOR18900 FHGEGROUP 32APRE 48298ORGEGROUP 33AORGEGROUP 33B545150-02-02 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR81900 FH6000 FCOR18300 FHPWGROUP 32APRE 48298ORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545150-02-06TASK DELETED IN ISSUE 18545150-02-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 82EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545150-02-08 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33300 FCOR99900 FH10500 FCOR31500 FHGEGROUP 33E545150-02-09 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR114100 FH10300 FCOR36000 FHGEGROUP 32APOST 48298ORGEGROUP 32E545150-02-10 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR101100 FH7800 FCOR24000 FHRRGROUP 32APRE 48298ORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545150-02-11 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36800 FCOR128800 FH11100 FCOR38800 FHPWGROUP 32APOST 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 83EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545150-02-13 452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.19400 FC 6900 FC PWA330-200F545150-02-14 452AL 462ALAIR DUCTPRE-COOLERRODSDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERALPANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37600 FCOR112800 FH11300 FCOR33900 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298545166-02-05TASK DELETED IN ISSUE 18545166-02-06TASK DELETED IN ISSUE 18545166-02-08TASK DELETED IN ISSUE 18545166-02-09TASK DELETED IN ISSUE 18545166-02-10TASK DELETED IN ISSUE 18545166-02-13TASK DELETED IN ISSUE 18545166-02-14TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 84EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545168-02-05 452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH8600 FCOR28100 FHGEGROUP 32AORGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EORGEGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 85EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545168-02-06 452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31600 FCOR103300 FH5500 FCOR17900 FHRRGROUP 32AORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EORRRGROUP 32E545168-02-08TASK DELETED IN ISSUE 18545168-02-09TASK DELETED IN ISSUE 18545168-02-10TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 86EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545168-02-13 452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25900 FCOR84600 FH4500 FCOR14700 FHPWGROUP 32AORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EORPWGROUP 32E545168-02-14TASK DELETED IN ISSUE 18545168-02-15 452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON)17000 FC 7900 FC PWA330-200F545168-02-16 452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON)17000 FC 4400 FC RRA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 87EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545174-02-03 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH7200 FCOR23500 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298ORGEGROUP 33AORGEGROUP 33B545174-02-06 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH6000 FCOR19600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 50003ORRRGROUP 33DPRE 50003A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 88EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545174-02-07 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH6200 FCOR21700 FHRRGROUP 32APRE 50003545174-02-09 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH7500 FCOR26200 FHPWGROUP 32APRE 48298ORGEGROUP 32APRE 48298545174-02-10 454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A17000 FC 10300 FC31100 FHPWA330-200F545174-02-11 454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A17000 FC 13300 FC39900 FHRRA330-200F545174-02-12 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH12400 FCOR37200 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 89EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545174-02-13 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH12300 FCOR43000 FHPWGROUP 32APOST 48298ORGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32E545174-02-14 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH9900 FCOR29700 FHRRGROUP 33CPOST 50003ORRRGROUP 33DPOST 50003ORRRGROUP 33E545174-02-15 PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR100000 FH9900 FCOR34600 FHRRGROUP 32APOST 50003ORRRGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 90EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545180-04-04 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18500 FCOR55500 FH14800 FCOR44400 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33E545180-04-05 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17500 FCOR52500 FH14000 FCOR42000 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33E545180-04-06 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17400 FCOR60900 FH13900 FCOR48600 FHPWGROUP 32AORPWGROUP 32E545180-04-07 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18300 FCOR64000 FH14700 FCOR51400 FHGEGROUP 32AORGEGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 91EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY545180-04-09 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)17000 FC 12900 FC PWA330-200F545180-04-10 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)17000 FC 17000 FC RRA330-200F545180-04-11 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18800 FCOR56400 FH15100 FCOR45300 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33E545180-04-12 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18700 FCOR65400 FH15000 FCOR52500 FHRRGROUP 32AORRRGROUP 32E551008-01-04 312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN SPANWISE SPLICES BETWEENFUSELAGE FAIRING LINES.27200 FCOR81600 FH4900 FCOR14700 FHA330-200F551008-01-06 312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN SPANWISE SPLICES BETWEENFUSELAGE FAIRING LINES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23100 FCOR69400 FH10600 FCOR32000 FHGROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 92EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY551008-01-07 312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN SPANWISE SPLICES BETWEENFUSELAGE FAIRING LINES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23100 FCOR69400 FH9800 FCOR29500 FHGROUP 33B551015-01-04 312ARGENERAL VISUAL INSPECTION OF HORIZONTALSTABILIZER CENTER BOX FRONT SPAR FORWARDFACE FROM RIB 3 LH TO RIB 3 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22700 FCOR68100 FH22700 FCOR68100 FHGROUP 33AORGROUP 33B551016-01-02TASK DELETED IN ISSUE 18551016-01-06 313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN REAR UPPERFLANGE JUST OUTBOARD OF RIB 3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32400 FCOR97400 FH31600 FCOR94800 FHGROUP 33A551016-01-07 313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN REAR UPPERFLANGE JUST OUTBOARD OF RIB 3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32400 FCOR97400 FH26300 FCOR79100 FHGROUP 33B551019-01-04 313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN INTERGRALFLANGE AT ATTACHMENT TO REAR SPAR WEB FROMRIB 3 LH TO RIB 3 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28800 FCOR100900 FH4400 FCOR15400 FHGROUP 32E551024-01-04 331 / 341BT, AT333 / 343AT, ABGENERAL VISUAL INSPECTION OF HORIZONTALSTABILIZER LATERAL BOX FRONT SPAR FORWARDFACE BETWEEN RIB 3 AND 4.16600 FCOR49800 FH8000 FCOR24000 FHA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 93EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYR 571102-01-01 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.15000 FCOR75400 FH5000 FCOR25100 FHGROUP 32APRE 49202PRE 52094ORGROUP 32APOST 50755PRE 52094R 571102-01-02 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.21500 FCOR107900 FH5000 FCOR25100 FHGROUP 32APOST 49202PRE 50755ORGROUP 32APRE 49202POST 52094ORGROUP 32APOST 50755POST 52094571102-01-03 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.17200 FCOR51600 FH6000 FCOR18100 FHGROUP 33APOST 44360PRE 52094ORGROUP 33BPOST 44360PRE 52094571102-01-04 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.16500 FCOR49700 FH5400 FCOR16200 FHGROUP 33CPRE 49202PRE 52094ORGROUP 33DPRE 49202PRE 52094571102-01-05 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.24200 FCOR72700 FH5550 FCOR16600 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 94EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571102-01-06 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.22400 FCOR112000 FH5140 FCOR25700 FHGROUP 32ER 571102-01-07 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.23700 FCOR71100 FH5400 FCOR16200 FHGROUP 33CPOST 49202ORGROUP 33CPRE 49202POST 52094ORGROUP 33DPOST 49202ORGROUP 33DPRE 49202POST 52094571102-01-08 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.24400 FCOR73200 FH6000 FCOR18100 FHGROUP 33APOST 44360POST 52094ORGROUP 33BPOST 44360POST 52094571102-01-09 821NOTE 1LININGAIR CONDITIONINGDUCTSDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FASTENER ON FRAME 40 FRONT FITTINGAT STRINGER 38 LEVEL, LH/RH.16300 FC 4600 FC A330-200F571103-01-03 191HB 192HB 821NOTE 1LININGAIR CONDITIONINGDUCTSFASTENER (2POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-03.15600 FCOR46900 FH6600 FCOR20000 FHGROUP 33APOST 44360PRE 50745ORGROUP 33BPOST 44360PRE 50745A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 95EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571103-01-04 191HB 192HB 821NOTE 1LININGAIR CONDITIONINGDUCTSFASTENER (2POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-04.14400 FCOR72000 FH6000 FCOR30200 FHGROUP 32APRE 49202PRE 50745571103-01-05 191HB 192HB 821NOTE 1LININGAIR CONDITIONINGDUCTSFASTENER (2POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-0515600 FCOR46800 FH6400 FCOR19300 FHGROUP 33DPRE 49202PRE 50745571103-01-06 191HB 192HB 821NOTE 1LININGAIR CONDITIONINGDUCTSFASTENER (2POSITIONS)SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-02-06.15800 FCOR47500 FH6500 FCOR19500 FHGROUP 33CPRE 49202PRE 50745571103-02-03 821NOTE 1LININGAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-0315600 FCOR46900 FH1450 FCOR4350 FHGROUP 33APOST 44360PRE 50745ORGROUP 33BPOST 44360PRE 50745A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 96EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571103-02-04 821NOTE 1LININGAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-04.14400 FCOR72000 FH930 FCOR4650 FHGROUP 32APRE 49202PRE 50745571103-02-05 821NOTE 1LININGAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-0515600 FCOR46800 FH990 FCOR2950 FHGROUP 33DPRE 49202PRE 50745571103-02-06 821NOTE 1LININGAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE IN AREA OF FASTENERS BETWEEN STR. 39AND 40, LH/RH.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 571103-01-06.15800 FCOR47500 FH1000 FCOR3000 FHGROUP 33CPRE 49202PRE 50745571104-01-01 191KB 192PBFASTENER TO BEREMOVED821131CX 131DX 132CX132DXSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 REAR FITTING WEBIN AREA OF FASTENER BETWEEN STR 38 AND STR 39,LH/RH.28100 FCOR84500 FH7100 FCOR21300 FHGROUP 33APRE 44360POST 52094ORGROUP 33BPRE 44360POST 52094571104-01-02 191KB 192PBFASTENER TO BEREMOVED821131CX 131DX 132CX132DXSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 REAR FITTING WEBIN AREA OF FASTENER BETWEEN STR 38 AND STR 39,LH/RH.16500 FCOR49600 FH7100 FCOR21300 FHGROUP 33APRE 44360PRE 52094ORGROUP 33BPRE 44360PRE 52094A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 97EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571104-01-03 191KB 192PBFASTENER TO BEREMOVED821131CX 131DX 132CX132DXSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 REAR FITTING WEBIN AREA OF FASTENER BETWEEN STR 38 AND STR 39,LH/RH.26100 FCOR78400 FH7100 FCOR21300 FHGROUP 33APOST 44360PRE 52094ORGROUP 33BPOST 44360PRE 52094R 571104-01-04 191KB 192PBFASTENER TO BEREMOVED821131CX 131DX 132CX132DXSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 REAR FITTING WEBIN AREA OF FASTENER BETWEEN STR 38 AND STR 39,LH/RH.19500 FCOR97800 FH5600 FCOR28000 FHGROUP 32APRE 49202PRE 52094ORGROUP 32APOST 50755PRE 52094571104-01-05 191KB 192PBFASTENER TO BEREMOVED821131CX 131DX 132CX132DXSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 REAR FITTING WEBIN AREA OF FASTENER BETWEEN STR 38 AND STR 39,LH/RH.23200 FCOR69600 FH6300 FCOR19000 FHGROUP 33CPRE 49202PRE 52094ORGROUP 33DPRE 49202PRE 52094571107-01-01 191QB 192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, DRAIN HOLES AT Y=2427BETWEEN STRINGERS 20 & 21, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35200 FCOR123400 FH5850 FCOR20400 FHGROUP 32A571107-01-03TASK DELETED IN ISSUE 18571107-01-04 191QB 192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, DRAIN HOLES AT Y=2427BETWEEN STRINGERS 20 & 21, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32100 FCOR105100 FH6500 FCOR21200 FHGROUP 33AORGROUP 33B571107-01-05TASK DELETED IN ISSUE 18571108-01-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 98EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571108-01-05 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, LOWER SKIN PANEL ANDSTIFFENERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38700 FCOR116200 FH8800 FCOR26500 FHGROUP 33AORGROUP 33B571108-01-06 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, LOWER SKIN PANEL ANDSTIFFENERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38600 FCOR135300 FH8200 FCOR28800 FHGROUP 32A571108-01-07TASK DELETED IN ISSUE 18571110-01-01 821NOTE 1LININGAIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 40 FRONT FITTINGFLANGE REINFORCING STRAP, 4 FASTENER HOLES ATSTR. 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 WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32700 FCOR98300 FH13600 FCOR41000 FHGROUP 33AORGROUP 33B571114-01-06 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26100 FCOR91500 FH12000 FCOR42000 FHGROUP 32APRE 49202ORGROUP 32APOST 50755A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 99EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571114-01-07 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28900 FCOR86900 FH12600 FCOR37900 FHGROUP 33DPRE 49202ORGROUP 33CPRE 49202571116-01-02 193DBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, FUEL LEVEL MAGNETICINDICATOR AREA BETWEEN STRINGERS 21 & 22, AT Y=-567.5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35200 FCOR123400 FH5800 FCOR20400 FHGROUP 32A571116-01-03TASK DELETED IN ISSUE 18571116-01-04 193DBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, FUEL LEVEL MAGNETICINDICATOR AREA BETWEEN STRINGERS 21 & 22, AT Y=-567.5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32100 FCOR105100 FH6500 FCOR21200 FHGROUP 33AORGROUP 33B571116-01-05TASK DELETED IN ISSUE 18571118-01-06 FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTORS AREAAT Y=-2230 BETWEEN STRINGERS 25 & 26, AND ATY=180 BETWEEN STRINGERS 27 & 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35200 FCOR123400 FH5800 FCOR20400 FHGROUP 32A571118-01-07 FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTORS AREAAT Y=-2230 BETWEEN STRINGERS 25 & 26, AND ATY=180 BETWEEN STRINGERS 27 & 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32100 FCOR105100 FH6500 FCOR21200 FHGROUP 33AORGROUP 33B571118-01-08TASK DELETED IN ISSUE 18571118-01-09TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 100EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571119-01-01 CABIN FLOOR PANELS,GALLEYS IF INSTALLEDSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAMS ABOVECWB, WEB HOLE AREA BETWEEN FRAMES 41 AND 42FROM Y=-1456 TO Y=1456.33000 FC 3100 FC GROUP 33AORGROUP 33BORGROUP 32APRE 49202ORGROUP 32APOST 50755ORGROUP 33DPRE 49202ORGROUP 33CPRE 49202571121-01-03 734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1959NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29600 FCOR89000 FH21600 FCOR64800 FHGROUP 33AORGROUP 33BORGROUP 32AORGROUP 33CORGROUP 33D571121-01-04 734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1960NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29700 FCOR89100 FH21600 FCOR64800 FHGROUP 33E571121-01-05 734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1961NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29900 FCOR104700 FH21600 FCOR75600 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 101EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571122-01-04TASK DELETED IN ISSUE 18571123-01-01 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28800 FCOR86400 FH11800 FCOR35600 FHGROUP 33APOST 49404ORGROUP 33BPOST 49404571123-01-02 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR80300 FH9900 FCOR29700 FHGROUP 33CPOST 49404ORGROUP 33DPOST 49404571123-01-03 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22900 FCOR80400 FH8300 FCOR29100 FHGROUP 32APOST 49404571123-01-04 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27400 FCOR82300 FH11500 FCOR34500 FHGROUP 33EPOST 49404571123-01-05 CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR83900 FH9600 FCOR33800 FHGROUP 32EPOST 49404571125-01-03 734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30200 FCOR98900 FH6400 FCOR21100 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 102EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571125-01-04 734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22300 FCOR78300 FH4200 FCOR14700 FHGROUP 32A571125-01-05 734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23500 FCOR76800 FH4300 FCOR14300 FHGROUP 33CORGROUP 33D571126-01-03 734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33600 FCOR100900 FH14300 FCOR43100 FHGROUP 33AORGROUP 33B571126-01-04 734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27500 FCOR96400 FH11500 FCOR40200 FHGROUP 32APRE 49202ORGROUP 32APOST 50755571126-01-05 734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29200 FCOR87800 FH12000 FCOR36200 FHGROUP 33DPRE 49202ORGROUP 33CPRE 49202571129-01-04 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX,CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38400 FCOR125600 FH13900 FCOR45400 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 103EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571130-01-03 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX, REAR SPAR, 30 MMAROUND MANHOLE CUTOUTS (2 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38400 FCOR125600 FH7900 FCOR26100 FHGROUP 33AORGROUP 33BR 571130-01-04 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX, REAR SPAR, 30 MMAROUND MANHOLE CUTOUTS (2 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37500 FCOR122600 FH7300 FCOR23900 FHGROUP 32APRE 49202ORGROUP 32APOST 50755ORGROUP 33DPRE 49202ORGROUP 33CPRE 49202571133-01-01 147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX, STRUTLUGS ON LONGITUDINALSTIFFENERS AND RODFITTING CONNECTIONS (63 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR112100 FH15900 FCOR54900 FHGROUP 32AORGROUP 33CORGROUP 33D571144-01-01 191HB 191QB 192HB192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX, LOWER SPLICE AT RIB 1, FIRST FASTENER ROWSON EACH SIDE OF RIB 1 DATUM AT STR.16, STR.20,STR.21 AND STR.25 TO 29 FOR INBOARD RIVET ROW,AND AT STR.11, STR.14, STR.18 TO 20 AND STR.23 TO28 FOR OUTBOARD RIVET ROW, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37900 FCOR113800 FH9700 FCOR29100 FHGROUP 33A571145-01-01 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31700 FCOR95300 FH7700 FCOR23100 FHGROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 104EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571145-01-03 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31500 FCOR110300 FH8400 FCOR29500 FHGROUP 32A571145-01-04 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31200 FCOR93800 FH8600 FCOR26000 FHGROUP 33E571145-01-05 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR107800 FH8200 FCOR28900 FHGROUP 32E571145-01-06 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32900 FCOR98900 FH8900 FCOR26900 FHGROUP 33CORGROUP 33D571145-01-07 147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.32000 FC 9100 FC A330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 105EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571146-02-04 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34200 FCOR102800 FH10000 FCOR30200 FHGROUP 33AORGROUP 33B571146-02-05 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29000 FCOR101700 FH8300 FCOR29200 FHGROUP 32A571146-02-06 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30400 FCOR91400 FH8400 FCOR25400 FHGROUP 33E571146-02-07 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29300 FCOR102800 FH8100 FCOR28600 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 106EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571146-02-08 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR92600 FH8700 FCOR26300 FHGROUP 33CORGROUP 33D571146-02-09 191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, 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 WINGBOX INTERNAL STRUCTURE, CENTER SPAR FITTINGFLANGE, RADIUS AREA AT FASTENERS 3 TO 4 LEVELAND FLANGE AT FASTENERS 3 TO 12, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21300 FCOR69600 FH6900 FCOR22600 FHGROUP 33A571153-01-01 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21400 FCOR70100 FH14800 FCOR48600 FHGROUP 33E571153-01-02 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20500 FCOR71900 FH14200 FCOR49800 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 107EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571153-01-03 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13600 FCOR44400 FH9450 FCOR30800 FHGROUP 33APOST 43577ORGROUP 33BPOST44440S13324571153-01-04 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19000 FCOR62200 FH14800 FCOR48600 FHGROUP 33CORGROUP 33DR 571153-01-05 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20700 FCOR67800 FH16600 FCOR54300 FHGROUP 33BPOST44440S13276ORGROUP 33BPOST44440S13090ORGROUP 33BPOST 44360571153-01-06 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18200 FCOR63800 FH14200 FCOR49800 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 108EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571153-01-07 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.11100 FC 11100 FC A330-200F571159-01-03 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29700 FCOR97000 FH9600 FCOR31500 FHGROUP 33AORGROUP 33B571159-01-04 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28000 FCOR91700 FH9200 FCOR30000 FHGROUP 32A571159-01-05 CABIN FLOOR PANELS SPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR92000 FH9200 FCOR30100 FHGROUP 33CORGROUP 33D571162-01-01 191HB 192HBSPECIAL DETAILED INSPECTION OF KEEL BEAMFITTING, TWO FASTENERS HOLES IN CONNECTION OFKEEL BEAM FITTING TO CWB BOTTOM PANEL AT STR.1LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12600 FCOR41200 FH7250 FCOR23800 FHGROUP 33APOST 43577POST 54459A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 109EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITYR 571163-01-01 191HB 192HBSPECIAL DETAILED INSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12000 FCOR39400 FH5800 FCOR19000 FHGROUP 33BPOST 56467ORGROUP 33CPOST 56467POST 44360ORGROUP 33DPOST 56467POST 44360ORGROUP 33EPOST 56467POST 49202PRE 55306ORGROUP 33EPOST 56467POST 49202PRE 55792R 571163-01-02 191HB 192HBSPECIAL DETAILED INSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED10900 FCOR35600 FH5250 FCOR17100 FHGROUP 32APOST 56467POST 44360ORGROUP 32EPOST 56467POST 49202PRE 55306ORGROUP 32EPOST 56467POST 49202PRE 55792571164-01-01 191HB 192HBDETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, KEEL BEAM FITTING ANGLE ANDDOUBLER AT FR 40, LH/RH.19600 FC 7400 FC A330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 110EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY571164-01-02 191HB 192HBDETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, KEEL BEAM FITTING ANGLE ANDDOUBLER AT FR 40, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19200 FCOR62900 FH7700 FCOR25200 FHGROUP 32EPOST 55306ORGROUP 32EPOST 55792ORGROUP 33EPOST 55306ORGROUP 33EPOST 55792571165-01-03 734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR, FILET RADIUS FROM Y=1959 TOY=2219 AND FROM Z=-1859.6 TO Z=-2073, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED12200 FCOR36700 FH7200 FCOR21800 FHGROUP 33APRE 43865ORGROUP 33BPRE 43865572001-02-01TASK DELETED IN ISSUE 18572001-02-03TASK DELETED IN ISSUE 18572001-02-04TASK DELETED IN ISSUE 18572002-01-05 454DL 454DR 454FL454FR 464DL 464DR464FL 464FRSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIBBAY 10-10ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR97900 FH6200 FCOR18800 FHGROUP 33APRE 43271ORGROUP 33BPRE 43271572002-01-08 454KL 454KR 454ML454MR 464KL 464KR464ML 464MRSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIBBAY 10-10ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR97900 FH6200 FCOR18800 FHGROUP 33APOST 43271ORGROUP 33BPOST 43271572003-01-04TASK DELETED IN ISSUE 18572003-01-06TASK DELETED IN ISSUE 18572003-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 111EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572004-02-01 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33500 FCOR117300 FH5800 FCOR20600 FHGROUP 32APRE 48437572004-02-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32800 FCOR98400 FH8400 FCOR25300 FHGROUP 33AORGROUP 33B572004-02-04 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32000 FCOR96100 FH5600 FCOR16800 FHGROUP 33CPRE 48437572004-02-05 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32000 FCOR96100 FH4400 FCOR13200 FHGROUP 33DPRE 48437572005-01-06 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25500 FCOR76600 FH4300 FCOR12900 FHGROUP 33CPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 112EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572005-01-07 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28500 FCOR100000 FH4300 FCOR15300 FHGROUP 32APRE 48437572005-01-08 541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR84500 FH8800 FCOR26400 FHGROUP 33APRE 41114ORGROUP 33BPRE 41114572005-01-09 541CB 641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR84500 FH8800 FCOR26400 FHGROUP 33APOST 41114ORGROUP 33BPOST 41114572005-01-12 541CB 641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINFORWARD OF REAR SPAR IN AREA MASKED BY MAINLANDINGGEAR REINFORCING PLATE INCLUDING ATTACHMENTTO REARSPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25500 FCOR76600 FH3300 FCOR10100 FHGROUP 33DPRE 48437572006-01-01TASK DELETED IN ISSUE 18572006-01-02TASK DELETED IN ISSUE 18572006-01-03TASK DELETED IN ISSUE 18572006-02-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 113EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572006-02-09 N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE MAIN LANDING GEARREINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35400 FCOR124100 FH7500 FCOR26400 FHGROUP 32APRE 48437572006-02-10 N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE MAIN LANDING GEARREINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29700 FCOR89300 FH6500 FCOR19600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572007-01-04TASK DELETED IN ISSUE 18572007-01-05TASK DELETED IN ISSUE 18572007-01-06TASK DELETED IN ISSUE 18572007-01-08TASK DELETED IN ISSUE 18572008-01-04TASK DELETED IN ISSUE 18572009-01-04 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29100 FCOR101900 FH5700 FCOR20200 FHGROUP 32APRE 48437572009-01-05 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27500 FCOR82700 FH5100 FCOR15300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 114EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572009-01-06 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27200 FCOR81700 FH5600 FCOR16800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572009-02-04 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29100 FCOR101900 FH15000 FCOR50000 FHGROUP 32APRE 48437572009-02-05 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27500 FCOR82700 FH9300 FCOR28000 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 115EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572009-02-06 454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27200 FCOR81700 FH14500 FCOR43600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572010-02-04TASK DELETED IN ISSUE 18572010-02-06TASK DELETED IN ISSUE 18572010-02-07TASK DELETED IN ISSUE 18572012-02-01 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35000 FCOR122700 FH5600 FCOR19900 FHGROUP 32APRE 48437572012-02-02 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27400 FCOR82300 FH7000 FCOR21000 FHGROUP 33AORGROUP 33B572012-02-03 FUEL PUMP FAIRINGS DETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34900 FCOR104800 FH5300 FCOR16100 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572012-02-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 116EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572013-03-01TASK DELETED IN ISSUE 18572013-03-02TASK DELETED IN ISSUE 18572013-03-03TASK DELETED IN ISSUE 18572013-03-04TASK DELETED IN ISSUE 18572014-02-02 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINTS AT SRINGER13 AND STRINGER 20 BETWEEN RIB 1 AND RIB 12EXCLUDING AREAS COVERED BY FAIRINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37200 FCOR111800 FH8200 FCOR24800 FHGROUP 33AORGROUP 33B572015-02-01TASK DELETED IN ISSUE 18572015-02-02TASK DELETED IN ISSUE 18572015-02-03TASK DELETED IN ISSUE 18572015-02-04TASK DELETED IN ISSUE 18572016-02-04TASK DELETED IN ISSUE 18572016-02-05TASK DELETED IN ISSUE 18572016-02-06TASK DELETED IN ISSUE 18572016-02-07TASK DELETED IN ISSUE 18572016-02-08 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN VISIBLE SURFACES OF FUEL PUMPAPERTURES BETWEEN RIB 2 AND RIB 4.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31900 FCOR95800 FH7800 FCOR23500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572016-02-09 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN VISIBLE SURFACES OF FUEL PUMPAPERTURES BETWEEN RIB 2 AND RIB 4.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27300 FCOR95600 FH7400 FCOR26000 FHGROUP 32APOST 48437ORGROUP 32E572016-02-12 FUEL PUMP FAIRINGS SPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN VISIBLE SURFACES OF FUEL PUMPAPERTURES BETWEEN RIB 2 AND RIB 4.26900 FCOR80900 FH17000 FCOR50000 FHA330-200F572018-01-05TASK DELETED IN ISSUE 18572018-01-06TASK DELETED IN ISSUE 18572018-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 117EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572018-01-08TASK DELETED IN ISSUE 18572018-01-09TASK DELETED IN ISSUE 18572018-01-10TASK DELETED IN ISSUE 18572018-01-11TASK DELETED IN ISSUE 18572018-01-12TASK DELETED IN ISSUE 18572019-01-05 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36200 FCOR127000 FH7900 FCOR27800 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 STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33200 FCOR99700 FH9800 FCOR29500 FHGROUP 33AORGROUP 33B572019-01-07TASK DELETED IN ISSUE 18572019-01-08TASK DELETED IN ISSUE 18572019-01-09TASK DELETED IN ISSUE 18572019-01-10TASK DELETED IN ISSUE 18572019-01-11 541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35600 FCOR106800 FH7400 FCOR22400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572019-01-12TASK DELETED IN ISSUE 18572021-03-02TASK DELETED IN ISSUE 18572022-01-04TASK DELETED IN ISSUE 17572022-01-05TASK DELETED IN ISSUE 17572022-01-06TASK DELETED IN ISSUE 17572022-01-07TASK DELETED IN ISSUE 17A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 118EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572023-02-03 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31500 FCOR110200 FH3900 FCOR13900 FHGROUP 32APRE 48437572023-02-04 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26300 FCOR79100 FH4100 FCOR12300 FHGROUP 33AORGROUP 33B572023-02-05 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR92400 FH3800 FCOR11500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572023-02-06TASK DELETED IN ISSUE 18572027-01-05 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36400 FCOR127500 FH9300 FCOR32700 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 119EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572027-01-06 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29000 FCOR87200 FH13200 FCOR39800 FHGROUP 33AORGROUP 33B572027-01-10 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35600 FCOR107000 FH9500 FCOR28500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572029-01-03TASK DELETED IN ISSUE 18572029-01-04TASK DELETED IN ISSUE 18572029-01-05TASK DELETED IN ISSUE 18572029-01-06TASK DELETED IN ISSUE 18572030-01-04TASK DELETED IN ISSUE 18572030-01-05TASK DELETED IN ISSUE 18572030-01-06TASK DELETED IN ISSUE 18572030-01-07TASK DELETED IN ISSUE 18572030-01-08TASK DELETED IN ISSUE 18572032-01-04 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15600 FCOR54700 FH10300 FCOR36000 FHGROUP 32APRE 48437572032-01-05 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15900 FCOR47300 FH10800 FCOR32500 FHGROUP 33APOST 46110PRE 43503ORGROUP 33BPOST 46110PRE 43503A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 120EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572032-01-06 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14400 FCOR43300 FH8300 FCOR24900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572032-01-07 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14400 FCOR43300 FH13300 FCOR39900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572032-01-08TASK DELETED IN ISSUE 18572032-01-09 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15600 FCOR54700 FH11300 FCOR39600 FHGROUP 32APOST 48437ORGROUP 32E572032-01-10TASK DELETED IN ISSUE 18572032-01-11TASK DELETED IN ISSUE 18572032-01-12 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18500 FCOR55600 FH10800 FCOR32500 FHGROUP 33APOST 43503ORGROUP 33BPOST 43503572033-01-04 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22400 FCOR78500 FH6900 FCOR24400 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 121EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572033-01-05 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22000 FCOR66000 FH9700 FCOR29100 FHGROUP 33AORGROUP 33B572033-01-06 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19900 FCOR59800 FH6700 FCOR20300 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572033-01-07TASK DELETED IN ISSUE 18572033-01-08 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19900 FCOR59800 FH10000 FCOR30000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572033-01-09 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22400 FCOR78500 FH8700 FCOR30600 FHGROUP 32APOST 48437ORGROUP 32E572034-01-04TASK DELETED IN ISSUE 18572034-01-05TASK DELETED IN ISSUE 18572034-01-06TASK DELETED IN ISSUE 18572034-01-07TASK DELETED IN ISSUE 18572035-01-04TASK DELETED IN ISSUE 18572035-01-05 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE FROM STRINGER 12 TO 19 ANDFROM RIB 4 TO RIB 8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33300 FCOR100100 FH10500 FCOR31600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 122EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572035-01-06TASK DELETED IN ISSUE 18572035-01-07TASK DELETED IN ISSUE 18572036-01-04TASK DELETED IN ISSUE 18572036-01-05TASK DELETED IN ISSUE 18572036-01-06TASK DELETED IN ISSUE 18572036-01-07TASK DELETED IN ISSUE 18572037-01-05 541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9AND TOP SKIN LOWER SURFACE AT ROOT JOINTFROM FRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31700 FCOR95200 FH14000 FCOR42100 FHGROUP 33AORGROUP 33B572039-01-04TASK DELETED IN ISSUE 18572039-01-05TASK DELETED IN ISSUE 18572039-01-06TASK DELETED IN ISSUE 18572039-01-07TASK DELETED IN ISSUE 18572040-01-04TASK DELETED IN ISSUE 18572040-01-05TASK DELETED IN ISSUE 18572040-01-06TASK DELETED IN ISSUE 18572040-01-07TASK DELETED IN ISSUE 18572043-01-04TASK DELETED IN ISSUE 18572043-01-05 573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30200 FCOR90800 FH8500 FCOR25700 FHGROUP 33AORGROUP 33B572043-01-06 573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39900 FCOR119800 FH13300 FCOR39900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572043-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 123EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572043-01-10 573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFTFACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38900 FCOR116900 FH8200 FCOR24700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572043-01-11 573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFTFACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37500 FCOR131500 FH7900 FCOR27700 FHGROUP 32APOST 48437572046-01-04 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR106200 FH7100 FCOR25000 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 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25100 FCOR75500 FH10800 FCOR32500 FHGROUP 33APOST 46111ORGROUP 33B572046-01-06TASK DELETED IN ISSUE 18572046-01-07 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28200 FCOR84600 FH7200 FCOR21800 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572046-01-08TASK DELETED IN ISSUE 18572046-01-09 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26900 FCOR94100 FH6900 FCOR24200 FHGROUP 32EORGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 124EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572046-01-10TASK DELETED IN ISSUE 18572046-01-11 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26100 FCOR78300 FH6100 FCOR18400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572046-01-12TASK DELETED IN ISSUE 18572046-01-13 541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND 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 WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31900 FCOR111700 FH20000 FCOR50000 FHGROUP 32APRE 48437572047-01-04 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR92000 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B572047-01-05 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28800 FCOR86400 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 125EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572047-01-06 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35200 FCOR105600 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572047-01-07TASK DELETED IN ISSUE 18572047-01-08TASK DELETED IN ISSUE 18572047-01-09 541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR118400 FH19500 FCOR50000 FHGROUP 32APOST 48437572047-01-10TASK DELETED IN ISSUE 18572048-01-01TASK DELETED IN ISSUE 18572048-01-02TASK DELETED IN ISSUE 18572048-01-03TASK DELETED IN ISSUE 18572048-01-04TASK DELETED IN ISSUE 18572049-01-04 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR103000 FH16200 FCOR50000 FHGROUP 32APRE 48437572049-01-05 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38300 FCOR115000 FH9900 FCOR29900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 126EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572049-01-06 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28000 FCOR84000 FH15400 FCOR46400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572049-01-07TASK DELETED IN ISSUE 18572049-01-08 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26400 FCOR79200 FH11200 FCOR33600 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572049-01-09 531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25200 FCOR88400 FH10700 FCOR37400 FHGROUP 32APOST 48437ORGROUP 32E572050-01-04 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35100 FCOR123100 FH9900 FCOR34700 FHGROUP 32APRE 48437572050-01-05 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22200 FCOR66600 FH10600 FCOR31900 FHGROUP 33AORGROUP 33B572050-01-06TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 127EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572050-01-07 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34200 FCOR102800 FH10500 FCOR31700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572050-01-08TASK DELETED IN ISSUE 18572050-01-09 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR98500 FH20000 FCOR50000 FHGROUP 32APOST 48437572050-01-10 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29500 FCOR88700 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572050-01-11 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29500 FCOR88700 FH17000 FCOR50000 FHGROUP 33E572050-01-12 573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR98500 FH17000 FCOR50000 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 128EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572051-01-05 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23800 FCOR83400 FH5300 FCOR18700 FHGROUP 32APRE 48437572051-01-06 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR101500 FH5300 FCOR16000 FHGROUP 33APOST 46241ORGROUP 33BPOST 46241572051-01-07 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13900 FCOR41700 FH5300 FCOR16000 FHGROUP 33APOST 42547ORGROUP 33BPOST 42547572051-01-08 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22100 FCOR66400 FH5300 FCOR16100 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572051-01-09TASK DELETED IN ISSUE 18572051-01-10 FLAPS EXTENDEDSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPARAFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28200 FCOR98800 FH6900 FCOR24300 FHGROUP 32EORGROUP 32APOST 48437572051-01-12 DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31800 FCOR95500 FH7800 FCOR23500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 129EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572052-03-01 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20900 FCOR96500 FH9800 FCOR34500 FHGROUP 32APRE 48437572052-03-02 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16000 FCOR51200 FH8900 FCOR26800 FHGROUP 33APOST 46110ORGROUP 33BPRE 43503POST 46110572052-03-04 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21400 FCOR64200 FH8100 FCOR24400 FHGROUP 33BPOST 43503572052-03-05 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21400 FCOR64300 FH10600 FCOR32000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572052-03-06 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23600 FCOR73900 FH11800 FCOR35500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572052-03-07 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23600 FCOR73900 FH11800 FCOR35500 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 130EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572052-03-08 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20300 FCOR119300 FH11100 FCOR39100 FHGROUP 32EORGROUP 32APOST 48437572052-03-09TASK DELETED IN ISSUE 18572052-03-10 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.27500 FCOR82500 FH17000 FCOR50000 FHA330-200F572054-01-05 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR70100 FH7900 FCOR27900 FHGROUP 32APRE 48437572054-01-06TASK DELETED IN ISSUE 18572054-01-07 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14100 FCOR42400 FH9300 FCOR28100 FHGROUP 33APOST 43503ORGROUP 33BPOST 43503572054-01-08 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18200 FCOR54700 FH8100 FCOR24300 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572054-01-09TASK DELETED IN ISSUE 18572054-01-10 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17400 FCOR60900 FH7700 FCOR27100 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 131EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572054-01-11 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15300 FCOR46100 FH5800 FCOR17600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572054-01-12TASK DELETED IN ISSUE 18572054-01-13 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21200 FCOR63600 FH5300 FCOR16100 FHGROUP 33APOST 46141ORGROUP 33BPOST 46141572054-01-14TASK DELETED IN ISSUE 18572054-01-15 DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.26800 FCOR80400 FH8300 FCOR25100 FHA330-200F572063-01-05TASK DELETED IN ISSUE 18572063-01-06TASK DELETED IN ISSUE 18572063-01-07TASK DELETED IN ISSUE 18572063-01-08TASK DELETED IN ISSUE 18572063-01-10TASK DELETED IN ISSUE 18572063-01-11TASK DELETED IN ISSUE 18572064-01-05TASK DELETED IN ISSUE 18572064-01-06TASK DELETED IN ISSUE 18572064-01-07TASK DELETED IN ISSUE 18572064-01-08TASK DELETED IN ISSUE 18572064-01-09TASK DELETED IN ISSUE 18572064-01-10TASK DELETED IN ISSUE 18572064-01-11TASK DELETED IN ISSUE 18572064-01-12TASK DELETED IN ISSUE 18572064-01-13 541EB 641EBDETAILED INSPECTION OF OUTER WING FRONT SPARAFT FACE BETWEEN RIB 8 AND RIB 10, INCLUDING TOPAND BOTTOM FLANGES.24800 FCOR74500 FH7300 FCOR22100 FHA330-200F572065-01-04TASK DELETED IN ISSUE 18572066-01-05TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 132EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572067-01-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18500 FCOR55500 FH3500 FCOR10700 FHGROUP 33APRE 41114572067-01-06TASK DELETED IN ISSUE 18572067-01-15 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38800 FCOR116600 FH4800 FCOR14500 FHGROUP 33APOST 54219ORPOST 53883ORGROUP 33BPOST 54219ORPOST 53883572067-01-17 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27700 FCOR83300 FH5000 FCOR15000 FHGROUP 33CPOST 54219PRE 48437ORGROUP 33CPOST 53883PRE 48437ORGROUP 33DPOST 54219PRE 48437ORGROUP 33DPOST 53883PRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 133EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572067-03-03 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27700 FCOR83300 FH5000 FCOR15000 FHGROUP 33CPOST 54219PRE 48437ORGROUP 33CPOST 53883PRE 48437ORGROUP 33DPOST 54219PRE 48437ORGROUP 33DPOST 53883PRE 48437R 572067-03-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38800 FCOR116600 FH4800 FCOR14500 FHGROUP 33APOST 54219ORGROUP 33APOST 53883ORGROUP 33BPOST 54219ORGROUP 33BPOST 53883572068-01-04 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37700 FCOR132100 FH20000 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 134EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572068-01-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36500 FCOR109700 FH5200 FCOR15700 FHGROUP 33AORGROUP 33B572068-01-06TASK DELETED IN ISSUE 18572068-01-13 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26000 FCOR78100 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572069-01-04 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27100 FCOR95100 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, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71700 FH6200 FCOR18800 FHGROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 135EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572069-01-06 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71700 FH5700 FCOR17100 FHGROUP 33B572069-01-08 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29900 FCOR89800 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572069-01-11 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34900 FCOR104800 FH15600 FCOR46800 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572069-01-12 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32400 FCOR113600 FH14500 FCOR50000 FHGROUP 32APOST 48437ORGROUP 32E572071-01-06TASK DELETED IN ISSUE 18572071-01-07TASK DELETED IN ISSUE 18572073-01-05TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 136EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572081-01-05 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22700 FCOR79700 FH12300 FCOR43000 FHGROUP 32APRE 48437572081-01-06 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18500 FCOR55600 FH7600 FCOR22900 FHGROUP 33APOST 43272572081-01-07 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71900 FH8200 FCOR24800 FHGROUP 33B572081-01-08 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21300 FCOR64100 FH10700 FCOR32200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572081-01-10TASK DELETED IN ISSUE 18572081-01-13 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21900 FCOR65900 FH18900 FCOR56900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572081-01-14 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21900 FCOR76900 FH18900 FCOR66300 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 137EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572081-01-15 541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.30100 FCOR90400 FH17000 FCOR50000 FHA330-200F572082-01-05TASK DELETED IN ISSUE 18572082-01-06 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22100 FCOR66300 FH11800 FCOR35500 FHGROUP 33AORGROUP 33B572082-01-07TASK DELETED IN ISSUE 18572082-01-08 541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33400 FCOR100300 FH7500 FCOR22500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572082-01-09TASK DELETED IN ISSUE 18572082-01-10 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,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31900 FCOR111900 FH7100 FCOR25100 FHGROUP 32APOST 48437ORGROUP 32E572082-01-11TASK DELETED IN ISSUE 18572082-01-12 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,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36600 FCOR110000 FH6800 FCOR20500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 138EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572082-01-13TASK DELETED IN ISSUE 18572082-01-14 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,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT 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 FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32500 FCOR97600 FH10000 FCOR30200 FHGROUP 33A572084-01-03 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR77600 FH11800 FCOR38400 FHGROUP 32AORGROUP 33C572084-01-04 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23800 FCOR71500 FH12100 FCOR36300 FHGROUP 33E572084-01-05 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23500 FCOR82200 FH11500 FCOR40400 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 139EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572084-01-06 541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25100 FCOR75400 FH12500 FCOR37600 FHGROUP 33D572084-01-07 541 AB, 641 AB,SEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE, RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR.11,STR.14, STR.18 TO 20 AND AT STR.23 TO 28, LH/RH.24500 FC 12600 FC A330-200F572090-01-01TASK DELETED IN ISSUE 18572090-01-03TASK DELETED IN ISSUE 18572090-01-04TASK DELETED IN ISSUE 18572090-02-01TASK DELETED IN ISSUE 18572090-02-03TASK DELETED IN ISSUE 18572090-02-04TASK DELETED IN ISSUE 18572092-01-04 541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR100700 FH10800 FCOR37800 FHGROUP 32APRE 48437572092-01-05 541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25800 FCOR77400 FH8800 FCOR26400 FHGROUP 33AORGROUP 33B572092-01-06 541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28900 FCOR86900 FH10900 FCOR32900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 140EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572093-01-06TASK DELETED IN ISSUE 18572093-01-07 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-02-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR91000 FH8400 FCOR25300 FHGROUP 33AMSN 0050AND SUBSORGROUP 33B572093-01-08 541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-02-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26300 FCOR79100 FH8400 FCOR25300 FHGROUP 33AUP TO MSN0045POST 45415572093-01-09TASK DELETED IN ISSUE 18572093-01-10TASK DELETED IN ISSUE 18572093-01-13TASK DELETED IN ISSUE 18572093-01-14TASK DELETED IN ISSUE 18572093-02-06TASK DELETED IN ISSUE 18572093-02-07 541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN JOINT OF STRINGER 15 TO CENTERSPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-01-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR91000 FH8400 FCOR25300 FHGROUP 33AMSN 0050AND SUBSORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 141EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572093-02-08 541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN JOINT OF STRINGER 15 TO CENTERSPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-01-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26300 FCOR79100 FH8400 FCOR25300 FHGROUP 33AUP TO MSN0045POST 45415572093-02-09TASK DELETED IN ISSUE 18572093-02-10TASK DELETED IN ISSUE 18572093-02-13TASK DELETED IN ISSUE 18572093-02-14TASK DELETED IN ISSUE 18572094-01-05TASK DELETED IN ISSUE 18572094-01-06 541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 9 AND RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33900 FCOR101800 FH13300 FCOR39900 FHGROUP 33AORGROUP 33B572094-01-10TASK DELETED IN ISSUE 18572095-01-05TASK DELETED IN ISSUE 18572095-01-06TASK DELETED IN ISSUE 18572095-01-07TASK DELETED IN ISSUE 18572095-01-08TASK DELETED IN ISSUE 18572101-01-04TASK DELETED IN ISSUE 18572101-01-06TASK DELETED IN ISSUE 18572101-01-07TASK DELETED IN ISSUE 18572104-01-04TASK DELETED IN ISSUE 18572104-01-05TASK DELETED IN ISSUE 18572104-01-06TASK DELETED IN ISSUE 18572104-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 142EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572107-01-05 N/ASPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT RUNOUTS OFSTRINGER BETWEEN RIB 23 AND RIB 39.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-05NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR101400 FH6100 FCOR18400 FHGROUP 33AORGROUP 33B572107-02-05 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT RUNOUTS OF STRINGERBETWEEN RIB 23 AND RIB 39.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-05NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR101400 FH3300 FCOR10000 FHGROUP 33AORGROUP 33B572108-02-04TASK DELETED IN ISSUE 18572108-02-06TASK DELETED IN ISSUE 18572108-02-07TASK DELETED IN ISSUE 18572109-02-05 542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN UPPER AND LOWER SURFACESAROUND ACCESS DOOR CUTOUTS, INCLUDING NACADUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32100 FCOR96300 FH7300 FCOR22000 FHGROUP 33AORGROUP 33B572110-01-04 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28600 FCOR100100 FH14000 FCOR49000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 143EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572110-01-05 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28300 FCOR85000 FH13300 FCOR40100 FHGROUP 33AORGROUP 33B572110-01-06 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28700 FCOR86200 FH13800 FCOR41400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572110-01-07TASK DELETED IN ISSUE 18572111-01-04 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19800 FCOR69600 FH11300 FCOR39800 FHGROUP 32APRE 48437572111-01-05 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19200 FCOR57600 FH12400 FCOR37300 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20000 FCOR60200 FH11500 FCOR34500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572111-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 144EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572111-01-09 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32300 FCOR113300 FH7200 FCOR25300 FHGROUP 32E572111-01-10 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWERSURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35400 FCOR106400 FH7900 FCOR23700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572111-01-11 532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWERSURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32300 FCOR113300 FH7200 FCOR25300 FHGROUP 32APOST 48437572116-02-01 N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE SPANWISE SKINJOINTS AT STRINGER 13 AND STRINGER 20 BETWEENRIB 12 AND RIB 27 EXCLUDING AREAS COVERED BYFLAP TRACK FAIRINGS 3, 4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38100 FCOR133400 FH5200 FCOR18400 FHGROUP 32APRE 48437572116-02-02 N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE SPANWISE SKINJOINTS AT STRINGER 13 AND STRINGER 20 BETWEENRIB 12 AND RIB 27 EXCLUDING AREAS COVERED BYFLAP TRACK FAIRINGS 3, 4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36500 FCOR109500 FH7000 FCOR21100 FHGROUP 33AORGROUP 33B572117-01-05TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 145EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572119-02-05 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT DRAIN HOLES FOR SLAT CANS,MLI HOLES AND DRAIN HOLES AFT OF FRONT SPARAND FORWARD OF REAR SPAR, BETWEEN RIBS 12AND 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32000 FCOR112100 FH12800 FCOR45100 FHGROUP 32APOST 48437ORGROUP 32E572119-02-10 N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT DRAIN HOLES FOR SLAT CANS,MLI HOLES AND DRAIN HOLES AFT OF FRONT SPARAND FORWARD OF REAR SPAR, BETWEEN RIBS 12AND 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24300 FCOR85200 FH8700 FCOR30700 FHGROUP 32APRE 48437572121-01-05 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71800 FH7600 FCOR22800 FHGROUP 33AORGROUP 33B572121-01-06TASK DELETED IN ISSUE 18572121-01-07 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24600 FCOR73900 FH8800 FCOR26500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 146EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572121-01-08 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36800 FCOR128800 FH6900 FCOR24200 FHGROUP 32APOST 48437572121-01-09TASK DELETED IN ISSUE 18572122-01-04TASK DELETED IN ISSUE 18572122-01-05TASK DELETED IN ISSUE 18572122-01-06TASK DELETED IN ISSUE 18572122-01-07TASK DELETED IN ISSUE 18572125-01-06 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27300 FCOR95700 FH11200 FCOR39400 FHGROUP 32APRE 48437572125-01-07 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-05.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR97900 FH10400 FCOR31300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 147EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572125-01-08 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28000 FCOR84200 FH11200 FCOR33700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572125-01-09TASK DELETED IN ISSUE 18572125-02-04 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27300 FCOR95700 FH11200 FCOR39400 FHGROUP 32APRE 48437572125-02-05 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-07.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32600 FCOR97900 FH10400 FCOR31300 FHGROUP 33AORGROUP 33B572125-02-06 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-08.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28000 FCOR84200 FH11200 FCOR33700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572125-02-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 148EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572129-01-03 541SB 641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-02-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30400 FCOR91400 FH6500 FCOR19700 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245572129-02-03 541SB 641SBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-01-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30400 FCOR91400 FH6500 FCOR19700 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245572130-01-03TASK DELETED IN ISSUE 18572130-02-03TASK DELETED IN ISSUE 18572131-01-04TASK DELETED IN ISSUE 18572131-01-05TASK DELETED IN ISSUE 18572131-01-06TASK DELETED IN ISSUE 18572131-01-07TASK DELETED IN ISSUE 18572133-01-04 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35900 FCOR125600 FH6600 FCOR23300 FHGROUP 32APRE 48437572133-01-05 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR99100 FH9600 FCOR28900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 149EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572133-01-07 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36900 FCOR110800 FH7000 FCOR21000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572133-01-10 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONTSPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36900 FCOR110800 FH11800 FCOR35500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572133-01-11 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONTSPAR TOREAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35900 FCOR125600 FH11200 FCOR39300 FHGROUP 32APOST 48437572138-01-05TASK DELETED IN ISSUE 18572138-01-07TASK DELETED IN ISSUE 18572138-01-09TASK DELETED IN ISSUE 18572138-01-10TASK DELETED IN ISSUE 18572139-01-05TASK DELETED IN ISSUE 18572139-01-07TASK DELETED IN ISSUE 18572139-01-09TASK DELETED IN ISSUE 18572139-01-10TASK DELETED IN ISSUE 18572140-01-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 150EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572140-01-05 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 STRINGERJOINTS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36000 FCOR108100 FH13900 FCOR41700 FHGROUP 33AORGROUP 33B572140-01-10 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 STRINGERJOINTS.30200 FCOR90800 FH17000 FCOR50000 FHA330-200F572141-01-04TASK DELETED IN ISSUE 18572141-01-05TASK DELETED IN ISSUE 18572141-01-08TASK DELETED IN ISSUE 18572144-01-05TASK DELETED IN ISSUE 18572144-01-07TASK DELETED IN ISSUE 18572144-01-09TASK DELETED IN ISSUE 18572144-01-10TASK DELETED IN ISSUE 18572148-01-04TASK DELETED IN ISSUE 18572148-01-05TASK DELETED IN ISSUE 18572148-01-06TASK DELETED IN ISSUE 18572148-01-07TASK DELETED IN ISSUE 18572153-01-04 574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38500 FCOR134900 FH11600 FCOR40600 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 151EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572153-01-05 574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23600 FCOR70900 FH7700 FCOR23300 FHGROUP 33AORGROUP 33B572153-01-06TASK DELETED IN ISSUE 18572153-01-08TASK DELETED IN ISSUE 18572153-01-11 574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACEJOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39400 FCOR118400 FH8100 FCOR24500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572153-01-12 574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35900 FCOR125700 FH7400 FCOR26100 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18600 FCOR65200 FH12300 FCOR43100 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 152EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572154-01-05 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19200 FCOR57800 FH9700 FCOR29300 FHGROUP 33AORGROUP 33B572154-01-06 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16700 FCOR50300 FH7700 FCOR23300 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572154-01-07TASK DELETED IN ISSUE 18572154-01-08TASK DELETED IN ISSUE 18572154-01-09 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16300 FCOR57100 FH7500 FCOR26500 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 153EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572154-01-10 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17800 FCOR53600 FH11800 FCOR35400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572154-01-11TASK DELETED IN ISSUE 18572154-01-13 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.32800 FCOR98400 FH8000 FCOR24000 FHA330-200F572158-01-05 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29000 FCOR101600 FH7200 FCOR25200 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26800 FCOR80400 FH8800 FCOR26500 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 154EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572158-01-10 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29600 FCOR88800 FH7400 FCOR22400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572158-01-12 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 RIB12 ANDRIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39200 FCOR137400 FH12000 FCOR42100 FHGROUP 32APOST 48437572159-01-04TASK DELETED IN ISSUE 18572159-01-05TASK DELETED IN ISSUE 18572159-01-09TASK DELETED IN ISSUE 18572162-01-05TASK DELETED IN ISSUE 18572164-01-05 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37400 FCOR131000 FH6500 FCOR22900 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 155EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572164-01-06 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29800 FCOR89500 FH7600 FCOR22900 FHGROUP 33AORGROUP 33B572164-01-07 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35500 FCOR106700 FH6700 FCOR20100 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572164-01-09TASK DELETED IN ISSUE 18572164-01-11 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34700 FCOR121600 FH5000 FCOR17600 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 156EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572164-01-12 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34700 FCOR104200 FH5000 FCOR15100 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572166-01-05TASK DELETED IN ISSUE 17572180-01-04 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20300 FCOR71300 FH15900 FCOR55800 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19600 FCOR59000 FH11300 FCOR33900 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED20500 FCOR61500 FH16000 FCOR48100 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 157EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572180-01-07 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33400 FCOR100300 FH7600 FCOR23000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572180-01-08TASK DELETED IN ISSUE 18572180-01-09 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR107200 FH6600 FCOR23400 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR107200 FH7000 FCOR24600 FHGROUP 32APOST 48437572180-01-11TASK DELETED IN ISSUE 18572180-01-12 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 FHA330-200F572181-01-04TASK DELETED IN ISSUE 18572181-01-05TASK DELETED IN ISSUE 18572181-01-06TASK DELETED IN ISSUE 18572181-01-07TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 158EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572183-01-04 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22300 FCOR78000 FH8000 FCOR28000 FHGROUP 32APRE 48437572183-01-05 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25200 FCOR75700 FH7000 FCOR21100 FHGROUP 33AORGROUP 33B572183-01-06 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22400 FCOR67200 FH7800 FCOR23500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572183-01-07 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-7NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88400 FH8300 FCOR25100 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 159EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572183-01-08 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR93600 FH7500 FCOR26500 FHGROUP 32E572183-01-10 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-02-10NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88400 FH8300 FCOR25100 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572183-01-11 542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-02-11NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR93600 FH7500 FCOR26500 FHGROUP 32APOST 48437572183-02-04 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22300 FCOR78000 FH8000 FCOR28000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 160EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572183-02-05 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25200 FCOR75700 FH7000 FCOR21100 FHGROUP 33AORGROUP 33B572183-02-06 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22400 FCOR67200 FH7800 FCOR23500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572183-02-07 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-7NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88400 FH8300 FCOR25100 FHGROUP 33E572183-02-08 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR93600 FH7500 FCOR26500 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 161EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572183-02-10 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-01-10NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR88400 FH8300 FCOR25100 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572183-02-11 542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-01-11NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26700 FCOR93600 FH7500 FCOR26500 FHGROUP 32APOST 48437572184-01-04TASK DELETED IN ISSUE 18572184-01-05TASK DELETED IN ISSUE 18572184-01-06TASK DELETED IN ISSUE 18572184-01-07TASK DELETED IN ISSUE 18572184-02-04TASK DELETED IN ISSUE 18572184-02-05TASK DELETED IN ISSUE 18572184-02-06TASK DELETED IN ISSUE 18572184-02-07TASK DELETED IN ISSUE 18572185-01-01TASK DELETED IN ISSUE 18572185-01-02TASK DELETED IN ISSUE 18572185-01-03TASK DELETED IN ISSUE 18572185-01-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 162EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY572606-01-02 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS3, 4 AND 5 AFT PICK-UP, ASSEMBLY.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33800 FCOR101400 FH20000 FCOR50000 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D572606-01-03 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS3, 4 AND 5 AFT PICK-UP, ASSEMBLY.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28900 FCOR101300 FH17600 FCOR50000 FHGROUP 32AORGROUP 32E572606-01-07 532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS3, 4 AND 5 AFT PICK-UP, ASSEMBLY.20100 FCOR60300 FH20100 FCOR60300 FHA330-200F572607-01-01 531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38500 FCOR115500 FH20000 FCOR50000 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D572607-01-06 531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.22100 FCOR66400 FH17000 FCOR50000 FHA330-200F572607-01-07 531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33000 FCOR115500 FH20000 FCOR50000 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 163EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY573001-01-05 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24100 FCOR84600 FH5900 FCOR20700 FHGROUP 32APRE 48437573001-01-07 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26400 FCOR79400 FH5900 FCOR17800 FHGROUP 33APOST 41460ORGROUP 33BPOST 41460573001-01-08 535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26600 FCOR79900 FH6500 FCOR19500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437573001-01-10TASK DELETED IN ISSUE 18573002-01-05 N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24100 FCOR84600 FH5900 FCOR20700 FHGROUP 32APRE 48437573002-01-07 N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26400 FCOR79400 FH5900 FCOR17800 FHGROUP 33APOST 41460ORGROUP 33BPOST 41460A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 164EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY573002-01-08 N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26600 FCOR79900 FH6500 FCOR19500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437573002-01-09TASK DELETED IN ISSUE 18573003-02-04 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29400 FCOR102900 FH6000 FCOR21100 FHGROUP 32APRE 48437573003-02-05 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30800 FCOR92500 FH6000 FCOR18000 FHGROUP 33AORGROUP 33B573003-02-06TASK DELETED IN ISSUE 18573003-02-07TASK DELETED IN ISSUE 18573003-02-08TASK DELETED IN ISSUE 18573003-02-09TASK DELETED IN ISSUE 18573003-02-10 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32400 FCOR97200 FH6600 FCOR19900 FHGROUP 33CPRE 48438ORGROUP 33DPRE 48437573003-02-12 WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).16400 FCOR49200 FH8100 FCOR24400 FHA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 165EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-04 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED24000 FCOR84300 FH24000 FCOR84300 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 166EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-05 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 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23900 FCOR71900 FH23900 FCOR71900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 167EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-06 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED26500 FCOR79600 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 168EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-07 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32500 FCOR114000 FH17000 FCOR50000 FHGROUP 32E574106-01-08TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 169EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-11 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED32500 FCOR114000 FH20000 FCOR50000 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 170EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574106-01-12 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 622LB622MB 622NB 622PB622QB 622RB 622SB623CB 623DB 623EB623FBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED35000 FCOR105100 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437574107-02-04 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34100 FCOR119300 FH15500 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 171EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574107-02-05 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36900 FCOR110700 FH16300 FCOR48900 FHGROUP 33AORGROUP 33B574107-02-06 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED36200 FCOR108800 FH16400 FCOR49400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 172EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-01 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13500 FCOR47500 FH6500 FCOR22700 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 173EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-02 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13500 FCOR40500 FH6400 FCOR19400 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 174EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-03 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19700 FCOR59200 FH9400 FCOR28400 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E574109-02-04TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 175EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-05 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18300 FCOR64300 FH8800 FCOR30800 FHGROUP 32APOST 48437ORGROUP 32E574109-02-06TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 176EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-07 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14900 FCOR44800 FH7100 FCOR21500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437574109-02-08TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 177EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574109-02-09 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.18300 FCOR55000 FH18300 FCOR55000 FHA330-200F574110-02-01 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR107400 FH18900 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 178EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574110-02-02 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30600 FCOR91900 FH6900 FCOR20700 FHGROUP 33AORGROUP 33B574110-02-03 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED29300 FCOR88100 FH17300 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437574114-03-01 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30500 FCOR106900 FH14600 FCOR50000 FHGROUP 32APRE 48437574114-03-02 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33400 FCOR100200 FH5600 FCOR16800 FHGROUP 33AORGROUP 33B574114-03-03 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR90900 FH13400 FCOR40400 FHGROUP 33CPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 179EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574114-03-04 N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30300 FCOR90900 FH13300 FCOR40000 FHGROUP 33DPRE 48437574115-02-01 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED16500 FCOR58000 FH7200 FCOR25300 FHGROUP 32APRE 48437574115-02-02 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19100 FCOR57300 FH2900 FCOR8900 FHGROUP 33AORGROUP 33B574115-02-03 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15900 FCOR47900 FH7000 FCOR21000 FHGROUP 33CPRE 48437574115-02-05 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15900 FCOR47900 FH6900 FCOR20800 FHGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 180EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574115-02-07 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED31400 FCOR94200 FH15100 FCOR45300 FHGROUP 33EORGROUP 33CPOST 48437ORGROUP 33DPOST 48437574115-02-09 522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED33500 FCOR117500 FH16100 FCOR50000 FHGROUP 32APOST 48437574704-02-03 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONSATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.31100 FCOR109000 FH6600 FCOR23300 FHA330-200574704-03-02 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 5, SKINCONNECTIONS ATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.31100 FCOR109000 FH6600 FCOR23300 FHA330-200574804-01-02 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 6, SKINCONNECTIONS ATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.6100 FCOR21500 FH4400 FCOR15400 FHA330-200574804-01-03 SLAT FULLY EXTENDED SPECIAL DETAILED INSPECTION OF SLAT 6, SKINCONNECTIONS ATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19800 FCOR59500 FH5400 FCOR16200 FHA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 181EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY574804-02-04 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONSATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19800 FCOR59500 FH5400 FCOR16200 FHA330-300574804-02-05 SLAT FULLY EXTENDED DETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONSATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.6100 FCOR21500 FH4400 FCOR15400 FHA330-200575011-01-04 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38000 FCOR133000 FH20000 FCOR50000 FHGROUP 32APRE 48437575011-01-05 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19000 FCOR57000 FH11600 FCOR34800 FHGROUP 33APRE 42391ORGROUP 33BPRE 42391575011-01-06 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39600 FCOR119000 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575011-01-07 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED39600 FCOR119000 FH9800 FCOR29400 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575011-01-08TASK DELETED IN ISSUE 18575011-01-09TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 182EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575011-01-10 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38000 FCOR133000 FH9300 FCOR32700 FHGROUP 32APOST 48437575011-01-11TASK DELETED IN ISSUE 18575011-01-12 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.28600 FCOR85800 FH9100 FCOR27300 FHA330-200F575011-01-13 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED37900 FCOR113700 FH11600 FCOR34800 FHGROUP 33APOST 42391ORGROUP 33BPOST 42391575012-01-02 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21900 FCOR76700 FH5600 FCOR19700 FHGROUP 32APRE 48437575012-01-03 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25300 FCOR76100 FH5400 FCOR16300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 183EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575012-01-06 N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21400 FCOR64200 FH5600 FCOR16800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575012-01-10TASK DELETED IN ISSUE 18575012-01-11TASK DELETED IN ISSUE 18575014-01-06 573DB 673DBSPECIAL DETAILED INSPECTION OF OUTER WINGTRAILINGEDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BYMLG REINFORCING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34300 FCOR103100 FH15900 FCOR47700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575016-01-04TASK DELETED IN ISSUE 18575016-01-05 531AB 631ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR UNDER FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED34900 FCOR104800 FH9000 FCOR27000 FHGROUP 33AORGROUP 33B575016-01-06TASK DELETED IN ISSUE 18575016-01-08TASK DELETED IN ISSUE 18575017-01-04TASK DELETED IN ISSUE 18575017-01-06TASK DELETED IN ISSUE 18575017-01-07TASK DELETED IN ISSUE 18575018-01-03 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED23400 FCOR81900 FH23400 FCOR81900 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 184EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575018-01-04 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27800 FCOR83400 FH13300 FCOR40100 FHGROUP 33AORGROUP 33B575018-01-05 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25700 FCOR77300 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575018-01-06 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27100 FCOR81500 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575018-01-07 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED27100 FCOR81500 FH17000 FCOR50000 FHGROUP 33E575018-01-08 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25200 FCOR88400 FH17000 FCOR50000 FHGROUP 32E575018-01-09 147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED25200 FCOR88400 FH20000 FCOR50000 FHGROUP 32APOST 48437575018-01-10TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 185EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575022-01-01 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14400 FCOR50400 FH10600 FCOR37200 FHGROUP 32APRE 48437575022-01-02 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14000 FCOR42100 FH14000 FCOR42100 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E575022-01-03TASK DELETED IN ISSUE 18575022-01-04 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13000 FCOR45700 FH13000 FCOR45700 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 186EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575022-01-05 575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15400 FCOR46400 FH11400 FCOR34300 FHGROUP 33AORGROUP 33BORGROUP 33CPRE 48437ORGROUP 33DPRE 48437575022-01-06TASK DELETED IN ISSUE 18575022-01-07TASK DELETED IN ISSUE 18575023-01-07 575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE OUTBOARD AILERON, HINGES 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED38200 FCOR133900 FH10700 FCOR37600 FHGROUP 32APOST 48437575025-01-04 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED19700 FCOR69000 FH8800 FCOR31000 FHGROUP 32APRE 48437575025-01-05 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED18800 FCOR56400 FH9600 FCOR28900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 187EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575025-01-06 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED21400 FCOR64400 FH8500 FCOR25700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575025-01-07 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED17400 FCOR52200 FH7000 FCOR21000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E575025-01-08 532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED14300 FCOR50000 FH6500 FCOR22900 FHGROUP 32APOST 48437ORGROUP 32E575025-01-09TASK DELETED IN ISSUE 18575051-01-01 734 744FLAPS EXTENDEDDETAILED INSPECTION OF FLAP TRACK BEAM NO 1,UPPER FLANGES RADII OF ROLLER TRACKS.35600 FC 8000 FC A330-200ORA330-300575051-01-02TASK DELETED IN ISSUE 18575053-01-02TASK DELETED IN ISSUE 18575054-01-01TASK DELETED IN ISSUE 18575054-01-02TASK DELETED IN ISSUE 18575055-01-02TASK DELETED IN ISSUE 18575055-01-03TASK DELETED IN ISSUE 18575057-01-02TASK DELETED IN ISSUE 18575059-01-02TASK DELETED IN ISSUE 18575061-01-02TASK DELETED IN ISSUE 18575061-01-03TASK DELETED IN ISSUE 18575063-01-01TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 188EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575067-01-02 FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575067-02-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22500 FCOR67500 FH8500 FCOR25500 FHA330-200ORA330-300575067-01-03TASK DELETED IN ISSUE 18575067-02-02 FWD FLAP TRACKFAIRINGSFAIL SAFE BOLTSPECIAL DETAILED INSPECTION OF FLAP TRACKBEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENTSPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575067-01-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED22500 FCOR67500 FH8500 FCOR25500 FHA330-200ORA330-300575067-02-03TASK DELETED IN ISSUE 18575069-01-02TASK DELETED IN ISSUE 18575069-01-03TASK DELETED IN ISSUE 18575401-01-02 FLAPS EXTENDED GENERAL VISUAL INSPECTION OF INBOARD FLAP,EXTERNAL SURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TASK TO 575401-02-01.3000 FC 3000 FC A330-200ORA330-300575401-02-01 FLAPS EXTENDED DETAILED INSPECTION OF INBOARD FLAP, EXTERNALSURFACE OF UPPER AND LOWER SKIN.NOTE: THIS TASK IS AN ALTERNATIVE TASK TO 575401-01-02.5900 FC 5900 FC A330-200ORA330-300575402-01-01TASK DELETED IN ISSUE 18575403-01-02TASK DELETED IN ISSUE 18575403-01-03TASK DELETED IN ISSUE 18575403-02-02TASK DELETED IN ISSUE 18575403-02-03TASK DELETED IN ISSUE 18575405-01-02TASK DELETED IN ISSUE 18575503-01-02TASK DELETED IN ISSUE 18A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 189EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY575503-02-02TASK DELETED IN ISSUE 18575505-01-02TASK DELETED IN ISSUE 18575505-02-02TASK DELETED IN ISSUE 18575507-01-02TASK DELETED IN ISSUE 18575507-02-02TASK DELETED IN ISSUE 18575509-01-02TASK DELETED IN ISSUE 18575509-02-02TASK DELETED IN ISSUE 18576105-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED13600 FCOR51300 FH13600 FCOR51300 FHA330-200POST 53074ORA330-300POST 53074576105-01-02 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1.11100 FCOR33500 FH8200 FCOR24700 FHA330-200F576108-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED30200 FCOR113800 FH23900 FCOR88200 FHA330-200POST 53074ORA330-300POST 53074576108-01-02 FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.15400 FCOR92600 FH15400 FCOR92600 FHA330-200F576114-02-01 JACK FAIRINGSSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGE OF OUTER JACK FITTING.30000 FCOR195500 FH6400 FCOR56200 FHA330-200ORA330-300576115-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGERADIUS AT LUG SIDE OF HINGE1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED28100 FCOR106100 FH28100 FCOR106100 FHA330-200POST 53074ORA330-300POST 53074576115-01-02 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGERADIUS AT LUG SIDE OF HINGE1.20400 FCOR61400 FH18400 FCOR55400 FHA330-200FA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 190EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY576117-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACKFITTING.11900 FCOR78000 FH9400 FCOR89300 FHA330-200POST 53074ORA330-300POST 53074576117-01-02 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF OUTER JACKFITTING.13100FCOR39400 FH8900 FCOR26700 FHA330-200F576118-01-01 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED15500 FCOR62000 FH15500 FCOR62000 FHA330-200POST 53074ORA330-300POST 53074576118-01-02 FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.10700 FCOR53600 FH10700 FCOR53600 FHA330-200F577003-01-02TASK DELETED IN ISSUE 18711141-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF INLET COWLATTACHMENT (A1 FLANGE).8000 FC 8000 FC GE711200-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOORHINGES AND SURROUNDING STRUCTURE (15 CMAROUND HINGE FITTINGS).8000 FC 8000 FC RRA330-200ORRRA330-300711246-01-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOORLATCHES AND SURROUNDING STRUCTURE (15 CMAROUND LATCH FITTINGS).8000 FC 8000 FC RRA330-200ORRRA330-300711301-02-02 415AL 415BL 416AR416BR 425AL 425BL426AR 426BRGENERAL VISUAL INSPECTION OF FWD AND AFT FANCOWL DOOR HINGES AND SURROUNDING STRUCTURE(15 CM AROUND HINGE FITTINGS).8000 FC 8000 FC PWA330-200ORPWA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 191EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY711302-02-02 415AL 415BL 416AR416BR 425AL 425BL426AR 426BRGENERAL VISUAL INSPECTION OF FWD AND AFT FANCOWL DOOR LATCHES AND SURROUNDINGSTRUCTURE (15 CM AROUND LATCH FITTINGS).8000 FC 8000 FC PWA330-200ORPWA330-300711341-02-02 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOORHINGES AND SURROUNDING STRUCTURE (15 CMAROUND HINGE FITTINGS).8000 FC 8000 FC GE711343-02-01 415AL 416AR 425AL426ARGENERAL VISUAL INSPECTION OF FAN COWL DOORLATCHES AND SURROUNDING STRUCTURE (15 CMAROUND LATCH FITTINGS).8000 FC 8000 FC GE711345-02-01 414AL 414AR 424AL424ARGENERAL VISUAL INSPECTION OF CORE COWL DOORHINGES AND SURROUNDING STRUCTURE (15 CMAROUND HINGE FITTINGS).8000 FC 8000 FC GE711347-01-01 414AL 414AR 424AL424ARGENERAL VISUAL INSPECTION OF CORE COWL DOORLATCHES AND SURROUNDING STRUCTURE (15 CMAROUND LATCH FITTINGS).8000 FC 8000 FC GE712102-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF CF6-80E1 FORWARDENGINE MOUNT EXCLUDING THE PLATFORM.4000 FCOR30800 FH4000 FCOR30800 FHGE712103-01-01 ENGINEFORWARD ENGINEMOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT PLATFORM.6300 FCOR65800 FH4100 FCOR42400 FHCF6-80E1A2PRE 43462712103-01-02 ENGINEFORWARD ENGINEMOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT PLATFORM.6600 FCOR68300 FH6600 FCOR68300 FHCF6-80E1A2POST 43462ORCF6-80E1A3ORCF6-80E1A4712104-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF FORWARD ENGINE MOUNTREAR TRUNNION CLEARANCE HOLE.NOTE: INSPECTION FOR ACTIVATION OF SECONDARYLOAD PATH.2360 FCOR24400 FH2360 FCOR24400 FHRRA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 192EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY712105-01-01 ENGINEFWD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT THRUST TRUNNION.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8000 FCOR30200 FH8000 FCOR30200 FHRRA330-200ORRRA330-300712105-01-02 ENGINEFWD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT THRUST TRUNNION.8000 FCOR30200 FH8000 FCOR30200 FHRRA330-200F712106-01-01 ENGINEFORWARD ENGINEMOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT.8000 FCOR52000 FH8000 FCOR52000 FHPW712107-01-01 415AL 416AR 425AL426AR 417AL 418AR427AL 428ARSPECIAL DETAILED INSPECTION OF PYLON BOLTS OFTHE FORWARD ENGINE MOUNT4000 FCOR30800 FH4000 FCOR30800 FHGE712202-01-01 414AL 414AR 424AL424ARDETAILED INSPECTION OF AFT ENGINE MOUNTEXCLUDING THE UPPER BEAM.8000 FCOR68400 FH8000 FCOR68400 FHGE712204-01-01 417AL 418AR 427AL428ARDETAILED INSPECTION OF AFT ENGINE MOUNT FAILSAFE LINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARYLOAD PATH.4130 FCOR42600 FH4130 FCOR42600 FHRR712204-02-01 417AL 418AR 427AL428ARENGINEENGINE MOUNTDETAILED INSPECTION OF AFT ENGINE MOUNT FAILSAFE LINK.NOTE: INSPECTION FOR ACTIVATION OF SECONDARYLOAD PATH.8000 FCOR52000 FH8000 FCOR52000 FHPWR 712205-01-01 417AL 418AR 427AL428ARENGINESPECIAL DETAILED INSPECTION OF AFT ENGINEMOUNT LINKSNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FC OPTIMIZED8000 FCOR30200 FH8000 FCOR30200 FHA330-200RRORA330-300RRR 712205-01-02 417AL 418AR 427AL428ARENGINESPECIAL DETAILED INSPECTION OF AFT ENGINEMOUNT LINKS8000 FCOR30200 FH8000 FCOR30200 FHA330-200FRRA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.1PAGE: 193EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESS TASK DESCRIPTION THRESHOLD INTERVAL APPLICABILITY783200-01-02 417DL 417EL 418DR418ER 427DL 427EL428DR 428ERGENERAL VISUAL INSPECTION OF THRUST RESERVERHINGES, SLEEVES, PINS AND SURROUNDINGSTRUCTURE (15 CM AROUND HINGE FITTINGS).2000 FC 2000 FC RRA330-200POST 46879ORRRA330-300POST 46879ORRRA330-200POST 47358ORRRA330-300POST 47358783201-03-01 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARGENERAL VISUAL INSPECTION OF THRUST REVERSERHINGES, ATTACHMENTS AND SURROUNDINGSTRUCTURE (15 CM AROUND HINGE ATTACHMENTS).8000 FC 8000 FC GE783201-04-01 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARGENERAL VISUAL INSPECTION OF THRUST REVERSERHINGES, ATTACHMENTS AND SURROUNDINGSTRUCTURE (15 CM AROUND HINGE ATTACHMENTS).8000 FC 8000 FC PWA330-200ORPWA330-300783202-01-02 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARLATCH ACCESS DOORGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES, ATTACHMENTS AND SURROUNDINGSTRUCTURE (15 CM AROUND LATCH ATTACHMENTS).8000 FC 8000 FC GE783202-02-02 415BL 416BR 417AL418AR 425BL 426BR427AL 428ARLATCH ACCESS DOORGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES, ATTACHMENTS AND SURROUNDINGSTRUCTURE (15 CM AROUND LATCH ATTACHMENTS).8000 FC 8000 FC PWA330-200ORPWA330-300783245-02-01 418HR 418JR 428HR428JRGENERAL VISUAL INSPECTION OF THRUST REVERSERLATCHES AND SURROUNDING STRUCTURE (15 CMAROUND LATCH FITTINGS).8000 FC 8000 FC RRA330-200ORRRA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 1EASA APPROVED©AIRBUS SAS 2012. All rights reserved.2 AIRWORTHINESS LIMITATIONS2-2 SECTION 2.2REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY531120-01-02713 714GENERAL VISUAL INSPECTION OF NLG BAY INTERNALSTRUCTURE, NOSE LANDING GEAR WELL PANELS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED1150 FCOR6750 FH1150 FCOR6750 FHA330-200ORA330-300531124-01-04713 714DETAILED INSPECTION OF NLG BAY SIDE PANEL TOPINNER RADIUS FROM NLG BAY FORWARD PANEL TONLG BAY AFT PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR144100 FH9200 FCOR52400 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532115-01-02821GENERAL VISUAL INSPECTION OF FORWARD CARGOCOMPARTMENT DOOR CUTOUT, VISIBLE PART OFLATERAL FRAMES (FR 20A AND FR 25A).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR97400 FH14300 FCOR97400 FHA330-200ORA330-300532126-01-01832 842DOOR FRAME LININGINSULATIONDETAILED INSPECTION OF DOOR 2, COVER PLATE OFTORSION BOX FROM FR 33 TO FR 35A, BETWEEN STR12 AND STR 13, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17300 FCOR104300 FH11700 FCGROUP 33APRE 45223ORGROUP 33BPRE 45223532127-01-01832 842DOOR FRAME LININGNOTE 1DETAILED INSPECTION OF DOOR NO 2, FR 33,BETWEEN STR 13 AND STR 15, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15900 FCOR108300 FH6300 FCGROUP 33APRE 44147ORGROUP 33BPRE 44147A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 2EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY532130-01-02N/ADETAILED INSPECTION OF FUSELAGE SKIN EXTERNALSURFACE AND VISIBLE PORTION OF WINDOWFORGINGS, BETWEEN FR18 AND FR 31, BETWEEN FR36 AND FR 38 FROM STR 18 TO STR 22, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20400 FC6700 FCOR44000 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D532156-01-02N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED35200 FCOR239600 FH3700 FCOR22500 FHGROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636532156-01-03N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED35200 FCOR239600 FH3500 FCOR21500 FHGROUP 33APRE 46636ORGROUP 33BPRE 46636ORGROUP 33CPRE 46636ORGROUP 33DPRE 46636532158-01-02833 843CEILING PANELSINSULATIONSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL SPLICE AT FR 37.1, FROM STR 13TO CROWN CENTER LINE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED35200 FCOR239600 FH3700 FCOR22500 FHGROUP 32AORGROUP 33CPOST 46636ORGROUP 33DPOST 46636A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 3EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533009-01-01251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR158100 FH13200 FCOR79700 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911533009-01-02251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-02NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26900 FCOR175200 FH10500 FCOR68500 FHGROUP 32APRE 49202PRE 52911ORGROUP 32APOST 50755PRE 56001533009-01-03251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-03NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24600 FCOR147900 FH9700 FCOR58200 FHGROUP 33DPRE 49202PRE 52911A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 4EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533009-01-04251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1FASTENERSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-02-04NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR151600 FH9800 FCOR59100 FHGROUP 33CPRE 49202PRE 52911533009-02-01251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR158100 FH4400 FCOR26600 FHGROUP 33APRE 52911ORGROUP 33BPRE 52911533009-02-02251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-02NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26900 FCOR175200 FH3500 FCOR22800 FHGROUP 32APRE 49202PRE 52911ORGROUP 32APOST 50755PRE 56001A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 5EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533009-02-03251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-03NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24600 FCOR147900 FH3200 FCOR19400 FHGROUP 33DPRE 49202PRE 52911533009-02-04251JC 251VW 252JC252VWOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL BUTT JOINT AT FRAME 45,BETWEEN STRINGER 3 AND 5, AND BETWEENSTRINGER 11 AND 13, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533009-01-04NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR151600 FH3250 FCOR19700 FHGROUP 33CPRE 49202PRE 52911533010-01-01N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR158100 FH3750 FCOR22500 FHGROUP 33AORGROUP 33BR 533010-01-02 N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26900 FCOR175200 FH2950 FCOR19300 FHGROUP 32APRE 49202ORGROUP 32APOST 50755A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 6EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533010-01-03N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24600 FCOR147900 FH2700 FCOR16400 FHGROUP 33DPRE 49202533010-01-04N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 45 FROM CROWNCENTERLINE TO STRINGER 17, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR151600 FH2750 FCOR16700 FHGROUP 33CPRE 49202533012-01-01261CC 262CCOVERHEAD STOWAGEBINSNOTE 1RIVETSSPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROMSTRINGER 4 TO 5, LH/RH.NOTE :- ROTOTEST INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-02-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27000 FCOR162000 FH7100 FCOR42600 FHGROUP 33APRE 52911533012-02-01261CC 262CCOVERHEAD STOWAGEBINSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54 FROMSTRINGER 4 TO 5, LH/RH.NOTE :- X-RAY INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 533012-01-01NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27000 FCOR162000 FH2200 FCOR13300 FHGROUP 33APRE 52911533014-01-01734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20FASTENERS AFT OF FRAME 47 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28200 FCOR191300 FH7150 FCOR48400 FHGROUP 33AORGROUP 33BPRE 45307S13490A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 7EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533014-01-02734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 20FASTENERS AFT OF FRAME 47 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27700 FCOR180400 FH7000 FCOR45600 FHGROUP 32APRE 45307S13490533016-01-01N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25000 FCOR169200 FH3750 FCOR25400 FHGROUP 33C533016-01-02N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24400 FCOR165500 FH3650 FCOR24900 FHGROUP 33D533016-01-03N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 38, FROM CROWNCENTERLINE TO STR 3 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23500 FCOR159000 FH3650 FCOR24900 FHGROUP 33E533018-01-01N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR170400 FH4150 FCOR27000 FHGROUP 32APRE 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 8EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533018-01-02N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR143600 FH3800 FCOR22900 FHGROUP 33DPRE 49202533018-01-03N/ASPECIAL DETAILED INSPECTION OF FUSELAGECIRCUMFERENTIAL JOINT AT FRAME 54, FROM CROWNCENTERLINE TO STR 4 AND FROM STR 5 TO STR 11,EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24500 FCOR147100 FH3850 FCOR23200 FHGROUP 33CPRE 49202533021-01-01734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8150 FCOR55100 FH5400 FCOR36700 FHGROUP 33APOST 45307ORGROUP 33BPOST 45307533021-01-02734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7550 FCOR49200 FH5050 FCOR32800 FHGROUP 32APOST 45307ORGROUP 33CORGROUP 33D533021-01-03734744SPECIAL DETAILED INSPECTION OF RADII OF TEEFITTINGS CONNECTING HYDRAULIC BRACKET TOVERTICAL BEAMS Y=953 and Y=450, BELOW PRESSUREFLOOR, AT PRESSURE BULKHEAD FR 53,2, LH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7800 FCOR51400 FH5200 FCOR34300 FHGROUP 32EORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 9EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533104-01-03ANTICOLLISION LIGHT:LENS 7LVADF: LENSES 2RP1 &SEAL AND 2RP2 & SEALDETAILED INSPECTION OF FUSELAGE SKIN 50 MMAROUND:- UPPER BEACON LIGHT CUTOUT BETWEEN FR.42 ANDFR.43- ADF LOOP AND SENSE ANTENNA CUTOUTS BETWEENFR.48 AND FR.49 AND BETWEEN FR.52 & FR.53,BETWEEN STRINGER 1 LH AND STRINGER 1 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33900 FCOR229600 FH5050 FCGROUP 33AORGROUP 33B533106-01-02N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19000 FCOR128800 FH5600 FCOR38300 FHGROUP 33AORGROUP 33B533106-01-03N/ADETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, FASTENERS AREA AT WINDOW FRAMESJUNCTION ON FUSELAGE SKIN BETWEEN STRG. 18AND STRG. 22, FROM FRAME 38 TO 53.3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR161800 FH8300 FCOR56300 FHGROUP 32A533107-01-03LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10800 FCOR73600 FH8650 FCOR58700 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 10EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533107-01-04LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9900 FCOR67200 FH7800 FCOR52800 FHGROUP 32APRE 49202533107-01-05LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8900 FCOR60800 FH7250 FCOR49000 FHGROUP 33DPRE 49202533107-01-06LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13900 FCOR94200 FH7500 FCOR51300 FHGROUP 33E533107-01-07LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16700 FCOR113000 FH8600 FCOR58300 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 11EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533107-01-08LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9200 FCOR62500 FH7400 FCOR50100 FHGROUP 33CPRE 49202533107-01-09LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR111900 FH7800 FCOR52800 FHGROUP 32APOST 49202533107-01-10LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14900 FCOR101300 FH7250 FCOR49000 FHGROUP 33DPOST 49202533107-01-11LININGNOTE 1AIR CONDITIONINGDUCTSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAMES 39 TO 39.2 WEBHOLE AREA JUST BELOW STRINGER 28 ANDFASTENERS AREA AT FRAMES JUNCTION BELOWSTRINGER 29 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR104100 FH7400 FCOR50100 FHGROUP 33CPOST 49202533112-01-01N/ASPECIAL DETAILED INSPECITON OF FUSELAGEEXTERNAL STRUCTURE, LONGITUDINAL JOINT ATSTRINGER 39 AHEAD OF FRAME 53.2, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED37000 FCOR250500 FH1600 FCOR11000 FHGROUP 33APOST 41897ORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 12EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533112-01-02N/ASPECIAL DETAILED INSPECITON OF FUSELAGEEXTERNAL STRUCTURE, LONGITUDINAL JOINT ATSTRINGER 39 AHEAD OF FRAME 53.2, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED34000 FCOR221600 FH1500 FCOR9900 FHGROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533113-01-04N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8500 FCOR58000 FH5900 FCOR40200 FHGROUP 33AORGROUP 33B533113-01-05N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED5800 FCOR39500 FH4600 FCOR31100 FHGROUP 33E533113-01-06N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7000 FCOR47400 FH5200 FCOR35400 FHGROUP 32E533113-01-07N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8050 FCOR54600 FH5650 FCOR38200 FHGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 13EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533113-01-08N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8900 FCOR60300 FH6050 FCOR41200 FHGROUP 32A533113-01-09N/ASPECIAL DETAILED INSPECTION OF FUSELAGEEXTERNAL STRUCTURE, FASTENERS ROWS AT FRAME47, FROM BELOW STRINGER 22 TO ABOVE STRINGER24 LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8250 FCOR56100 FH5750 FCOR39100 FHGROUP 33C533114-01-03251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15900 FCOR107800 FH15900 FCOR107800 FHGROUP 33AORGROUP 33B533114-01-04251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11800 FCOR80300 FH11800 FCOR80300 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533114-01-06251XW 252XWNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME 47 WEB AT JUNCTIONWITH STABILIZERS STRINGER 20 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13100 FCOR88700 FH13100 FCOR88700 FHGROUP 32APRE 49202533115-01-04251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10300 FCOR70300 FH4350 FCOR29600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 14EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533115-01-05251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8500 FCOR57900 FH3650 FCOR24700 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533115-01-06251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10400 FCOR70700 FH3500 FCOR24200 FHGROUP 33E533115-01-07251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12500 FCOR84800 FH4000 FCOR27500 FHGROUP 32E533115-01-08251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9400 FCOR64000 FH3900 FCOR26600 FHGROUP 32APRE 49202533115-01-10251XW 252XWNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 47, STABILIZERS FROMSTRINGER 19 TO 23, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11200 FCOR76100 FH3650 FCOR24700 FHGROUP 32APOST 49202ORGROUP 33CPOST 49202ORGROUP 33DPOST 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 15EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533126-01-03734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED3800 FCOR24700 FH3800 FCOR24700 FHGROUP 32A533126-01-05734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED3850 FCOR26100 FH3850 FCOR26100 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533126-01-06734 744GENERAL VISUAL INSPECTION OF SKIN PANEL AREAAROUND CLG AND MLG CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE : A CENTERLINE LANDING GEAR (CLG) IS NOTFITTED TO THE A330. HOWEVER, THE TERM CLG HASBEEN KEPT IN THE DESCRIPTION DUE TO FUSELAGESTRUCTURAL COMMONALITY WITH THE A340 IN THISAREA.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED5000 FCOR32800 FH5000 FCOR32800 FHGROUP 32EORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 16EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533127-03-01FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED3850 FCOR26100 FH3850 FCOR26100 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D533127-03-02FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACENOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED3800 FCOR24700 FH3800 FCOR24700 FHGROUP 32A533127-03-03FAIRING PANELSBETWEEN FR.39.1 ANDFR.47DETAILED INSPECTION OF AREA AROUND AIRCONDITIONING ACCESS CUTOUT TO AN EXTENT OF15.0 CM (6.0 IN) EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED5000 FCOR32800 FH5000 FCOR32800 FHGROUP 32EORGROUP 33E533138-01-02FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FLOOR BEAM INBOARDFLANGE AT Y=1959, AT FR48 LEVEL LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22100 FCOR150100 FH21500 FCOR146100 FHGROUP 33APOSTMSB 53-3013R533151-01-01 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13400 FCOR90600 FH10200 FCOR69100 FHGROUP 33AORGROUP 33BR533151-01-02 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11000 FCOR74700 FH7900 FCOR53400 FHGROUP 33CORGROUP 33DORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 17EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYR533151-01-03 832 842GALLEYS AND TOILETS,IFINSTALLED.SIDEWALL LININGS ATFR40 (LH/RH)DETAILED INSPECTION OF FR.40 FRONT FITTING ATSTRINGER 21 LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12200 FCOR82500 FH9000 FCOR61200 FHGROUP 32AORGROUP 32E533155-01-01251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33900 FCOR220900 FH11900 FCOR77800 FHGROUP 32APRE 49202533155-01-02251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27900 FCOR188800 FH9950 FCOR67500 FHGROUP 33AORGROUP 33B533155-01-03251FG 252FGNOTE 1DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAME 46 CUTOUT AT STRINGER 28LEVEL, LH/RHNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED34300 FCOR232100 FH12100 FCOR82100 FHGROUP 33CPRE 49202ORGROUP 33DPRE 49202533156-01-01822LININGNOTE 1LD-MCR IF INSTALLEDPOST 46678: LDLTOILETS ANDFURNISHINGSSPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE,SPLICE AT FRAME JUNCTIONSBETWEEN STRINGERS 32 AND 33 AT FRAMES 53.3 TO54, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29200 FCOR198000 FH6250 FCOR42300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 18EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533156-01-02822LD-MCR IF INSTALLEDOR POST 46678 LDLTOILETS ANDFURNISHINGSLININGNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNALSTRUCTURE,SPLICE AT FRAME JUNCTIONS BETWEENSTRINGERS32 AND 33 AT FRAMES 53.3 TO 54, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33200 FCOR216000 FH7100 FCOR46100 FHGROUP 32APRE 49202ORGROUP 33CPRE 49202ORGROUP 33DPRE 49202533162-01-02734 744SPECIAL DETAILED INSPECTION OF MAIN LANDINGGEAR BAY, LOWER FLANGE OF GANTRY Y=1456, 40FASTENERS FORWARD AND AFT FR. 48 DATUM, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15700 FCOR106400 FH9500 FCOR64700 FHGROUP 33AORGROUP 33BPRE 43852533164-01-03734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR106300 FH10600 FCOR69300 FHGROUP 32A533164-01-04734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20900 FCOR136300 FH12900 FCOR84200 FHGROUP 32EORGROUP 33E533164-01-06734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22300 FCOR151000 FH13000 FCOR87900 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 19EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533164-01-07734 744DETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, CANTED DIAPHRAGMS AND JUNCTIONAREA OF CANTED DIAPHRAGMS ON FLOOR BEAMSBETWEEN FRAMES 47 AND 48 FROM Y=450 TO Y=1959,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17200 FCOR116600 FH10900 FCOR74400 FHGROUP 33CORGROUP 33D533165-01-02251MG 251SG 252MG252SGNOTE 1GALLEYS & TOILETS IFINSTALLEDDETAILED INSPECTION OF FUSELAGE INTERNALSTRUCTURE, FRAMES 48 TO 53.1 HORIZONTAL LEG ATSTRINGER PASSAGE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10300 FCOR69900 FH9200 FCOR62200 FHGROUP 33APOST 43904533180-01-03N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20100 FCOR136300 FH7100 FCOR46500 FHGROUP 32A533180-01-04N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14500 FCOR98400 FH4000 FCOR27600 FHGROUP 33AORGROUP 33BR 533180-01-05 N/ADETAILED INSPECTION OF SKIN IN CIRCUMFERENTIALSPLICE AND STRINGER COUPLING AREAS BETWEENFR 53,6 AND FR 53,7, EXTERNAL SURFACE, LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24600 FCOR166600 FH4900 FCOR33600 FHGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 20EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533181-01-03N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20400 FCOR138100 FH12600 FCOR81900 FHGROUP 32A533181-01-04N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR99500 FH7400 FCOR50600 FHGROUP 33AORGROUP 33B533181-01-05N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR170400 FH8200 FCOR55800 FHGROUP 33CORGROUP 33DR 533181-01-06 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21400 FCOR144900 FH12200 FCOR82800 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 21EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYR 533181-01-07 N/ASPECIAL DETAILED INSPECTION OF SPLICE PLATE ATTHE CIRCUMFERENTIAL SPLICE BETWEEN FR 53.6 ANDFR 53.7 , LH/RH:- FROM STR 5 TO STR 13 (DOOR TYPE A)- FROM STR 5 TO STR 15 (DOOR TYPE 1)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20700 FCOR140000 FH13300 FCOR86400 FHGROUP 32E533187-01-01CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23500 FCOR159000 FH8500 FCGROUP 32AORGROUP 32E533187-01-02CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22100 FCOR150100 FH8000 FCGROUP 33AORGROUP 33B533187-01-03CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18700 FCOR126700 FH7150 FCGROUP 33CORGROUP 33D533187-01-05CABIN FLOOR PANELSGALLEYS & TOILETS IFINSTALLEDSPECIAL DETAILED INSPECTION OF LARGEMEMBRANES AROUND 6 FASTENERS BETWEENFRAME 48 AND FRAME 49, AT Y-1456 AND Y+1456.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17800 FCOR120700 FH7000 FCGROUP 33E533194-01-04 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR112000 FH10000 FCOR68200 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 22EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533194-01-05 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10000 FCOR68200 FH5500 FCOR37600 FHGROUP 33ADOOR TYPE 1ORGROUP 33BDOOR TYPE 1533194-01-06 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR111800 FH13200 FCOR89600 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352533194-01-07 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR112000 FH6700 FCOR45900 FHGROUP 33ADOOR TYPE APOST 42352PRE 41848ORGROUP 33BDOOR TYPE APOST 42352PRE 41848533194-01-08 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21500 FCOR145600 FH6500 FCOR44200 FHGROUP 33ADOOR TYPE APOST 41848ORGROUP 33BDOOR TYPE APOST 41848533194-01-09 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR137400 FH9500 FCOR64600 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 23EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533194-01-11 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR99900 FH5800 FCOR39800 FHGROUP 32E533194-01-12 834 844SPECIAL DETAILED INSPECTION OF FUSELAGE SKINAT DOOR 3 (EMERGENCY/PASSENGER/CREW DOOR)CUT-OUT UPPER CORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR134400 FH9800 FCOR66600 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR134400 FH10100 FCOR68700 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10000 FCOR68200 FH5500 FCOR37600 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR111800 FH13200 FCOR89600 FHGROUP 33ADOOR TYPE APOST 42351PRE 42352ORGROUP 33BDOOR TYPE APOST 42351PRE 42352A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 24EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY533195-02-07 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR112000 FH6700 FCOR45900 FHGROUP 33ADOOR TYPE APOST 42352PRE 41848ORGROUP 33BDOOR TYPE APOST 42352PRE 41848533195-02-08 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21500 FCOR145600 FH6500 FCOR44200 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,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR137400 FH9500 FCOR64600 FHGROUP 32A533195-02-11 834 844SCUFF PLATESPECIAL DETAILED INSPECTION OF DOOR 3(EMERGENCY/PASSENGER/CREW DOOR) CUT-OUT,STRUCTURE UNDERNEATH THE SCUFF PLATE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR97300 FH5800 FCOR39800 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR134400 FH9800 FCOR66600 FHGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 25EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY534102-01-03N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 58 FROM STRINGERS 13 TO CROWNCENTER LINE, EXTERNAL SURFACE, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26500 FCOR179600 FH9300 FCOR63200 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534104-01-08833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 58, FROMSTRINGERS 4 TO 6, STRINGERS 12 TO 14 ANDSTRINGERS 21 TO 22, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7300 FCOR49600 FH7300 FCOR49600 FHGROUP 33APRE 43996ORGROUP 33BPRE 43996ORGROUP 33CPRE 43996ORGROUP 33DPRE 43996534105-01-03N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33700 FCOR202400 FH10600 FCOR64100 FHGROUP 33APRE 40556ORGROUP 33BPRE 40556534105-01-04N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28000 FCOR172200 FH15600 FCOR99300 FHGROUP 32AORGROUP 33APOST 40556ORGROUP 33BPOST 40556ORGROUP 33CPOST 40556ORGROUP 33DPOST 40556A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 26EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY534105-01-06N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS AT FR 72 FROM STRINGERS 13 LH/RH TOCROWN CENTER LINE, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21100 FCOR137300 FH13400 FCOR87400 FHGROUP 32E534107-01-02833 843CEILING PANELSOVERHEAD STOWAGEBINS, INSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3TO STR 7, AND STR 11 TO STR 13, AT INTERSECTIONOF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28300 FCOR183200 FH13100 FCOR86900 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534107-01-04833 843CEILING PANELSOVERHEAD STOWAGEBINSINSULATIONSPECIAL DETAILED INSPECTION OF SPLICE PLATE ATCIRCUMFERENTIAL SKIN SPLICE AT FR 72, FROM STR 3TO STR 7, AND STR 11 TO STR 13, AT INTERSECTIONOF LAP JOINTS AND CIRCUMFERENTIAL SKIN SPLICE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21100 FCOR137300 FH11200 FCOR73000 FHGROUP 32ER 534108-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE AND STRINGER COUPLINGAREAS ATFR 76 FROM STR 13 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28500 FCOR185600 FH22600 FCOR146300 FHA330-200ORA330-300R 534110-01-02 N/ADETAILED INSPECTION OF FUSELAGE SKIN INCIRCUMFERENTIAL SPLICE COUPLING AREA AT FR 80FROMSTR 6 TO STR 13 LH/RH, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28500 FCOR185600 FH22600 FCOR146300 FHA330-200ORA330-300A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 27EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY534120-01-04N/ADETAILED INSPECTION OF FUSELAGE SKIN ANDVISIBLE PART OF WINDOW FORGINGS BETWEEN FR53.8 AND FR 73 AND BETWEEN STRINGERS 18 AND 22LH/RH, EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16400 FCOR106900 FH16400 FCOR106900 FHGROUP 32E534131-01-02833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8000 FCOR52500 FH8000 FCOR52500 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534131-01-03833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8700 FCOR52300 FH8700 FCOR52300 FHGROUP 33E534131-01-04833 843SPECIAL DETAILED INSPECTION OF AT DOOR 4 (AFTPASSENGER/CREW DOOR) CUT-OUT UPPERCORNERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8000 FCOR52400 FH8000 FCOR52400 FHGROUP 32E534136-01-02N/ASPECIAL DETAILED INSPECTION OF FUSELAGE SKINOF AFT CARGO COMPARTMENT DOOR CUT-OUT ATUPPER REAR AND LOWER FORWARD CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR131000 FH4900 FCOR33100 FHGROUP 33APRE 41045ORGROUP 33BPRE 41045A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 28EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY534139-01-04822GENERAL VISUAL INSPECTION OF AFT CARGOCOMPARTMENT DOOR CUT-OUT, VISIBLE PART OFLATERAL FRAMES (FR 59A AND 65) AS FAR AS VISIBLE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR97400 FH14300 FCOR97400 FHA330-200ORA330-300534143-01-02N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED4400 FCOR29200 FH4400 FCOR29200 FHGROUP 32A534143-01-03N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7000 FCOR42200 FH7000 FCOR42200 FHGROUP 33E534143-01-04N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6900 FCOR45300 FH6900 FCOR45300 FHGROUP 32E534143-01-06N/ADETAILED INSPECTION OF SKIN OF BULK CARGOCOMPARTMENT DOOR CUT-OUT AT UPPER CORNERS,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED4700 FCOR28400 FH4700 FCOR28400 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 29EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY534144-01-02823SCUFF PLATEDETAILED INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT STRUCTUREUNDERNEATH SCUFF PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18600 FCOR111700 FH4400 FCOR28400 FHGROUP 32AORGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D534144-01-04823SCUFF PLATEDETAILED INSPECTION OF BULK CARGOCOMPARTMENT DOOR CUT-OUT STRUCTUREUNDERNEATH SCUFF PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21100 FCOR137300 FH6900 FCOR45300 FHGROUP 32E534148-01-02ANTENNADETAILED INSPECTION OF SKIN AROUND VHF 3ANTENNA CUT-OUT BETWEEN FR 56 AND FR 57 FROMSTRINGERS 2 LH/RH TO CROWN CENTER LINE,EXTERNAL SURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20600 FCOR139500 FH7900 FCOR54100 FHGROUP 33AORGROUP 33B545104-02-03415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12100 FCOR81900 FH1200 FCOR8100 FHGEGROUP 33AORGEGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 30EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545104-02-04415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12500 FCOR84600 FH1200 FCOR8100 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545104-02-05415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10800 FCOR73100 FH1100 FCOR7400 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545104-02-12415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11800 FCOR76700 FH1200 FCOR7800 FHGEGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 31EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545104-02-13415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12200 FCOR79300 FH1200 FCOR7800 FHPWGROUP 32APRE 48298545104-02-14415AL 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)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10500 FCOR68200 FH1100 FCOR7100 FHRRGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 32EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545108-03-01415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED5600 FCOR36400 FH5600 FCOR36400 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 32APRE48298ORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298ORPWGROUP 32APRE48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 33EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545108-03-03415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED4700 FCOR30500 FH4700 FCOR30500 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298ORRRGROUP 32APRE48298545108-03-09415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINE FORWARD MOUNT FITTING TO RIB 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8500 FCOR57500 FH8500 FCOR57500 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 34EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545108-03-11415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6600 FCOR44600 FH6600 FCOR44600 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545108-03-12415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8100 FCOR52600 FH8100 FCOR52600 FHGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32APOST 48298ORPWGROUP 32E545108-03-14415AL 416AR 425AL426ARDETAILED INSPECTION OF PYLON PYRAMID FROMENGINEFORWARD MOUNT FITTING TO RIB 1NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6300 FCOR40900 FH6300 FCOR40900 FHRRGROUP 32APOST 48298ORRRGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 35EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545129-01-03454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21200 FCOR143500 FH6700 FCOR45300 FHPWGROUP 32AORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 32EORPWGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 36EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545129-01-04454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21200 FCOR143500 FH6800 FCOR46000 FHRRGROUP 32AORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 32EORRRGROUP 33ER 545129-01-09 454DL 454DR 464DL464DRDETAILED INSPECTION OF PYLON AFT UPPER SPAR,WEBCUTOUT BETWEEN RIB 16 AND RIB 17NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24300 FCOR164500 FH7600 FCOR51400 FHGEGROUP 32AORGEGROUP 33AORGEGROUP 33BORGEGROUP 32EORGEGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 37EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545138-01-07N/ADETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR177300 FH5600 FCOR37900 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545138-01-12N/ADETAILED INSPECTION OF PYLON LATERAL PANELS,AREA OF FASTENERS SECURING SUPPORT TO FRONTACCESS DOOR, BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-02-12NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR167000 FH5500 FCOR35700 FHRRGROUP 32APRE 48298545138-02-03N/ASPECIAL DETAILED INSPECTION OF PYLON LATERALPANELS, AREA OF FASTENERS SECURING SUPPORTTO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-07.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR177300 FH11400 FCOR77100 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 38EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545138-02-12N/ASPECIAL DETAILED INSPECTION OF PYLON LATERALPANELS, AREA OF FASTENERS SECURING SUPPORTTO FRONT ACCESS DOOR, BETWEEN RIB 10 AND RIB11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545138-01-12NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR167000 FH11200 FCOR72800 FHRRGROUP 32APRE 48298545140-01-01N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (4750 FC OR 14250 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10500 FCOR63000 FH4500 FCOR27000 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 39EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-01-02N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (3770 FC OR 11310 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11200 FCOR67200 FH3600 FCOR21600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304545140-01-03N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (3060 FC OR 9180 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7900 FCOR47400 FH2900 FCOR17400 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 40EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-01-06N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (4560 FC OR 22800 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9900 FCOR64300 FH4200 FCOR27200 FHGEGROUP 32AORGEGROUP 32EPRE 57304545140-01-07N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (3620 FC OR 18090 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10600 FCOR68900 FH3400 FCOR22100 FHRRGROUP 32AORRRGROUP 32EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 41EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-01-08N/ADETAILED INSPECTION OF PYLON, LATERAL PANELS,AREA OF FASTENERS NEAR UPPER EDGE AT RIB 8LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-02-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (2930 FC OR 14680 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7500 FCOR48700 FH2700 FCOR17500 FHPWGROUP 32AORPWGROUP 32EPRE 57304545140-02-01N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-01.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (7600 FC OR 22800 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10500 FCOR63000 FH7300 FCOR43800FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 42EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-02-02N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-02.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (7100 FC OR 21310 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11200 FCOR67200 FH6800 FCOR40800 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EPRE 57304545140-02-03N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-03.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS REVISED ALI INTERVAL (5630 FC OR 16900 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7900 FCOR47400 FH5400 FCOR32400 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 43EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-02-06N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-06.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (7290 FC OR 36450 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9900 FCOR64300 FH6900 FCOR44800 FHGEGROUP 32AORGEGROUP 32EPRE 57304545140-02-07N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-07.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (6810 FC OR 34080 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10600 FCOR68900 FH6400 FCOR41600 FHRRGROUP 32AORRRGROUP 32EPRE 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 44EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-02-08N/ASPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545140-01-08.THIS ALI TASK SUPERSEDES THE AOT A330-54A3025FOR A/C THAT HAVE ALREADY BEEN INSPECTEDTHROUGH AOT A330-54A3025, NEXT DUE IS WITHINTHIS ALI INTERVAL (5400 FC OR 27030 FH)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7500 FCOR48700 FH5100 FCOR33100 FHPWGROUP 32AORPWGROUP 32EPRE 57304545140-02-09FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10500 FCOR63000 FH7300 FCOR43800FHGEGROUP 33EPOST 57304545140-02-10FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11200 FCOR67200 FH6800 FCOR40800 FHRRGROUP 33EPOST 57304545140-02-11FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7900 FCOR47400 FH5400 FCOR32400 FHPWGROUP 33EPOST 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 45EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545140-02-12FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9900 FCOR64300 FH6900 FCOR44800 FHGEGROUP 32EPOST 57304545140-02-13FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10600 FCOR68900 FH6400 FCOR41600 FHRRGROUP 32EPOST 57304545140-02-14FASTENERSSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, AREA OF FASTENERS NEAR UPPER EDGE ATRIB 8 LEVEL, EXTERNAL SURFACE,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7500 FCOR48700 FH5100 FCOR33100 FHPWGROUP 32EPOST 57304A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 46EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545142-02-01453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6900 FCOR46700 FH6900 FCOR46700 FHGEGROUP 33AORGEGROUP 33BORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545142-02-02453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6200 FCOR41900 FH6200 FCOR41900 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 47EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545142-02-05453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11300 FCOR76500 FH11300 FCOR76500 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33E545142-02-06453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9500 FCOR64300 FH9500 FCOR64300 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545142-02-07453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10800 FCOR70200 FH10800 FCOR70200 FHGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32APOST 48298ORPWGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 48EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545142-02-08453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9100 FCOR59100 FH9100 FCOR59100 FHRRGROUP32APOST 48298ORRRGROUP 32E545142-02-09453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6800 FCOR44200 FH6800 FCOR44200 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE48298545142-02-10453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS MATING SURFACEAND INTERNAL AREA 30 MM AROUND CUTOUTBETWEEN RIB 13 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED6000 FCOR39000 FH6000 FCOR39000 FHRRGROUP 32APRE 48298545143-02-04453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22900 FCOR155000 FH2500 FCOR16900 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 49EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545143-02-13453CL 453CR 463CL463CRDETAILED INSPECTION OF PYLON, LATERAL PANELS,EDGE OF ACCESS DOOR CUTOUTS AND MATINGSURFACE BETWEEN RIB 10 AND RIB 11NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-03-13NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23200 FCOR157000 FH2500 FCOR16900 FHRRGROUP 32APRE 48298545143-03-01453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS ANDMATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22900 FCOR155000 FH6600 FCOR44600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545143-03-13453CL 453CR 463CL463CRSPECIAL DETAILED INSPECTION OF PYLON, LATERALPANELS, EDGE OF ACCESS DOOR CUTOUTS ANDMATING SURFACE BETWEEN RIB 10 AND RIB 11.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 545143-02-13NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23200 FCOR157000 FH6700 FCOR45300 FHRRGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 50EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545146-03-01452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28700 FCOR194200 FH10300 FCOR69700 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545146-03-02452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22200 FCOR150200 FH7300 FCOR49400 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 51EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545146-03-04452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28000 FCOR189500 FH8000 FCOR54100 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545146-03-06452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26800 FCOR174200 FH7600 FCOR49400 FHRRGROUP 32APOST 48298RRGROUP 32E545146-03-07452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28100 FCOR182600 FH10000 FCOR65000 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 52EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545146-03-08452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- HIGH FREQUENCY EDDY CURRENT INSPECTION- THIS TASK IS AN ALTERNATIVE TO TASK 545146-04-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21700 FCOR141000 FH7100 FCOR46100 FHRRGROUP 32APRE 48298545146-04-01452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-01.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28700 FCOR194200 FH6000 FCOR40600 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 53EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545146-04-02452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22200 FCOR150200 FH4100 FCOR27700 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545146-04-04452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28000 FCOR189500 FH4000 FCOR27000 FHRRGROUP 33CPOST 48298ORRRGROUP 33DPOST 48298ORRRGROUP 33E545146-04-06452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26800 FCOR174200 FH3800 FCOR24700 FHRRGROUP 32APOST 48298ORRRGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 54EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545146-04-07452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES :- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28100 FCOR182600 FH5900 FCOR38300 FHGEGROUP 32APRE 48298ORPWGROUP 32APRE 48298545146-04-08452AL 453BL 453BR462AL 463BL 463BRPRE-COOLERRODS, AIR DUCTSPECIAL DETAILED INSPECTION OF PYLON, LOWERSPAR AND LATERAL PANEL JUNCTIONS, BETWEEN RIB6 AND RIB 7.NOTES:- INSPECTION THROUGHFLEXIBLE BOROSCOPE- THIS TASK IS AN ALTERNATIVE TO TASK 545146-03-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21700 FCOR141000 FH4000 FCOR26000 FHRRGROUP 32APRE 48298545150-02-01452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR126000 FH5500 FCOR35400 FHGEGROUP 32APRE 48298ORGEGROUP 33AORGEGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 55EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545150-02-02452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24100 FCOR153600 FH5400 FCOR34200 FHPWGROUP 32APRE 48298ORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298545150-02-08452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED31300 FCOR187800 FH9900 FCOR59400 FHGEGROUP 33E545150-02-09452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29500 FCOR191700 FH9300 FCOR60400 FHGEGROUP 32APOST 48298ORGEGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 56EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545150-02-10452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29800 FCOR189600 FH7100 FCOR45000 FHRRGROUP 32APRE 48298ORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 48298ORRRGROUP 33DPRE 48298545150-02-11452AL 462ALPRE-COOLERRODSAIR DUCTDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERAL PANEL JUNCTIONS, BETWEEN RIB 6 AND RIB8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33300 FCOR216400 FH10000 FCOR65000 FHPWGROUP 32APOST 48298545150-02-14452AL 462ALAIR DUCTPRE-COOLERRODSDETAILED INSPECTION OF PYLON, UPPER SPAR ANDLATERALPANEL JUNCTIONS, BETWEEN RIB 6 AND RIB 8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED35300 FCOR211800 FH10600 FCOR63600 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 57EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545168-02-05452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH6700 FCOR45300 FHGEGROUP 32AORGEGROUP 33AORGEGROUP 33BORGEGROUP 33CORGEGROUP 33DORGEGROUP 33EORGEGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 58EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545168-02-06452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING LINKS AT RIB 12 (4 PLACES PERPYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24900 FCOR168500 FH4400 FCOR29700 FHRRGROUP 32AORRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33EORRRGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 59EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545168-02-13452CL 452CR 462CL462CR 454BL 454BR464BL 464BRDETAILED INSPECTION OF PYLON TO WINGATTACHMENTFITTING LINKS AT RIB 12 (4 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20400 FCOR138100 FH3600 FCOR24300 FHPWGROUP 32AORPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33EORPWGROUP 32E545174-02-03PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH6800 FCOR40800 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CPRE 48298ORPWGROUP 33DPRE 48298ORGEGROUP 33AORGEGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 60EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545174-02-06PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH5600 FCOR33600 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CPRE 50003ORRRGROUP 33DPRE 50003545174-02-07PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH5500 FCOR35700 FHRRGROUP 32APRE 50003R545174-02-09PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH6700 FCOR43500 FHPWGROUP 32APRE 48298ORGEGROUP 32APRE 48298A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 61EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545174-02-12PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH11000 FCOR66000 FHPWGROUP 33CPOST 48298ORPWGROUP 33DPOST 48298ORGEGROUP 33EORPWGROUP 33E545174-02-13PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH10100 FCOR65600 FHPWGROUP 32APOST 48298ORGEGROUP 32APOST 48298ORGEGROUP 32EORPWGROUP 32E545174-02-14PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH8800 FCOR52800 FHRRGROUP 33CPOST 50003ORRRGROUP 33DPOST 50003ORRRGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 62EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY545174-02-15PRE 43271:454DL 454DR 454FL454FR 464DL 464DR464FL 464FRPOST 43271:454KL 454KR 454ML454MR 464KL 464KR464ML 464MRDETAILED INSPECTION OF PYLON TO WINGATTACHEMENT FITTING AND LINKS AT RIB 18A.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33000 FCOR100000 FH8100 FCOR52600 FHRRGROUP 32APOST 50003ORRRGROUP 32E545180-04-04ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR97800 FH13000 FCOR78000 FHGEGROUP 33AORGEGROUP 33BORGEGROUP 33E545180-04-05ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15400 FCOR92400 FH12300 FCOR73800 FHPWGROUP 33AORPWGROUP 33BORPWGROUP 33CORPWGROUP 33DORPWGROUP 33E545180-04-06ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14200 FCOR92300 FH11300 FCOR73400 FHPWGROUP 32AORPWGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 63EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYR 545180-04-07 ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15000 FCOR97500 FH12000 FCOR78000 FHGEGROUP 32AORGEGROUP 32E545180-04-11ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16600 FCOR99600 FH13300 FCOR79800 FHRRGROUP 33AORRRGROUP 33BORRRGROUP 33CORRRGROUP 33DORRRGROUP 33E545180-04-12ENGINELINKSSLEEVESAFT SECONDARYSTRUCTURESPECIAL DETAILED INSPECTION OF PYLON TO WINGATTACHMENT FITTING SLEEVES AND BOLTS AT RIB18A (3 PLACES PER PYLON)NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR99400 FH12200 FCOR79300 FHRRGROUP 32AORRRGROUP 32E551008-01-06312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN SPANWISE SPLICES BETWEENFUSELAGE FAIRING LINES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR104100 FH7500 FCOR50700 FHGROUP 33A551008-01-07312AR313ALDETAILED INSPECTION OF HORIZONTAL STABILIZERCENTER BOX TOP SKIN SPANWISE SPLICES BETWEENFUSELAGE FAIRING LINES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR104100 FH6900 FCOR46700 FHGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 64EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY551015-01-04312ARGENERAL VISUAL INSPECTION OF HORIZONTALSTABILIZER CENTER BOX FRONT SPAR FORWARDFACE FROM RIB 3 LH TO RIB 3 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16900 FCOR114800 FH16900 FCOR114800 FHGROUP 33AORGROUP 33B551016-01-06313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN REAR UPPERFLANGE JUST OUTBOARD OF RIB 3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26500 FCOR179700 FH22100 FCOR149600 FHGROUP 33A551016-01-07313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN REAR UPPERFLANGE JUST OUTBOARD OF RIB 3, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26500 FCOR179700 FH18400 FCOR124800 FHGROUP 33B551019-01-04313ALSPECIAL DETAILED INSPECTION OF HORIZONTALSTABILIZER CENTER BOX TOP SKIN INTERGRALFLANGE AT ATTACHMENT TO REAR SPAR WEB FROMRIB 3 LH TO RIB 3 RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18900 FCOR128400 FH3100 FCOR20200 FHGROUP 32E571107-01-01191QB 192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, DRAIN HOLES AT Y=2427BETWEEN STRINGERS 20 & 21, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR171200 FH4700 FCOR30700 FHGROUP 32A571107-01-04191QB 192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, DRAIN HOLES AT Y=2427BETWEEN STRINGERS 20 & 21, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24900 FCOR168600 FH5200 FCOR35300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 65EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571108-01-05147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, LOWER SKIN PANEL ANDSTIFFENERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29600 FCOR200600 FH7000 FCOR47700 FHGROUP 33AORGROUP 33B571108-01-06147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOXINTERNAL STRUCTURE, LOWER SKIN PANEL ANDSTIFFENERS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29400 FCOR191500 FH6700 FCOR43700 FHGROUP 32A571114-01-05147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25000 FCOR169600 FH10900 FCOR73900 FHGROUP 33AORGROUP 33B571114-01-06147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19900 FCOR129600 FH9800 FCOR63800 FHGROUP 32APRE 49202ORGROUP 32APOST 50755571114-01-07147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, DRAIN HOLES ATSTIFFENERS 27 AND 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22100 FCOR150100 FH10000 FCOR68200 FHGROUP 33DPRE 49202ORGROUP 33CPRE 49202571116-01-02193DBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, FUEL LEVEL MAGNETICINDICATOR AREA BETWEEN STRINGERS 21 & 22, AT Y=-567.5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR171200 FH4700 FCOR30700 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 66EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571116-01-04193DBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, FUEL LEVEL MAGNETICINDICATOR AREA BETWEEN STRINGERS 21 & 22, AT Y=-567.5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24900 FCOR168600 FH5200 FCOR35300 FHGROUP 33AORGROUP 33B571118-01-06FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTORS AREAAT Y=-2230 BETWEEN STRINGERS 25 & 26, AND ATY=180 BETWEEN STRINGERS 27 & 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR171200 FH4700 FCOR30700 FHGROUP 32A571118-01-07FAIRING PANELSBETWEEN FR.44 ANDFR.47SPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, HYDRAULIC CONNECTORS AREAAT Y=-2230 BETWEEN STRINGERS 25 & 26, AND ATY=180 BETWEEN STRINGERS 27 & 28.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24900 FCOR168600 FH5200 FCOR35300 FHGROUP 33AORGROUP 33B571121-01-03734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1959NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24500 FCOR152800 FH18700 FCOR116800 FHGROUP 33AORGROUP 33BORGROUP 32AORGROUP 33CORGROUP 33D571121-01-04734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1960NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25500 FCOR153000 FH19400 FCOR116800 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 67EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571121-01-05734 744SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, LONGITUDINAL BEAM FITTINGAND LONGITUDINAL BEAM AT JUNCTION WITH CWBAFT PANEL FROM Y=-1959 TO Y=1961NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24500 FCOR159400 FH18700 FCOR121900 FHGROUP 32E571123-01-01CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19900 FCOR119600 FH7800 FCOR47000 FHGROUP 33APOST 49404ORGROUP 33BPOST 49404571123-01-02CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18500 FCOR111200 FH6500 FCOR39300 FHGROUP 33CPOST 49404ORGROUP 33DPOST 49404571123-01-03CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14100 FCOR91700 FH4500 FCOR29600 FHGROUP 32APOST 49404571123-01-04CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19000 FCOR114000 FH7600 FCOR45700 FHGROUP 33EPOST 49404571123-01-05CABIN FLOOR PANELSNOTE 1SPECIAL DETAILED INSPECTION OF FUSELAGEINTERNAL STRUCTURE, FRAME FOOT JUNCTION WITHLATERAL FRAME FROM FR 40.3 TO FR 45, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR95700 FH5200 FCOR34400 FHGROUP 32EPOST 49404A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 68EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571125-01-03734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23400 FCOR158800 FH5200 FCOR35200 FHGROUP 33AORGROUP 33B571125-01-04734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16700 FCOR108700 FH3300 FCOR22000 FHGROUP 32A571125-01-05734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR AFT FACE, FASTENERS AREABETWEEN Y=2219 AND FRAME 47 LOWER CORNERFITTING, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18200 FCOR123300 FH3500 FCOR23800 FHGROUP 33CORGROUP 33D571126-01-03734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR174100 FH11400 FCOR77600 FHGROUP 33AORGROUP 33B571126-01-04734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21000 FCOR136500 FH9400 FCOR61000 FHGROUP 32APRE 49202ORGROUP 32APOST 50755571126-01-05734SPECIAL DETAILED INSPECTION OF CENT WING BOX,REAR SPAR WEB AT APU FUEL PUMP APERTURE INTHE LEFT SIDE LOWER CORNER.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22400 FCOR151600 FH9600 FCOR65300 FHGROUP 33DPRE 49202ORGROUP 33CPRE 49202A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 69EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571129-01-04147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX,CENTER SPAR, 30MM AROUND ACCESS CUT-OUTS (2PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED34300 FCOR232100 FH12700 FCOR86200 FHGROUP 33AORGROUP 33B571130-01-03147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX, REAR SPAR, 30 MMAROUND MANHOLE CUTOUTS (2 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED34300 FCOR232100 FH7300 FCOR49500 FHGROUP 33AORGROUP 33BR 571130-01-04 147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX, REAR SPAR, 30 MMAROUND MANHOLE CUTOUTS (2 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED31800 FCOR207000 FH6500 FCOR42300 FHGROUP 32APRE 49202ORGROUP 32APOST 50755ORGROUP 33DPRE 49202ORGROUP 33CPRE 49202571133-01-01147AZ 148AZ 734744DETAILED INSPECTION OF CENTER WING BOX, STRUTLUGS ON LONGITUDINALSTIFFENERS AND RODFITTING CONNECTIONS (63 PLACES).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24300 FCOR158500 FH11900 FCOR77600 FHGROUP 32AORGROUP 33CORGROUP 33D571144-01-01191HB 191QB 192HB192QBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX, LOWER SPLICE AT RIB 1, FIRST FASTENER ROWSON EACH SIDE OF RIB 1 DATUM AT STR.16, STR.20,STR.21 AND STR.25 TO 29 FOR INBOARD RIVET ROW,AND AT STR.11, STR.14, STR.18 TO 20 AND STR.23 TO28 FOR OUTBOARD RIVET ROW, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED31100 FCOR211000 FH7900 FCOR47900 FHGROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 70EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571145-01-01147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26100 FCOR176800 FH6300 FCOR38100 FHGROUP 33A571145-01-03147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25100 FCOR163600 FH6600 FCOR43300 FHGROUP 32A571145-01-04147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR173900 FH7100 FCOR42800 FHGROUP 33E571145-01-05147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24600 FCOR159900 FH6500 FCOR42400 FHGROUP 32E571145-01-06147AZ 148AZ 734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, RIB 1 LOWER T FITTINGINBOARD FLANGE, FASTENERS IN RADIUS AREA ATSTR.16, STR.20, STR.21 AND STR.25 TO 29, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27100 FCOR183400 FH7400 FCOR44400 FHGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 71EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571146-02-04191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR177400 FH8000 FCOR54500 FHGROUP 33AORGROUP 33B571146-02-05191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22100 FCOR143900 FH6800 FCOR44400 FHGROUP 32A571146-02-06191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23300 FCOR157800 FH6700 FCOR45800 FHGROUP 33E571146-02-07191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22400 FCOR145600 FH6600 FCOR43500 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 72EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571146-02-08191QB 192QB191HB 192HBSPECIAL DETAILED INSPECTION OF CENTER WINGBOX LOWER PANEL, LOWER SURFACE, FIRSTFASTENER ROW ON EACH SIDE OF RIB1 BUTT STRAPEDGE, AT STR16, STR20, STR21 AND STR25 TO STR29,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23600 FCOR159900 FH7000 FCOR47500 FHGROUP 33CORGROUP 33D571152-01-02147AZ 148AZ 734744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, CENTER SPAR FITTINGFLANGE, RADIUS AREA AT FASTENERS 3 TO 4 LEVELAND FLANGE AT FASTENERS 3 TO 12, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR111700 FH5500 FCOR37600 FHGROUP 33A571153-01-01147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17200 FCOR116600 FH11900 FCOR80800 FHGROUP 33E571153-01-02147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16600 FCOR107900 FH11500 FCOR74800 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 73EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571153-01-03147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10900 FCOR73900 FH7550 FCOR51300 FHGROUP 33APOST 43577ORGROUP 33BPOST44440S13324571153-01-04147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR103500 FH11900 FCOR80800 FHGROUP 33CORGROUP 33DR 571153-01-05 147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16600 FCOR112900 FH13300 FCOR90300 FHGROUP 33BPOST44440S13276ORGROUP 33BPOST44440S13090ORGROUP 33BPOST 44360571153-01-06147AZ 148AZ734 744SEALANT TO BEREMOVEDSPECIAL DETAILED INSPECTION OF CENTER WINGBOX INTERNAL STRUCTURE, STIFFENING RIB ANDRADIUS OF GUSSET INSTALLED ON LOWER L FITTINGAT CROSSING AREA WITH KEEL BEAM FITTING ATFR.40, AND LOWER L FITTING RADIUS ON EACH SIDEOF GUSSET, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR95800 FH11500 FCOR74800 FHGROUP 32AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 74EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571159-01-03CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26400 FCOR179200 FH8800 FCOR59800 FHGROUP 33AORGROUP 33B571159-01-04CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23800 FCOR155000 FH8100 FCOR53200 FHGROUP 32A571159-01-05CABIN FLOOR PANELSSPECIAL DETAILED INSPECTION OF CENTER WINGBOX PORTAL BEAMS ATCONNECTION WITH FRONTSPAR VERTICAL STIFFENERS FROM Y=-1959 TO Y=1959(9 BEAMS).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25100 FCOR170000 FH8400 FCOR57200 FHGROUP 33CORGROUP 33D571162-01-01191HB 192HBSPECIAL DETAILED INSPECTION OF KEEL BEAMFITTING, TWO FASTENERS HOLES IN CONNECTION OFKEEL BEAM FITTING TO CWB BOTTOM PANEL AT STR.1LEVEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11500 FCOR78200 FH6650 FCOR45200 FHGROUP 33APOST 43577POST 54459A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 75EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITYR 571163-01-01 191HB 192HBSPECIAL DETAILED INSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11000 FCOR74800 FH5300 FCOR36100 FHGROUP 33BPOST 56467ORGROUP 33CPOST 56467POST 44360ORGROUP 33DPOST 56467POST 44360ORGROUP 33EPOST 56467POST 49202PRE 55306ORGROUP 33EPOST 56467POST 49202PRE 55792R 571163-01-02 191HB 192HBSPECIAL DETAILED INSPECTION OF FRAME 40 NODE,FASTENER HOLE AT JUNCTION BETWEEN KEEL BEAMFITTING AND LOWER PANEL, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9700 FCOR63100 FH4650 FCOR30400 FHGROUP 32APOST 56467POST 44360ORGROUP 32EPOST 56467POST 49202PRE 55306ORGROUP 32EPOST 56467POST 49202PRE 55792A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 76EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY571164-01-02191HB 192HBDETAILED INSPECTION OF FUSELAGE EXTERNALSTRUCTURE, KEEL BEAM FITTING ANGLE ANDDOUBLER AT FR 40, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16400 FCOR106900 FH6900 FCOR44900 FHGROUP 32EPOST 55306ORGROUP 32EPOST 55792ORGROUP 33EPOST 55306ORGROUP 33EPOST 55792571165-01-03734 744SPECIAL DETAILED INSPECTION OF CENTER WINGBOX REAR SPAR, FILET RADIUS FROM Y=1959 TOY=2219 AND FROM Z=-1859.6 TO Z=-2073, LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9300 FCOR63400 FH5800 FCOR39200 FHGROUP 33APRE 43865ORGROUP 33BPRE 43865572002-01-05 454DL 454DR 454FL454FR 464DL 464DR464FL 464FRSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIBBAY 10-10ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24400 FCOR146400 FH4600 FCOR28100 FHGROUP 33APRE 43271ORGROUP 33BPRE 43271572002-01-08454KL 454KR 454ML454MR 464KL 464KR464ML 464MRSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN MASKED BY PYLON DIAPHRAGM IN RIBBAY 10-10ANOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24400 FCOR146400 FH4600 FCOR28100 FHGROUP 33APOST 43271ORGROUP 33BPOST 43271572004-02-01FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23400 FCOR152700 FH4100 FCOR26800 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 77EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572004-02-03FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24500 FCOR147200 FH6300 FCOR37900 FHGROUP 33AORGROUP 33B572004-02-04FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR143800 FH4200 FCOR25200 FHGROUP 33CPRE 48437572004-02-05FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 12 EXCLUDING AREASCOVERED BY MAIN LANDING GEAR REINFORCINGPLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR143800 FH3300 FCOR19800 FHGROUP 33DPRE 48437572005-01-06541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18900 FCOR113600 FH3200 FCOR19200 FHGROUP 33CPRE 48437572005-01-07541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19600 FCOR127500 FH3000 FCOR19500 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 78EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572005-01-08541BB 541CB 641BB641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20800 FCOR125300 FH6500 FCOR39200 FHGROUP 33APRE 41114ORGROUP 33BPRE 41114572005-01-09541CB 641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN FORWARD OF REAR SPAR IN AREAMASKED BY MAIN LANDING GEAR REINFORCINGPLATE INCLUDING ATTACHMENT TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20800 FCOR125300 FH6500 FCOR39200 FHGROUP 33APOST 41114ORGROUP 33BPOST 41114572005-01-12541CB 641CBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINFORWARD OF REAR SPAR IN AREA MASKED BY MAINLANDINGGEAR REINFORCING PLATE INCLUDING ATTACHMENTTO REARSPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18900 FCOR113600 FH2500 FCOR15100 FHGROUP 33DPRE 48437572006-02-09N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE MAIN LANDING GEARREINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27000 FCOR175500 FH5700 FCOR37300 FHGROUP 32APRE 48437572006-02-10N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE MAIN LANDING GEARREINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24300 FCOR146100 FH5300 FCOR32100 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 79EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572009-01-04454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR129300 FH3900 FCOR25700 FHGROUP 32APRE 48437572009-01-05454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20200 FCOR121000 FH3700 FCOR22400 FHGROUP 33AORGROUP 33B572009-01-06454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT STRINGERRUN-OUTS, STR 1 (RIBBAY 2-3), STR 2 (RIB BAY 4-5), STR 3 (RIB BAY 6-7), STR4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIBBAY 8-9), STR 27 (RIB BAY 4-5) AND STR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-02-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19900 FCOR119700 FH4100 FCOR24600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 80EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572009-02-04454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR129300 FH10200 FCOR50000 FHGROUP 32APRE 48437572009-02-05454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20200 FCOR121000 FH6800 FCOR41000 FHGROUP 33AORGROUP 33B572009-02-06454GL 454GR 464GL464GR 531AB 631ABINBOARD FUEL PUMPFAIRINGSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT STRINGER RUNOUTS, STR 1 (RIB BAY 2-3), STR 2 (RIB BAY 4-5), STR 3(RIB BAY 6-7), STR 4 (RIB BAY 8-9), STR 25 (RIB BAY 11-12), STR 26 (RIB BAY 8-9), STR 27 (RIB BAY 4-5) ANDSTR 28 (RIB BAY 2-3)NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572009-01-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19900 FCOR119700 FH10600 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 81EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572012-02-01FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24800 FCOR161600 FH4000 FCOR26200 FHGROUP 32APRE 48437572012-02-02FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20500 FCOR123200 FH5200 FCOR31500 FHGROUP 33AORGROUP 33B572012-02-03FUEL PUMP FAIRINGSDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 1 AND RIB 3 ANDBETWEEN RIB 10 AND RIB 12 FROM FRONT SPAR TOREAR SPAR EXCLUDING AREAS COVERED BY PYLONFAIRING AND PYLON REINFORCING PLATE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26100 FCOR156800 FH4000 FCOR24000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572014-02-02N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE SPANWISE SKIN JOINTS AT SRINGER13 AND STRINGER 20 BETWEEN RIB 1 AND RIB 12EXCLUDING AREAS COVERED BY FAIRINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26700 FCOR160600 FH5900 FCOR35600 FHGROUP 33AORGROUP 33B572016-02-08FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN VISIBLE SURFACES OF FUEL PUMPAPERTURES BETWEEN RIB 2 AND RIB 4.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21000 FCOR126400 FH5800 FCOR35000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 82EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572016-02-09FUEL PUMP FAIRINGSSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN VISIBLE SURFACES OF FUEL PUMPAPERTURES BETWEEN RIB 2 AND RIB 4.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15700 FCOR102200 FH5300 FCOR34400 FHGROUP 32APOST 48437ORGROUP 32E572019-01-05541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR164300 FH5500 FCOR36000 FHGROUP 32APRE 48437572019-01-06541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24200 FCOR145700 FH7100 FCOR43000 FHGROUP 33AORGROUP 33B572019-01-11541EB 541FB 541GB641EB 641FB 641GBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS BETWEEN RIB 9 AND RIB 12, EXCLUDINGSTRINGERS 15 & 18 AND BUTTSTRAPS AT STRINGERS13 & 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26000 FCOR156000 FH5400 FCOR32800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572023-02-03N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20100 FCOR131100 FH2500 FCOR16500 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 83EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572023-02-04N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18500 FCOR111200 FH2800 FCOR17300 FHGROUP 33AORGROUP 33B572023-02-05N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINAT STRINGER ATTACHMENTS BETWEEN RIB 3 AND RIB10 FROM FRONT SPAR TO REAR SPAR EXCLUDINGAREAS COVERED BY PYLON FAIRING ANDREINFORCING PLATE, MAIN LANDING GEARREINFORCING PLATE AND FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21600 FCOR129900 FH2700 FCOR16200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572027-01-05541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23600 FCOR153700 FH6000 FCOR39400 FHGROUP 32APRE 48437572027-01-06541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20200 FCOR121300 FH9200 FCOR50000 FHGROUP 33AORGROUP 33B572027-01-10541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 1 AND RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24800 FCOR148900 FH6600 FCOR39700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 84EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572032-01-04N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9600 FCOR62900 FH6300 FCOR41400 FHGROUP 32APRE 48437572032-01-05 N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15900 FCOR47300 FH7600 FCOR45800 FHGROUP 33APOST 46110PRE 43503ORGROUP 33BPOST 46110PRE 43503572032-01-06N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10100 FCOR61000 FH5800 FCOR35000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572032-01-07N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10100 FCOR61000 FH9300 FCOR56300 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572032-01-09N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9600 FCOR62900 FH7000 FCOR45500 FHGROUP 32APOST 48437ORGROUP 32E572032-01-12N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE AT ATTACHMENT TO REAR SPARBETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13000 FCOR78300 FH7600 FCOR45800 FHGROUP 33APOST 43503ORGROUP 33BPOST 43503A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 85EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572033-01-04N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14500 FCOR94300 FH4500 FCOR29300 FHGROUP 32APRE 48437572033-01-05N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR95100 FH6900 FCOR41900 FHGROUP 33AORGROUP 33B572033-01-06N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR86200 FH4800 FCOR29300 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572033-01-08N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR86200 FH7200 FCOR43200 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572033-01-09N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 1 AND RIB 12 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14500 FCOR94300 FH5600 FCOR36800 FHGROUP 32APOST 48437ORGROUP 32E572035-01-05N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE FROM STRINGER 12 TO 19 ANDFROM RIB 4 TO RIB 8.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25100 FCOR150600 FH7900 FCOR47600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 86EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572037-01-05541AB 541AZ 541BB541BZ 541CB 541CZ541DB 541DZ 541EZ541FZ 641AB 641AZ641BB 641BZ 641CB641CZ 641DB 641DZ641EZ 641FZDETAILED INSPECTION OF OUTER WING TOP SKINSTRINGER ASSEMBLIES BETWEEN RIB 1 AND RIB 9AND TOP SKIN LOWER SURFACE AT ROOT JOINTFROM FRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22200 FCOR133400 FH9800 FCOR50000 FHGROUP 33AORGROUP 33B572043-01-05573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25100 FCOR150700 FH7100 FCOR42700 FHGROUP 33AORGROUP 33B572043-01-06573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33100 FCOR199000 FH11000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572043-01-10573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFTFACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED32300 FCOR194100 FH6800 FCOR41000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572043-01-11573FB 673FBDETAILED INSPECTION OF OUTER WING REAR SPARAFTFACE SPAR JOINT PLATE AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28400 FCOR184900 FH6000 FCOR39000 FHGROUP 32APOST 48437572046-01-04541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23300 FCOR151800 FH5500 FCOR35700 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 87EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572046-01-05541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR121800 FH8700 FCOR50000 FHGROUP 33APOST 46111ORGROUP 33B572046-01-07541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22900 FCOR137700 FH5900 FCOR35400 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572046-01-09541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20700 FCOR134500 FH5300 FCOR34600 FHGROUP 32EORGROUP 32APOST 48437572046-01-11541AB 541BB 541CB541DB 541EB 541FB641AB 641BB 641CB641DB 641EB 641FBDETAILED INSPECTION OF OUTER WING REAR SPARFORWARD FACE BETWEEN RIB 7 AND RIB 11INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21000 FCOR126200 FH4900 FCOR29600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572047-01-03541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR170400 FH20000 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 88EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572047-01-04541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26100 FCOR156600 FH20000 FCOR50000 FHGROUP 33AORGROUP 33B572047-01-05541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24500 FCOR147100 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572047-01-06541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29900 FCOR179800 FH17300 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572047-01-09541AB 541BB 541BZ541CB 541CZ 641AB641BB 641BZ 641CB641CZSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE AT MLG FITTINGS (GEARRIB 6, FORWARD PINTLE FITTING, RETRACTION JACKFITTING AND SIDESTAY FITTING) BOLTING AREAS ANDTOP ANGLE BRACKET BETWEEN RIB 1 AND RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27800 FCOR180700 FH16000 FCOR50000 FHGROUP 32APOST 48437572049-01-04531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22400 FCOR145900 FH12400 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 89EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572049-01-05531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED30800 FCOR185100 FH8000 FCOR48200 FHGROUP 33AORGROUP 33B572049-01-06531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22500 FCOR135300 FH12400 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572049-01-08531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21200 FCOR127600 FH9000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572049-01-09531AB 631ABSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR UPPER AND LOWER FLANGE JOINTSTRAPS AT RIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19200 FCOR125200 FH8100 FCOR50000 FHGROUP 32APOST 48437ORGROUP 32E572050-01-04573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26700 FCOR173600 FH7500 FCOR49000 FHGROUP 32APRE 48437572050-01-05573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17900 FCOR107700 FH8600 FCOR51600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 90EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572050-01-07573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27600 FCOR166000 FH8500 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572050-01-09573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21300 FCOR138900 FH20000 FCOR50000 FHGROUP 32APOST 48437572050-01-10573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR143400 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572050-01-11573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23900 FCOR143400 FH17000 FCOR50000 FHGROUP 33E572050-01-12573DB 673DBDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE UPPER ATTACHMENT ANGLE FROM RIB 4 TORIB 7 AND LOWER ATTACHMENT ANGLE FROM RIB 1TO RIB 7.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21300 FCOR138900 FH17000 FCOR50000 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 91EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572051-01-05DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15300 FCOR99900 FH3400 FCOR22400 FHGROUP 32APRE 48437572051-01-06DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23700 FCOR142600 FH3700 FCOR22500 FHGROUP 33APOST 46241ORGROUP 33BPOST 46241572051-01-07DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9700 FCOR58600 FH3700 FCOR22500 FHGROUP 33APOST 42547ORGROUP 33BPOST 42547572051-01-08DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15500 FCOR93300 FH3700 FCOR22600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572051-01-10FLAPS EXTENDEDSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPARAFT FACE AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18200 FCOR118300 FH4400 FCOR29100 FHGROUP 32EORGROUP 32APOST 48437572051-01-12DEPLOY FLAPSSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AT BUILD SLOT BETWEEN RIBS 1 & 2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22300 FCOR134100 FH5500 FCOR33000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572052-03-01 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20900 FCOR96500 FH7800 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 92EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572052-03-02 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16000 FCOR51200 FH7100 FCOR42800 FHGROUP 33APOST 46110ORGROUP 33BPRE 43503POST 46110572052-03-04541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17700 FCOR106700 FH6700 FCOR40600 FHGROUP 33BPOST 43503572052-03-05541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17800 FCOR106900 FH8800 FCOR53300 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572052-03-06 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23600 FCOR73900 FH9400 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572052-03-07 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23600 FCOR73900 FH9400 FCOR50000 FHGROUP 33E572052-03-08 541BB 541CB 641BB641CBSEALANT REMOVAL ASPER NTM.SPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR FORWARD FACE BETWEEN RIB 1 AND RIB7 INCLUDING TOP AND BOTTOM FLANGE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR119300 FH8300 FCOR50000 FHGROUP 32EORGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 93EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572054-01-05DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR103000 FH6300 FCOR41000 FHGROUP 32APRE 48437572054-01-07DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11600 FCOR70000 FH7700 FCOR46400 FHGROUP 33APOST 43503ORGROUP 33BPOST 43503572054-01-08DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15000 FCOR90400 FH6700 FCOR40200 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572054-01-10DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13700 FCOR89400 FH6100 FCOR39800 FHGROUP 32APOST 48437ORGROUP 32E572054-01-11DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12700 FCOR76300 FH4800 FCOR29000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572054-01-13DEPLOY FLAPSSPECIAL DETAILED INSPECTION OF OUTER WINGREAR SPAR AFT FACE SYSTEMS HOLE BETWEEN RIBS4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105200 FH4400 FCOR26700 FHGROUP 33APOST 46141ORGROUP 33BPOST 46141A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 94EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572067-01-05541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12800 FCOR77000 FH2700 FCOR16300 FHGROUP 33APRE 41114572067-01-15541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29500 FCOR177100 FH3600 FCOR22000 FHGROUP 33APOST 54219ORPOST 53883ORGROUP 33BPOST 54219ORPOST 53883572067-01-17541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19200 FCOR115600 FH3700 FCOR22700 FHGROUP 33CPOST 54219PRE 48437ORGROUP 33CPOST 53883PRE 48437ORGROUP 33DPOST 54219PRE 48437ORGROUP 33DPOST 53883PRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 95EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572067-03-03541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19200 FCOR115600 FH3700 FCOR22700 FHGROUP 33CPOST 54219PRE 48437ORGROUP 33CPOST 53883PRE 48437ORGROUP 33DPOST 54219PRE 48437ORGROUP 33DPOST 53883PRE 48437R 572067-03-05 541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZSPECIAL DETAILED INSPECTION OF OUTER WING RIB 6FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29500 FCOR177100 FH3600 FCOR22000 FHGROUP 33APOST 54219ORGROUP 33APOST 53883ORGROUP 33BPOST 54219ORGROUP 33BPOST 53883572068-01-04541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR167500 FH20000 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 96EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572068-01-05541CB 541DB 541EZ541FZ 641CB 641DB641EZ 641FZDETAILED INSPECTION OF OUTER WING RIB 7FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26200 FCOR157200 FH3700 FCOR22500 FHGROUP 33AORGROUP 33BR 572068-01-13 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18600 FCOR111900 FH18600 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437R 572069-01-04 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18400 FCOR119600 FH18400 FCOR50000 FHGROUP 32APRE 48437572069-01-05541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR94800 FH4100 FCOR24800 FHGROUP 33AA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 97EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572069-01-06541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR94800 FH3700 FCOR22700 FHGROUP 33BR 572069-01-08 541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19800 FCOR118800 FH19800 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572069-01-11541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23100 FCOR138600 FH10300 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572069-01-12541DB 541FZ 641DB641FZDETAILED INSPECTION OF OUTER WING RIBS 8 AND 9FORWARD AND AFT OF CENTER SPAR AT SKINATTACHMENTS INCLUDING CLEATS, SPARATTACHMENTS, REGION OF STRINGER CUTOUTS ANDACCESS CUTOUT SURROUNDS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22000 FCOR143000 FH9800 FCOR50000 FHGROUP 32APOST 48437ORGROUP 32E572081-01-05541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18700 FCOR121700 FH10100 FCOR65700 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 98EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572081-01-06541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14800 FCOR89300 FH6100 FCOR36900 FHGROUP 33APOST 43272572081-01-07541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19700 FCOR118300 FH6800 FCOR40800 FHGROUP 33B572081-01-08541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105400 FH8800 FCOR52900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572081-01-13541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR108500 FH15500 FCOR93500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E572081-01-14541AB 541AZ 641AB641AZDETAILED INSPECTION OF OUTER WING CENTER SPARASSEMBLY FORWARD FACE BETWEEN RIB 1 AND RIB2.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR117500 FH15500 FCOR101300 FHGROUP 32APOST 48437ORGROUP 32E572082-01-06541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15200 FCOR91200 FH8100 FCOR48800 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 99EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572082-01-08541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23000 FCOR138000 FH5100 FCOR30900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572082-01-10541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23000 FCOR149500 FH5100 FCOR33500 FHGROUP 32APOST 48437ORGROUP 32E572082-01-12541AB 541AZ 541BB541CB 541DB 541DZ541EB 541EZ 541FB541FZ 641AB 641AZ641BB 641CB 641DB641DZ 641EB 641EZ641FB 641FZDETAILED INSPECTION OF OUTER WING CENTER SPARBETWEEN RIB 2 AND RIB 11 FORWARD AND AFT FACESCOMPRISING SKIN ATTACHMENTS, RIB ATTACHMENTS,AREA AROUND ACCESS HOLES, DRAIN AND VENTHOLES AND CONDUIT HOLES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25200 FCOR151400 FH4700 FCOR28200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572084-01-01541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26700 FCOR180900 FH8300 FCOR49800 FHGROUP 33A572084-01-03541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19200 FCOR124800 FH9300 FCOR60600 FHGROUP 32AORGROUP 33CA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 100EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572084-01-04541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19600 FCOR132600 FH9900 FCOR59800 FHGROUP 33E572084-01-05541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18700 FCOR122000 FH9100 FCOR59300 FHGROUP 32E572084-01-06541AB 641ABSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WING BOXINTERNAL STRUCTURE RIB 1 LOWER T FITTINGOUTBOARD FLANGE IN RADIUS AREA AT STR. 11, STR.14, STR. 18 TO 20 AND AT STR. 23 TO 28 LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20600 FCOR139900 FH10300 FCOR62000 FHGROUP 33D572092-01-04541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19500 FCOR127000 FH7300 FCOR47700 FHGROUP 32APRE 48437572092-01-05541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18200 FCOR109500 FH6200 FCOR37300 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 101EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572092-01-06541EB 541FB 641EB641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 15 AND STRINGER 18 BETWEEN RIB 9 ANDRIB 12, EXCLUDING JOINT OF STRINGER 15 TOCENTER SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20500 FCOR123000 FH7700 FCOR46500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572093-01-07541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-02-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20000 FCOR120500 FH5500 FCOR33500 FHGROUP 33AMSN 0050AND SUBSORGROUP 33B572093-01-08541FB 641FBDETAILED INSPECTION OF OUTER WING BOTTOM SKINJOINT OF STRINGER 15 TO CENTER SPARNOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-02-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17400 FCOR104700 FH5500 FCOR33500 FHGROUP 33AUP TO MSN 0045POST 45415572093-02-07541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN JOINT OF STRINGER 15 TO CENTERSPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-01-07NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20000 FCOR120500 FH5500 FCOR33500 FHGROUP 33AMSN 0050AND SUBSORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 102EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572093-02-08541FB 641FBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN JOINT OF STRINGER 15 TO CENTERSPAR.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572093-01-08NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17400 FCOR104700 FH5500 FCOR33500 FHGROUP 33AUP TO MSN 0045POST 45415572094-01-06541EB 541FB 541GB641EB 641FB 641GBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN BUTTSTRAP AT STRINGER 13 &STRINGER 20 BETWEEN RIB 9 AND RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23400 FCOR140800 FH9200 FCOR50000 FHGROUP 33AORGROUP 33B572107-01-05N/ASPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE AT RUNOUTS OFSTRINGER BETWEEN RIB 23 AND RIB 39.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-02-05NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20800 FCOR125200 FH3700 FCOR22700 FHGROUP 33AORGROUP 33B572107-02-05N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT RUNOUTS OF STRINGERBETWEEN RIB 23 AND RIB 39.NOTE: THIS TASK IS AN ALTERNATIVE TO TASK 572107-01-05NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20800 FCOR125200 FH2000 FCOR12400 FHGROUP 33AORGROUP 33B572109-02-05542EB 542FB 542GB542HB 542JB 542KB550AB 550BB 550CB550DB 550EB 550FB642EB 642FB 642GB642HB 642JB 642KB650AB 650BB 650CB650DB 650EB 650FBSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN UPPER AND LOWER SURFACESAROUND ACCESS DOOR CUTOUTS, INCLUDING NACADUCT, IN ALL BAYS BETWEEN RIBS 27 AND 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20500 FCOR123400 FH4700 FCOR28200 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 103EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572110-01-04N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20100 FCOR131200 FH9800 FCOR50000 FHGROUP 32APRE 48437572110-01-05N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21300 FCOR128200 FH10000 FCOR50000 FHGROUP 33AORGROUP 33B572110-01-06N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE BETWEEN RIB 12 AND RIB 23 FROMFRONT SPAR TO REAR SPAR EXCLUDING AREASCOVERED BY FLAP TRACK FAIRINGS 3, 4 AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21600 FCOR129900 FH10400 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572111-01-04532AB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13400 FCOR87400 FH7700 FCOR50100 FHGROUP 32APRE 48437572111-01-05532AB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13700 FCOR82600 FH8900 FCOR53400 FHGROUP 33AORGROUP 33B572111-01-06532AB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR86200 FH8200 FCOR49400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 104EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572111-01-09532AB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21900 FCOR142400 FH4800 FCOR31800 FHGROUP 32E572111-01-10532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWERSURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25400 FCOR152500 FH5600 FCOR34000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572111-01-11532AB 532CB 533AB533CB 534AB 534CB632AB 632CB 633AB633CB 634AB 634CBDETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWERSURFACE IN AREAS COVERED BY FLAP TRACKFAIRINGS 3,4AND 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21900 FCOR142400 FH4800 FCOR31800 FHGROUP 32APOST 48437572116-02-01N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE SPANWISE SKINJOINTS AT STRINGER 13 AND STRINGER 20 BETWEENRIB 12 AND RIB 27 EXCLUDING AREAS COVERED BYFLAP TRACK FAIRINGS 3, 4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23600 FCOR153500 FH3200 FCOR21200 FHGROUP 32APRE 48437572116-02-02N/AGENERAL VISUAL INSPECTION OF OUTER WINGBOTTOM SKIN LOWER SURFACE SPANWISE SKINJOINTS AT STRINGER 13 AND STRINGER 20 BETWEENRIB 12 AND RIB 27 EXCLUDING AREAS COVERED BYFLAP TRACK FAIRINGS 3, 4 & 5.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23800 FCOR143300 FH4600 FCOR27600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 105EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572119-02-05N/ADETAILED INSPECTION OF OUTER WING BOTTOM SKINLOWER SURFACE AT DRAIN HOLES FOR SLAT CANS,MLI HOLES AND DRAIN HOLES AFT OF FRONT SPARAND FORWARD OF REAR SPAR, BETWEEN RIBS 12AND 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED32000 FCOR112100 FH7500 FCOR48800 FHGROUP 32APOST 48437ORGROUP 32E572121-01-04541GB 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16400 FCOR107000 FH5900 FCOR38600 FHGROUP 32APRE 48437572121-01-05541GB 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17000 FCOR102500 FH5400 FCOR32600 FHGROUP 33AORGROUP 33B572121-01-07541GB 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105400 FH6300 FCOR37900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 106EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572121-01-08541GB 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 ATSTRINGERS 13 AND 20.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24800 FCOR161800 FH4600 FCOR30400 FHGROUP 32APOST 48437572125-01-06542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-04.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR117000 FH7400 FCOR48200 FHGROUP 32APRE 48437572125-01-07542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-05.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20700 FCOR124700 FH6600 FCOR39900 FHGROUP 33AORGROUP 33B572125-01-08542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER JOINTS BETWEEN RIB 26 AND RIB 28EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-02-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17800 FCOR107300 FH7100 FCOR42900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 107EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572125-02-04542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-06.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR117000 FH7400 FCOR48200 FHGROUP 32APRE 48437572125-02-05542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-07.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20700 FCOR124700 FH6600 FCOR39900 FHGROUP 33AORGROUP 33B572125-02-06542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER JOINTS BETWEEN RIB 26 ANDRIB 28 EXCLUDING JOINTS ON STRINGERS 15 AND 18.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572125-01-08.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17800 FCOR107300 FH7100 FCOR42900 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572129-01-03541SB 641SBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGER 13 JOINT BETWEEN RIB 22 AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-02-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18900 FCOR113800 FH4000 FCOR24500 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 108EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572129-02-03541SB 641SBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGER 13 JOINT BETWEEN RIB 22AND RIB 23.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572129-01-03.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18900 FCOR113800 FH4000 FCOR24500 FHGROUP 33APRE 44245ORGROUP 33BPRE 44245572133-01-04N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26500 FCOR172400 FH4900 FCOR32000 FHGROUP 32APRE 48437572133-01-05N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24900 FCOR149800 FH7300 FCOR43800 FHGROUP 33AORGROUP 33B572133-01-07N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPER SURFACE BETWEEN RIB 12 AND RIB 27 FROMFRONT SPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27900 FCOR167600 FH5200 FCOR31700 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572133-01-10N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONTSPAR TO REAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27900 FCOR167600 FH8900 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 109EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572133-01-11N/ADETAILED INSPECTION OF OUTER WING TOP SKINUPPERSURFACE BETWEEN RIB 12 AND RIB 27 FROM FRONTSPAR TOREAR SPAR.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26500 FCOR172400 FH8300 FCOR50000 FHGROUP 32APOST 48437572140-01-05541EB 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 STRINGERJOINTS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED29000 FCOR174000 FH11200 FCOR50000 FHGROUP 33AORGROUP 33B572153-01-04574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26000 FCOR169300 FH7800 FCOR50000 FHGROUP 32APRE 48437572153-01-05574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR108400 FH5900 FCOR35600 FHGROUP 33AORGROUP 33B572153-01-11574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACEJOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED30100 FCOR180900 FH6200 FCOR37500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572153-01-12574AT 674ATDETAILED INSPECTION OF OUTER WING REAR SPARAFT FACE SPAR JOINT PLATE AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24200 FCOR157800 FH5000 FCOR32700 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 110EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572154-01-04541FB 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14000 FCOR91300 FH9200 FCOR60400 FHGROUP 32APRE 48437572154-01-05541FB 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14100 FCOR84800 FH7100 FCOR42900 FHGROUP 33AORGROUP 33B572154-01-06541FB 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12200 FCOR73700 FH5700 FCOR34200 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 111EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572154-01-09541FB 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12200 FCOR79900 FH5700 FCOR37100 FHGROUP 32APOST 48437ORGROUP 32E572154-01-10541FB 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 30INCLUDING TOP AND BOTTOM FLANGES AND SPARJOINT BOLTING AT RIB 27.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13100 FCOR78600 FH8600 FCOR52000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572158-01-05541GB 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18000 FCOR117300 FH4400 FCOR29100 FHGROUP 32APRE 48437572158-01-06541GB 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17400 FCOR104900 FH5700 FCOR34600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 112EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572158-01-10541GB 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 RIB12 AND RIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR115800 FH4800 FCOR29200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572158-01-12541GB 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 RIB12 ANDRIB 23.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24300 FCOR158500 FH7400 FCOR48600 FHGROUP 32APOST 48437572164-01-05541GB 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27700 FCOR180400 FH4800 FCOR31500 FHGROUP 32APRE 48437572164-01-06541GB 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22100 FCOR132700 FH5600 FCOR34000 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 113EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572164-01-07541GB 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED26300 FCOR158200 FH4900 FCOR29800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572164-01-11541GB 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR167500 FH3700 FCOR24200 FHGROUP 32APOST 48437572164-01-12541GB 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 SPARAFT FACE BETWEEN RIB 12 AND RIB 27 INCLUDINGTOP AND BOTTOM FLANGES.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25700 FCOR154600 FH3700 FCOR22400 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572180-01-04541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13900 FCOR90400 FH10800 FCOR70800 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 114EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572180-01-05541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14200 FCOR85300 FH8100 FCOR49000 FHGROUP 33AORGROUP 33B572180-01-06541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14800 FCOR88800 FH11500 FCOR69500 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572180-01-07541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24100 FCOR144900 FH5500 FCOR33200 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572180-01-09541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20900 FCOR136000 FH4500 FCOR29700 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 115EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572180-01-10541GB 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.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20900 FCOR136000 FH4800 FCOR31200 FHGROUP 32APOST 48437572183-01-04542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14600 FCOR94900 FH5200 FCOR34000 FHGROUP 32APRE 48437572183-01-05542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR99300 FH4600 FCOR27600 FHGROUP 33AORGROUP 33B572183-01-06542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR88200 FH5100 FCOR30800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 116EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572183-01-07542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-7NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR116000 FH5400 FCOR32900 FHGROUP 33E572183-01-08542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-02-8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR113700 FH4900 FCOR32300 FHGROUP 32E572183-01-10542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-02-10NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR116000 FH5400 FCOR32900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572183-01-11542DB 542EB 642DB642EBDETAILED INSPECTION OF OUTER WING BOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-02-11NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR113700 FH4900 FCOR32300 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 117EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572183-02-04542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-4NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14600 FCOR94900 FH5200 FCOR34000 FHGROUP 32APRE 48437572183-02-05542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-5NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16500 FCOR99300 FH4600 FCOR27600 FHGROUP 33AORGROUP 33B572183-02-06542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-6NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14700 FCOR88200 FH5100 FCOR30800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437572183-02-07542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-7NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR116000 FH5400 FCOR32900 FHGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 118EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572183-02-08542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKIN STRINGERS 15 AND 18 BETWEEN RIBS26 AND 28 INCLUDING STRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 572183-01-8NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR113700 FH4900 FCOR32300 FHGROUP 32E572183-02-10542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-01-10NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19300 FCOR116000 FH5400 FCOR32900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437572183-02-11542DB 542EB 642DB642EBSEALANT REMOVAL ASPER NTMSPECIAL DETAILED INSPECTION OF OUTER WINGBOTTOM SKINSTRINGERS 15 AND 18 BETWEEN RIBS 26 AND 28INCLUDINGSTRINGER JOINTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME ASTASK 572183-01-11NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR113700 FH4900 FCOR32300 FHGROUP 32APOST 48437572606-01-02532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS3, 4 AND 5 AFT PICK-UP, ASSEMBLY.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22300 FCOR134100 FH13600 FCOR50000 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33DA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 119EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY572606-01-03532CB 533CB 534CB632CB 633CB 634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS3, 4 AND 5 AFT PICK-UP, ASSEMBLY.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20600 FCOR134100 FH12500 FCOR50000 FHGROUP 32AORGROUP 32E572607-01-01531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25400 FCOR152800 FH20000 FCOR50000 FHGROUP 33AORGROUP 33BORGROUP 33CORGROUP 33D572607-01-07531AB 531CB 532AB532CB 533AB 533CB534AB 534CB 631AB631CB 632AB 632CB633AB 633CB 634AB634CBDETAILED INSPECTION OF OUTER WING FLAP TRACKS2, 3, 4 AND 5 FORWARD PICK-UP LUGS FITTINGS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23500 FCOR152800 FH20000 FCOR50000 FHGROUP 32A573001-01-05535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR106500 FH4000 FCOR26000 FHGROUP 32APRE 48437573001-01-07535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105000 FH3900 FCOR23600 FHGROUP 33APOST 41460ORGROUP 33BPOST 41460573001-01-08535AZ 535BZ 635AZ635BZDETAILED INSPECTION OF WINGTIP TO MAIN WINGBOXJOINT AT RIB 39 INCLUDING TOP AND BOTTOM SKINS,FRONT AND REAR SPARS AND ALL FITTINGS ANDBUTTSTRAPS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17600 FCOR105700 FH4300 FCOR25800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 120EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY573002-01-05N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR106500 FH4000 FCOR26000 FHGROUP 32APRE 48437573002-01-07N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105000 FH3900 FCOR23600 FHGROUP 33APOST 41460ORGROUP 33BPOST 41460573002-01-08N/ADETAILED INSPECTION OF WINGTIP BOX TOP SKINUPPER SURFACE AND BOTTOM SKIN LOWERSURFACE.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17600 FCOR105700 FH4300 FCOR25800 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437573003-02-04WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19900 FCOR129400 FH4000 FCOR26500 FHGROUP 32APRE 48437573003-02-05WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20400 FCOR122400 FH3900 FCOR23800 FHGROUP 33AORGROUP 33B573003-02-10WINGLETSPECIAL DETAILED INSPECTION OF WINGTIP TOWINGLET FORWARD ANDAFT LUGS (BOTH ONWINGTIP AND WINGLET).NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21400 FCOR128500 FH4300 FCOR26300 FHGROUP 33CPRE 48438ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 121EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-04521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16300 FCOR106000 FH16300 FCOR106000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 122EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-05521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR95100 FH15800 FCOR95100 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 123EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-06521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17500 FCOR105300 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 124EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-07521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22000 FCOR143500 FH17000 FCOR50000 FHGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 125EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-11521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22000 FCOR143500 FH20000 FCOR50000 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 126EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574106-01-12521BB 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 FIXEDLEADING EDGE BOTTOM SUB-SPAR JOINT STRAPS ONTRACK RIB 1 TO TRACK RIB 16.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23100 FCOR139000 FH20000 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437574107-02-04521FB 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED24000 FCOR156000 FH10900 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 127EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574107-02-05521FB 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27800 FCOR166900 FH12200 FCOR50000 FHGROUP 33AORGROUP 33B574107-02-06521FB 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 WINGFIXED LEADING EDGE TOP SPREADER PLATE ANDSUB-SPAR JOINT STRAPS AT TRACK RIB 3 TO TRACKRIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED27300 FCOR164000 FH12400 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 128EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574109-02-01521AB 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9100 FCOR59700 FH4400 FCOR28600 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 129EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574109-02-02521AB 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8900 FCOR53600 FH4200 FCOR25600 FHGROUP 33AORGROUP 33BA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 130EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574109-02-03521AB 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13000 FCOR78400 FH6200 FCOR37500 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 131EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574109-02-05521AB 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12400 FCOR80900 FH5900 FCOR38700 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 132EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574109-02-07521AB 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 622AB622BB 622CB 622DB622EB 622FB 622GB622HB 622JB 622KB622LB 622MB 622NB622PB 622QB 622RB622SB 623CB 623DB623EB 623FB 623GB623HB 623JB 623KB623LB 623MB 623NB623PBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM JOINT SPREADER PLATESAND SUB-SPAR JOINT STRAPS ON ALL INTERMEDIATERIBS (INCLUDING CLOSING RIBS AND TELESCOPERIBS) AND SLAT HOLD DOWN RIBS.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9800 FCOR59300 FH4700 FCOR28400 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437574110-02-01N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22400 FCOR146100 FH13900 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 133EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574110-02-02N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23500 FCOR141000 FH5300 FCOR31800 FHGROUP 33AORGROUP 33B574110-02-03N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 1 TORIB 9.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22500 FCOR135100 FH13300 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437574114-03-01N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21500 FCOR139700 FH9700 FCOR50000 FHGROUP 32APRE 48437574114-03-02N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED22400 FCOR134800 FH3700 FCOR22200 FHGROUP 33AORGROUP 33B574114-03-03N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR122300 FH8900 FCOR50000 FHGROUP 33CPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 134EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574114-03-04N/ADETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG LOWERSURFACE FORWARD OF FRONT SPAR FROM RIB 11 TORIB 39.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED20300 FCOR122300 FH8800 FCOR50000 FHGROUP 33DPRE 48437574115-02-01522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11500 FCOR74900 FH5000 FCOR32700 FHGROUP 32APRE 48437574115-02-02522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED12900 FCOR77400 FH2000 FCOR12000 FHGROUP 33AORGROUP 33B574115-02-03522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10700 FCOR64700 FH4700 FCOR28300 FHGROUP 33CPRE 48437574115-02-05522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10700 FCOR64700 FH4600 FCOR28100 FHGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 135EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY574115-02-07522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21100 FCOR127100 FH10200 FCOR50000 FHGROUP 33EORGROUP 33CPOST 48437ORGROUP 33DPOST 48437574115-02-09522AB 522BB 522CB622AB 622BB 622CBDETAILED INSPECTION OF OUTER WING FIXEDLEADING EDGE BOTTOM SKIN OVERHANG UPPERSURFACE FORWARD OF FRONT SPAR BETWEEN RIBS9 AND 11.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED23300 FCOR151700 FH11200 FCOR50000 FHGROUP 32APOST 48437574804-01-03SLAT FULLY EXTENDEDSPECIAL DETAILED INSPECTION OF SLAT 6, SKINCONNECTIONS ATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10300 FCOR61900 FH3000 FCOR18000 FHA330-300574804-02-04SLAT FULLY EXTENDEDDETAILED INSPECTION OF SLAT 6, SKIN CONNECTIONSATTRACK RIB AND HOLD DOWN RIB STATIONS,EXTERNAL,LH/RH.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10300 FCOR61900 FH3000 FCOR18000 FHA330-300575011-01-04N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED30300 FCOR197000 FH18600 FCOR50000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 136EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575011-01-05N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16100 FCOR96800 FH9800 FCOR59100 FHGROUP 33APRE 42391ORGROUP 33BPRE 42391575011-01-06N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33600 FCOR202000 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575011-01-07N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED33600 FCOR202000 FH8300 FCOR49900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575011-01-10N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED30300 FCOR197000 FH7400 FCOR48400 FHGROUP 32APOST 48437575011-01-13N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE TOP SKIN UPPER SURFACE AFT OF REAR SPARBETWEEN RIB 1 AND RIB 14.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED32100 FCOR192800 FH9800 FCOR50000 FHGROUP 33APOST 42391ORGROUP 33BPOST 42391575012-01-02N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15400 FCOR100200 FH3900 FCOR25800 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 137EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575012-01-03N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19000 FCOR114200 FH4000 FCOR24500 FHGROUP 33AORGROUP 33B575012-01-06N/ADETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR BETWEEN RIB 1 AND RIB 9 EXCLUDING AREACOVERED BY FLAP TRACK 2 FAIRING AND CURVEDSKIN EDGE AFT OF REAR SPAR JUST INBOARD OFGEAR SUPPORT RIB 6.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED16000 FCOR96300 FH4200 FCOR25200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575014-01-06573DB 673DBSPECIAL DETAILED INSPECTION OF OUTER WINGTRAILINGEDGE BOTTOM SKIN AFT OF REAR SPAR COVERED BYMLG REINFORCING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED28600 FCOR172000 FH13200 FCOR79600 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575016-01-05531AB 631ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR UNDER FLAP TRACK 2 FAIRING.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25800 FCOR155300 FH6600 FCOR40000 FHGROUP 33AORGROUP 33B575018-01-03147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED15800 FCOR103000 FH15800 FCOR103000 FHGROUP 32APRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 138EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575018-01-04147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18300 FCOR110300 FH8800 FCOR50000 FHGROUP 33AORGROUP 33B575018-01-05147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17000 FCOR102300 FH20000 FCOR50000 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437575018-01-06147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17900 FCOR107800 FH17900 FCOR50000 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437575018-01-07147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17900 FCOR107800 FH17000 FCOR50000 FHGROUP 33E575018-01-08147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17100 FCOR111200 FH17000 FCOR50000 FHGROUP 32E575018-01-09147AT 148AT 191CT192CTDEPLOY FLAPSDETAILED INSPECTION OF OUTER WING TRAILINGEDGE ATTACHMENT OF SHROUD BOX.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED17100 FCOR111200 FH17200 FCOR50000 FHGROUP 32APOST 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 139EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575022-01-01575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9700 FCOR63400 FH7200 FCOR46900 FHGROUP 32APRE 48437575022-01-02575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED9200 FCOR55700 FH9200 FCOR55700 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E575022-01-04575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED8800 FCOR57500 FH8800 FCOR57500 FHGROUP 32APOST 48437ORGROUP 32EA330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 140EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575022-01-05575AB 575BB 675AB675BBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE INBOARD AILERON HINGES, 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOSTAND ATTACHMENT OFHINGEPOST TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, INTERNAL AND EXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10200 FCOR61400 FH7500 FCOR45400 FHGROUP 33AORGROUP 33BORGROUP 33CPRE 48437ORGROUP 33DPRE 48437575023-01-07575CB 575DB 675CB675DBDETAILED INSPECTION OF OUTER WING TRAILINGEDGE OUTBOARD AILERON, HINGES 1-3 AT LUG ANDATTACHMENT TO REAR SPAR AND TOP AND BOTTOMSKIN OVERHANGS, HINGES 4 AND 5 AT LUG ANDATTACHMENT TO HINGEPOST TO REAR SPAR AND TOPAND BOTTOM SKIN OVERHANGS, INTERNAL ANDEXTERNAL.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25900 FCOR168500 FH7200 FCOR47300 FHGROUP 32APOST 48437575025-01-04532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED19700 FCOR69000 FH6300 FCOR40900 FHGROUP 32APRE 48437575025-01-05532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED11600 FCOR69700 FH7300 FCOR43900 FHGROUP 33AORGROUP 33B575025-01-06532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13200 FCOR79400 FH6500 FCOR39200 FHGROUP 33CPRE 48437ORGROUP 33DPRE 48437A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 141EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY575025-01-07532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10700 FCOR64500 FH5300 FCOR31900 FHGROUP 33CPOST 48437ORGROUP 33DPOST 48437ORGROUP 33E575025-01-08532AB 632ABDETAILED INSPECTION OF OUTER WING TRAILINGEDGE BOTTOM SKIN LOWER SURFACE AFT OF REARSPAR FROM RIB 8 TO RIB 12.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED14300 FCOR50000 FH4600 FCOR30300 FHGROUP 32APOST 48437ORGROUP 32E575067-01-02FWD FLAP TRACKFAIRINGSDETAILED INSPECTION OF FLAP TRACK BEAMS NO2,3,4 AND 5, FORWARD ATTACHMENT SPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575067-02-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18200 FCOR109200 FH6400 FCOR38400 FHA330-200ORA330-300575067-02-02FWD FLAP TRACKFAIRINGSFAIL SAFE BOLTSPECIAL DETAILED INSPECTION OF FLAP TRACKBEAMS NO 2,3,4 AND 5, FORWARD ATTACHMENTSPIGOTS.NOTE: THIS TASK MUST BE PERFORMED AT THE SAMETIME AS TASK 575067-01-02.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED18200 FCOR109200 FH6400 FCOR38400 FHA330-200ORA330-300576105-01-01FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,LOWER FLANGE RADIUS AT LUG SIDE OF HINGE 1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED10700 FCOR70400 FH10700 FCOR70400 FHA330-200POST 53074ORA330-300POST 53074A330 AIRWORTHINESS LIMITATIONS SECTIONISSUE: 23 MAR 2012ALI SECTION 2.2PAGE: 142EASA APPROVED©AIRBUS SAS 2012. All rights reserved.REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLD INTERVAL APPLICABILITY576108-01-01FAIRINGPANELSPECIAL DETAILED INSPECTION OF OUTER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED25000 FCOR163400 FH21000 FCOR137900 FHA330-200POST 53074ORA330-300POST 53074576115-01-01FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,LOWER FLANGERADIUS AT LUG SIDE OF HINGE1.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED21900 FCOR143000 FH21900 FCOR143000 FHA330-200POST 53074ORA330-300POST 53074576118-01-01FAIRINGPANELSPECIAL DETAILED INSPECTION OF INNER AILERONS,UPPER FLANGE RADIUS AT LUG SIDE OF HINGE 3.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED13900 FCOR94500 FH13900 FCOR94500 FHA330-200POST 53074ORA330-300POST 53074712105-01-01ENGINEFWD ENGINE MOUNTDISASSEMBLEDSPECIAL DETAILED INSPECTION OF FORWARD ENGINEMOUNT THRUST TRUNNION.NOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7100 FCOR47900 FH7100 FCOR47900 FHRRA330-200ORRRA330-300712205-01-01417AL 418AR 427AL428ARENGINESPECIAL DETAILED INSPECTION OF AFT ENGINEMOUNT LINKSNOTE: THE THRESHOLDS/INTERVALS OF THISMAINTENANCE REQUIREMENT ARE FH OPTIMIZED7100 FCOR47900 FH7100 FCOR47900 FHA330-200RRORA330-300RR

# A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA - 1

© AIRBUS SAS 2012. All rights reserved. 

# 1 SUMMARY OF CHANGES

Section 1 INTRODUCTION

The WV 062 has been added in the applicability table for A330/200 aircraft.

The WV 055 has been added in the applicability table for A330/300 aircraft.

Section 2 AIRWORTHINESS LIMITATIONS:

REV

CODE TASK

REFERENCE SUMMARY OF CHANGES SECTION 2-1

STANDARD

(SR) SECTION 2-2

ALTERNATIVE

(LR)

R 531144-01-03 Task number updated x

R 531186-01-02 Applicability updated x

R 532152-01-01 Task number updated x

R 533010-01-02 Applicability updated x x

R 533151-01-01 Access updated x x

R 533151-01-02 Access updated x x

R 533151-01-03 Access updated x x

R 533152-01-06 Task number updated x

R 533180-01-05 Interval updated x

R 533181-01-06 Applicability updated x x

R 533181-01-07 Applicability updated x x

R 533195-02-04 Threshold updated x

R 533197-01-01 Note updated in task description x

R 533197-02-01 Note updated in task description x

R 534108-01-02 Task number updated x x

R 534110-01-02 Task number updated x x

R 545129-01-09 Applicability updated x x

R 545174-02-09 Threshold udpated x

R 545180-04-07 Threshold udpated x

R 571102-01-01 Applicability updated x

R 571102-01-02 Applicability updated x

R 571102-01-07 Applicability updated x

R 571104-01-04 Applicability updated x

R 571130-01-04 Applicability updated x x

R 571153-01-05 Applicability updated x x

R 571163-01-01 Applicability updated x x

R 571163-01-02 Applicability updated x x

D 572022-01-04 Task kept for historical reference x

D 572022-01-05 Task kept for historical reference x

D 572022-01-06 Task kept for historical reference x

D 572022-01-07 Task kept for historical reference x

R 572067-03-05 Applicability updated x x

# A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA - 2

© AIRBUS SAS 2012. All rights reserved. REV

CODE TASK

REFERENCE SUMMARY OF CHANGES SECTION 2-1

STANDARD

(SR) SECTION 2-2

ALTERNATIVE

(LR)

R 572068-01-13 Interval updated x

R 572069-01-04 Interval updated x

R 572069-01-08 Interval updated x

D 572166-01-05 Task kept for historical reference x

R 712205-01-01 Threshold/Interval updated x

R 712205-01-02 Threshold/Interval updated x



# APPENDIX A SUMMARY OF CHANGES

Correction of ALI Rev 18 Summary of Changes further to identified anomalies:

REV

CODE TASK

REFERENCE SUMMARY OF CHANGES SECTION 2-1

STANDARD

(SR) SECTION 2-2

ALTERNATIVE

(LR)

R 523104-01-02 Interval updated x

R 523204-01-02 Interval updated x

R 531142-02-02 Interval updated x

R 532148-01-02 Threshold and interval updated x

R 532166-02-03 Note updated in the description x

R 533014-01-02 Threshold/Interval updated

Note added in the description

Applicability updated x x

R 533115-01-06 Threshold/Interval updated

Note added in the description x x

R 533115-01-07 Threshold/Interval updated

Note added in the description x x

R 533126-01-03 Threshold/Interval updated

Description updated

Note added in the description x x

R 533126-01-05 Threshold/Interval updated

Description updated

Note added in the description x x

R 533126-01-06 Threshold/Interval updated

Description updated

Note added in the description x x

R 534132-02-01 Applicability updated x

R 545138-02-03 Threshold updated

Note added in the description

Applicability updated x x

N 571164-01-02 New task x x

R 572047-01-04 Threshold updated

Note added in the description x x

R 572052-03-08 Threshold updated

Interval updated

Note added in the description

Applicability updated x x

# A330 Airworthiness Limitation Items

APPENDIX A – SUMMARY OF CHANGES

ISSUE: 23 MAR 2012 PAGE: APXA - 3

© AIRBUS SAS 2012. All rights reserved. REV

CODE TASK

REFERENCE SUMMARY OF CHANGES SECTION 2-1

STANDARD

(SR) SECTION 2-2

ALTERNATIVE

(LR)

R 572069-01-04 Threshold updated

Note added in the description x x

R 572069-01-08 Threshold updated

Note added in the description

Applicability updated x x

R 572164-01-12 Threshold/Interval updated

Note added in the description

Applicability updated x x

R 574106-01-06 Threshold updated

Note added in the description

Applicability updated x x

R 574106-01-11 Threshold updated

Note added in the description x x

R 574106-01-12 Threshold updated

Note added in the description x x

R 575018-01-05 Threshold updated

Note added in the description

Applicability updated x x

R 575018-01-06 Threshold updated

Note added in the description x x

R 575018-01-07 Threshold updated

Note added in the description x x

R 575018-01-08 Threshold updated

Note added in the description x x

R 575401-02-01 Applicability updated x

R 712105-01-01 Threshold/Interval updated

Note added in the description

Applicability updated x x

# A330 Airworthiness Limitation Items

APPENDIX B – ABBREVIATIONS

ISSUE: 23 MAR 2012 PAGE: APXB - 1

© AIRBUS SAS 2012. All rights reserved. ABBREVIATION MEANING

AD Airworthiness Directive

ALI Airworthiness Limitation Item

ALS Airworthiness Limitations Section

AMM Aircraft Maintenance Manual

ATA Air Transport Association

CPCP Corrosion Prevention and Control Program

D Deleted

EASA European Aviation Safety Agency

FAA Federal Aviation Agency

FC Flight Cycle

FH Flight Hour

FR Frame

HFEC High Frequency Eddy Current (NDT inspection method)

HTP Horizontal Tail Plane

JAR Joint Aviation Requirements

LOV Limit Of Validity

MOD Modification

MPD Maintenance Planning Document

MRBR Maintenance Review Board Report

MSN Manufacturer Serial Number

N New

N/A Not Applicable

NDT Non Destructive Test

NTM Non Destructive Test Manual

R Revised

RAS Repair Design Approval Sheet

ROR Record Of Revisions

SB Service Bulletins

SRM Structural Repair Manual

SSI Structural Significant Item

STC Supplemental Type Certificate

STR Stringer

THS Trimmable Horizontal Stabilizer

TPS Temporary Protection System

TOC Table Of Contents

US UltraSonic (NDT inspection method)

WV Weight Variant

# A330 Airworthiness Limitation Items

APPENDIX C – TERMS AND DEFINITIONS

ISSUE: 23 MAR 2012 PAGE: APXC - 1

© AIRBUS SAS 2012. All rights reserved. TERM DEFINITION

AIRCRAFT

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

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

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

doors, etc. are treated as systems components. Attachment of the actuators to

the airframe are treated as structure.

CALENDAR TIME

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

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

freeze calendar time accumulation.

CONTINUED

AIRWORTHINESS Is the process of ensuring that the level of airworthiness guaranteed by TC is

maintained for each individual aircraft at the time of its entry into service and

during all its service life.

DAMAGE

TOLERANCE

CONCEPT The damage-tolerance evaluation of structure is intended to ensure that should

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

of the aeroplane, the remaining structure can withstand reasonable loads without

failure or excessive structural deformation until the damage is detected.

Damage-tolerance design is required, unless it entails such complications that an

effective damage-tolerant structure cannot be achieved within the limitations of

geometry, inspectability, or good design practice. Under these circumstances, a

design that complies with the fatigue evaluation (safe life) requirements is used.

DAMAGETOLERANT

AIRWORTHINESS

LIMITATION ITEMS

(DT ALI) They are all those parts of the structure whose failure could result in catastrophic

failure of the airplane and that are designed to fatigue and damage-tolerance

concept.

DESIGN SERVICE

GOAL Is a reference figure selected for the design and certification of the aircraft.

EXTENDED

SERVICE GOAL Is an extension of the DSG.

FLIGHT CYCLE (FC) A complete take-off and landing sequence

FLIGHT HOUR (FH) The accumulated time intervals between ‘wheels-off’ and ‘wheels-on’.

INTERVAL The maximum period expressed in usage parameters between the completion of

a task and its next due accomplishment.

LIMIT OF VALIDITY

(LOV) Is a limitation to the validity of the Airworthiness Limitation Sections

THRESHOLD The maximum period of time expressed in usage parameters between the first

flight of the aircraft, and the frist due completion of the task.

Subsequent accomplishment deadlines are obtained by adding the repeat

interval and its multiples to the threshold.

TOUCH AND GO A ‘Touch and go’ is a landing in which an aircraft touches the runway and does

not come to a full stop prior to commencing an additional flight.

# A330 Airworthiness Limitation Items

ISSUE: 23 MAR 2012

© AIRBUS SAS 2012. All rights reserved. 

# INTENTIONALLY LEFT BLANK