# AIRBUS

Customer Services

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document.

This document and all information contained herein is t he sole property of AIRBUS SAS. No intellectual property

rights are granted by the delivery of th is document or the disclos ure 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 t he 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 

# A300-600

Airworthiness Limitation Items

Document

Airbus

Customer Services

1, Rond Point Maurice Bellonte

31707 Blagnac Cedex AI/SE-M2/95A.1310/07

FRANCE February 2011

Temporary Revision 13.1

### CUSTOMER SERVICES



### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: 1-TOC

EASA APPROVED

Ref: 95A.1310/07

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### TABLE OF CONTENTS

TABLE OF CONTENTS

.............................................................................................................................. . 1 

### -TOC

RECORD OF REVISIONS

............................................................................................................................ 1-ROR

1.1 Introduction

.............................................................................................................................. ................... TR13.1- 1

1.2 Revised ALI Requirements:

....................................................................................................................... TR13.1- 1

1.2.1 ALIs valid without changes

......................................................................................................... TR13.1- 1

1.2.2 New ALIs

.............................................................................................................................. ....... TR13.1- 1

1.2.3 Revised ALIs

............................................................................................................................... TR13.1- 2

1.3 Compliance Time

............................................................................................................................... .......... TR13.1- 2

ALI REQUIREMENTS TABLES:

.................................................................................................................. TR13.1- 3

NEW DT ALI ILLUSTRATIONS

................................................................................................................... TR13.1- 4

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: 1-ROR

EASA APPROVED

Ref: 95A.1310/07

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### RECORD OF REVISIONS

Issue Date Reason for Revision Approved by EASA

1 Sept 98 Section 2 of CMR documents originally

identified 'Structural Inspections'. These are

not CMRs. New document created.

Reference to A300-600 MRB Document

dated Feb 1992 changed to A300-600 MRB

Report dated April 1998.

Reference to "FLP-1 limits" replaced by

"100% limits".

Reference to "FLP 1 concept" replaced by

'concept S'.

2 June 99 A300C4-605R Variant F added to Section 0

para 2.

Reference to Variant F MRB Report

complement document added in Section 1

3 July 99 To reflect reduced inspection threshold

and/or interval values for specified SSIs on

PW4000 powered aircraft following reappraisal of powerplant weight used in

original calculations. Table 1 added.

To highlight the need to reduce, in defined

circumstances, certain FC figures using the

'‘Adjustment for Range’ formulae

4 June 00 Section 0, para 1, the ref. to AMM 05 has

been replaced by the ref. to MPD section 9.1.

Section 0, para 2, the A300F4-622R model

has been added.

Section 1, paragraph 1, the ref. to the MRB

approved complement for A300C4-605R

Variant F has been deleted (complement

introduced in MRB Report, March 2000).

Section 1, paragraph 3 has been deleted

(introduced in the MRBR, March 2000).

The table 1 has been revised to reflect all

ALIs that are not included in the MRB Report,

March 2000.

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: 2-ROR

EASA APPROVED

Ref: 95A.1310/07

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### Issue Date Reason for Revision Approved by EASA

5 Aug 00 Section 1, paragraphs 1 and 5, ref. to the

table 2 has been added.

Table 2 has been created to identify specific

ALIs which must be performed to permit

operation between the Design Service Goal

and the intermediate Extended Service Goal.

These ALIs are only applicable to the 16

affected A300-600 aircraft.

6 Jan 01 Section 1, table 2 has been updated to

introduce the item number 53.12.39.

7 Sept 02 “Airbus Industrie” logo replaced by “Airbus”

logo on all pages.

Page Issue / Date not modified by this

change.

Section 1 has been updated to introduce the

MSN 358.

8 Dec 02 Format of document completely revised

ESG requirements added

9 Feb 04 Section A: Limit of Validity definition added

Section B: CPCP level 1 definition added

Section D and E:

ALI 531208 and 545002 introduced

Several ALI revised (see SOC)

Section G: illustrations added

10 June 04 Introduction of new and revised requirements

due to General Freighter for CPA.

11 Feb 06 Application tolerance on first interval for new

and revised requirement paragraph revised

Corrosion level 2 & 3 reporting added.

Contact amended

Introduction of New and revised

requirement/Illustrations

Numbering and notes changed EASA.A.C.03920

Approved 31-May-06



### 12 June 08 ALI Document layout has been reworked

New / updated ALI requirements due to

modifications/In-service experience 

### EASA.A.C.10908

Approved 09-Dec-08

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: 3-ROR

EASA APPROVED

Ref: 95A.1310/07

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### Issue Date Reason for Revision Approved by EASA

13 Oct 10 Revision due to Extended Service Goal 2,

plus consideration of the result of the fleet

survey

Adjustment for Range section deleted

New / updated DT ALI requirements due to

modifications/In-service experience

Section C deleted. Paragraph in Section A

related to modification requirements deleted. 

### EASA 10035072

Approved 24-May-11



### TR13.1 Feb 11 Revision due to completion of the work

performed on the list of reserves given in

page 4-ROR of the A300-600 ALI Document

Issue 13 Oct 10. 

### EASA 10035073

Approved 24-May-11

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: TR13.1- 1

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### 1.1 INTRODUCTION

This Temporary Revision (T.R.) 13.1 contains new and revised requirement to A300-600

Airworthiness Limitation Items document Issue 13 dated on October 2010 and approved by

EASA with Reference 10035073 dated on the 24 May 2011 in order to complete the ESG2

exercise review.

The applicability and limit of validity, program ru les, program notes and definitions remain valid

as stated in the A300-600 ALI Document Issue 13.

The validity of this Temporary Revision (T.R.) will expire at the approval date of the A300-600

Airworthiness Limitation Item Document Issue 14.

IMPORTANT: The requirements given in this document are mandatory. Non-compliance

suspends the validity of the Airworthiness Certificate.

This document does not take into account Airw orthiness Directives (AD) or Consignes de

Navigabilité (CN) which, if issued against a fatigue related structural inspection, supersede the

specific requirement given in this document.

1.2 REVISED ALI REQUIREMENTS:

The maintenance requirements contained in the A300-600 ALI Issue 13 have been reviewed

and classified as follows:

- ALIs valid without changes;

- New ALIs

- Revised ALIs

1.2.1 ALIs valid without changes

All ALIs not mentioned in this document remain valid as defined in the A300-600 ALI Issue 13

dated on October 2010 and approved by EASA with Reference 10035072 dated 24 May 2011

.

1.2.2 New ALIs

The following ALI Tasks have been introduced through this T.R. They have to be added in the

Maintenance Program as ALIs requirement.

Section D:

572108-01-3A 572124-01-2A 572125-01-3A

572131-01-2A 572149-01-3A 572163-01-2A

572503-01-2A 572503-01-3A 572504-01-2A

572504-01-3A 572507-01-2A 572507-01-3A

572508-01-2A 572508-01-3A 572521-01-2A

572525-01-2A 574106-01-2A 574111-01-3A

574129-01-2A 575135-01-2A

Section E:

572108-01-3A-S 572124-01-2A-S 572525-01-2A-S

572131-01-2A-S 572149-01-3A-SS 572163-01-2A-S

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: TR13.1- 2

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### 572503-01-2A-S 572503-01-3A-S 572504-01-2A-S

572504-01-3A-S 572507-01-2A-S 572507-01-3A-S

572508-01-2A-S 572508-01-3A-S 572521-01-2A-S

572525-01-2A-S 574106-01-2A-S 574111-01-3A-S

574129-01-2A-S

1.2.3 Revised ALIs

The following ALI Tasks have been revised. They replace the corresponding requirements of

A300-600 ALI Issue 13.

Section D:

572525-01-1A

572164-01-3A

Section E:

572525-01-1A-S

572164-01-3A-S

1.3 COMPLIANCE TIME

For aircraft that have already exceeded or are close to exceeding the new or revised

airworthiness limitations in ALI Issue TR13.1, the next due accomplishment of each such task

may be deferred by up to 2000 FC or 50% of the new interval, whichever is the lesser, without

exceeding the limitations and special compliance times quoted in ALI Issue 13.

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: TR13.1- 3

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### ALI REQUIREMENTS TABLES:

In the following pages are listed new/revised requirements by section (D and E).RevCodeTask Reference Zone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteN 572108-01-3A 543/643 543/643 AB to DB Detailed inspection of outer wing front spar AFT face from rib 9to rib 14Th. 49500 FC89000 FHInt. 3500 FC7500 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FHto LOVSN 572124-01-2A 543/643 543/643 AB to DB Detailed inspection of outer wing rear spar fwd face between rib9 and rib 14.Th. 47200 FC89000 FHInt. 7900 FC17000 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FHto LOVSN 572125-01-3A 541/641542/642541/641CB542/642 DBSpecial detailed inspection (Ultrasonic) of outer wing centerspar, pylon fitting, fwd and aft faces.Th. 45200 FC89000 FHInt. 4400 FC9500 FHNTM 572125 B4-600B4-600RFrom 0 FC/FHto LOVSN 572131-01-2A 541/641542/642542/642 EB Detailed inspection of outer wing center spar upper and lowerbooms between rib 8 and rib 9.Th. 49500 FC89000 FHInt. 7200 FC15500 FHB4-600B4-600RFrom 0 FC/FHto LOVSN 572149-01-3A 500/600 N/A Detailed inspection of outer wing top skin upper surface atattachments to ribs and stringers from ribs 1 to 14 and fromTh. 39700 FC85700 FHB4-600/B4-600RFrom 0 FC/FHto LOVSA300-600Airworthiness Limitations Itemsgfront spar to rear spar. Int. 6400 FC13800 FHN 572163-01-2A 541/641542/642543/643541/641 AB,BB, CB542/642 CB, DB543/643 AB, BB,CB, DBDetailed inspection of outer wing bottom skin stringers from rib 1to rib 14.Th. 39300 FC84800 FHInt. 19600 FC42400 FHB4-600B4-600RFrom 0 FC/FHto LOVSR 572164-01-3A 543/643550/650543/643 DB550/650 BBSpecial detailed inspection (HFEC) of outer wing bottom skinstringers adjacent to rib 14.Th. 23100FC49900FHInt. 4400FC9500FHNTM 572164 B4-600/B4-600RPRE 10324PRE 10325PRE 10326(57-6046)From 0 FC/FHto LOVSN 572503-01-2A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib 14 torib 27, excluding areas adjacent to stringer termination plates.Th. 39300 FC84800 FHInt. 4300 FC9200 FHB4-600/B4-600RPRE 4741PRE 10470(57-6048)From 0 FC/FHto LOVSIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section D© AIRBUS SAS 2011. All rights reserved.Confidential and proprietary document.Page : 3 - DRevCodeTask Reference Zone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteA300-600Airworthiness Limitations ItemsN 572503-01-3A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib 14 torib 27, excluding areas adjacent to stringer termination plates.Th. 43200 FC89000 FHInt. 15200 FC32800 FHB4-600/B4-600RPOST 4741PRE 10324PRE 10325PRE 10470(57-6048)From 0 FC/FHto LOVSN 572504-01-2A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib 14 torib 27.Th. 39300 FC84800 FHInt. 4300 FC9200 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FHto LOVSN 572504-01-3A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib 14 torib 27.Th. 43200 FC89000 FHInt. 15200 FC32800 FHB4-600/B4-600RPOST 10324ORB4-600/B4-600RPOST 10325ORFrom 0 FC/FHto LOVSB4-600/B4-600RPOST 4741POST 10470(57-6048)N 572507-01-2A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib 14to rib 27, excluding area adjacent to stringer termination platefrom rib 21 to rib 22.Th. 36100 FC77900 FHInt. 7900 FC17000 FHB4-600/B4-600RPRE 4741PRE 10470(SB 57-6048)From 0 FC/FHto LOVSN 572507-01-3A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib 14to rib 27, excluding area adjacent to stringer termination platefrom rib 21 to rib 22.Th. 39800 FC85900 FHInt. 19900 FC42900 FHB4-600/B4-600RPOST 4741PRE 10324PRE 10325PRE 10470(SB 57-6048)From 0 FC/FHto LOVSN 572508-01-2A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib 14to rib 27.Th. 36100 FC77900 FHInt. 7900 FC17000 FHB4-600/B4-600RPRE 4741POST 10470(SB 57-6048)From 0 FC/FHto LOVSIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section D© AIRBUS SAS 2011. All rights reserved.Confidential and proprietary document.Page : 4 - DRevCodeTask Reference Zone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteA300-600Airworthiness Limitations ItemsN 572508-01-3A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib 14to rib 27.Th. 39800 FC85900 FHInt. 19900 FC42900 FHB4-600/B4-600RPOST 10324ORB4-600/B4-600RPOST 10325ORB4-600/B4-600RPOST 4741POST 10470(SB 57-6048)From 0 FC/FHto LOVSN 572521-01-2A 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing bottom skin stringers from rib14 to rib 27.Th. 39300 FC84800 FHInt. 6200 FC13300 FHB4-600B4-600RFrom 0 FC/FHto LOVSR 572525-01-1A 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skinaccess doors and door surrounds from rib 22 to rib 27.Th. 18000 FC38900 FHInt. 12200 FCNTM 572525 ALLF4-600R/C4-605R.F/From 0 FC/FHto LOVSNote : TPS not to be applied to upper surface of wing skin. 26300 FH C4-600N 572525-01-2A 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skinaccess doors and door surrounds from rib 22 to rib 27.Note : TPS not to be applied to upper surface of wing skin.Th. 18000 FC38900 FHInt. 9600 FC20700 FHNTM 572525 B4-600B4-600RFrom 0 FC/FHto LOVSN 574106-01-2A 512/612523/623524/624Slat extended Detailed inspection of outer wing leading edge "D" nose skinjoint plate (including reinforcing plate and landing reinforcingplate) at slat track cutouts.Th. 42500 FC89000FHInt. 3300 FC7100 FHB4-600B4-600RFrom 0 FC/FHto LOVSN 574111-01-3A 512/612523/623512/612 KB, LB523/623 AB, BBDetailed inspection of outer wing fixed leading edge ribs inboardand outboard of pylon.Th. 42500 FC89000FHInt. 5000 FC10800 FHB4-600B4-600RFrom 0 FC/FHto LOVSN 574129-01-2A 500/600 N/A Detailed inspection of outer wing bottom skin lower surface fwdof front spar from root to tip.Th. 47800 FC89000FHInt. 23000 FC49600 FHB4-600B4-600RFrom 0 FC/FHto LOVSN 575135-01-2A 500/600575/675575/675 AT, BT Detailed inspection of outer wing top skin upper surface andreinforcing at access door cutouts inboard of from rib 6A aft ofrear spar.Th. 42500 FC89000FHInt. 10400 FC23400 FHB4-600B4-600RFrom 0 FC/FHto LOVIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section D© AIRBUS SAS 2011. All rights reserved.Confidential and proprietary document.Page : 5 - DRevCodeTaskReferenceZone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteN 572108-01-3A-S 543/643 543/643 AB to DB Detailed inspection ofouter wing front spar AFT face from rib9 to rib 14Th. 51000 FC80100 FHInt. 3700 FC5600 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FHto LOVN 572124-01-2A-S 543/643 543/643 AB to DB Detailed inspection of outer wing rear spar fwd face betweenrib 9 and rib 14.Th. 51000 FC76400 FHInt. 8500 FC12700 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FH toLOVN 572125-01-3A-S 541/641542/642541/641CB542/642 DBSpecial detailed inspection (Ultrasonic) of outer wing centerspar, pylon fitting, fwd and aft faces.Th. 48800 FC73200 FHInt. 4800 FC7100 FHNTM 572125 B4-600B4-600RFrom 0 FC/FH toLOVN 572131-01-2A-S 541/641542/642542/642 EB Detailed inspection of outer wing center spar upper and lowerbooms between rib 8 and rib 9.Th. 51000 FC80100 FHInt. 7800 FC11600 FHB4-600B4-600RFrom 0 FC/FH toLOVN 572149-01-3A-S 500/600 N/A Detailed inspection of outer wing top skin upper surface atattachments to ribs and stringers from ribs 1 and 14 and fromTh. 42800 FC64300 FHB4-600B4-600RFrom 0 FC/FH toLOVA300-600Airworthiness Limitations Itemsfront spar to rear spar. Int. 6900 FC10300 FHN 572163-01-2A-S 541/641542/642543/643541/641AB, BB,CB542/642 CB, DB,EB543/643 AB, BB,CB, DBDetailed inspection of outer wing bottom skin stringers fromrib 1 to rib 14.Th. 42500 FC63600 FHInt. 21200 FC31800 FHB4-600B4-600RFrom 0 FC/FH toLOVR 572164-01-3A-S 543/643550/650543/643 DB550/650 BBSpecial detailed inspection (HFEC) of outer wing bottom skinstringers adjacent to rib 14.Th. 24900FC37400FHInt. 4800FC7100FHNTM 572164 B4-600/B4-600RPRE 10324PRE 10325PRE 10326(57-6046)From 0 FC/FH toLOVN 572503-01-2A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib14 to rib 27, excluding areas adjacent to stringer terminationplates.Th. 42400 FC63600 FHInt. 4700 FC6900 FHB4-600/B4-600RPRE 4741PRE 10470(57-6048)From 0 FC/FH toLOVIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section E© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document.Page : 2 - ERevCodeTaskReferenceZone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteA300-600Airworthiness Limitations ItemsN 572503-01-3A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib14 to rib 27, excluding areas adjacent to stringer terminationplates.Th. 46700 FC69900 FHInt. 16400 FC24600 FHB4-600/B4-600RPOST 4741PRE 10324PRE 10325PRE 10470(57-6048)From 0 FC/FH toLOVN 572504-01-2A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib14 to rib 27.Th. 42400 FC63600 FHInt. 4700 FC6900 FHB4-600/B4-600RPRE 4741POST 10470(57-6048)From 0 FC/FH toLOVN 572504-01-3A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing front spar aft face from rib14 to rib 27.Th. 46700 FC69900 FHInt. 16400 FC24600 FHB4-600/B4-600RPOST 10324ORB4-600/B4-600RPOST 10325ORB4 600/From 0 FC/FH toLOVB4-600/B4-600RPOST 4741POST 10470(57-6048)N 572507-01-2A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib14 to rib 27, excluding area adjacent to stringer terminationplate from rib 21 to rib 22.Th. 39000 FC58400 FHInt. 8500 FC12700 FHB4-600/B4-600RPRE 4741PRE 10470(SB 57-6048)From 0 FC/FH toLOVN 572507-01-3A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib14 to rib 27, excluding area adjacent to stringer terminationplate from rib 21 to rib 22.Th. 43000 FC64400 FHInt. 21500 FC32200 FHB4-600/B4-600RPOST 4741PRE 10324PRE 10325PRE 10470(SB 57-6048)From 0 FC/FH toLOVN 572508-01-2A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib14 to rib 27.Th. 39000 FC58400 FHInt. 8500 FC12700 FHB4-600/B4-600RPRE 4741POST 10470(SB 57-6048)From 0 FC/FH toLOVIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section E© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document.Page : 3 - ERevCodeTaskReferenceZone Access Task DescriptionTh.Int.NTMRef.Appli.Appli.PeriodNoteA300-600Airworthiness Limitations ItemsN 572508-01-3A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing rear spar fwd face from rib14 to rib 27.Th. 43000 FC64400 FHInt. 21500 FC32200 FHB4-600/B4-600RPOST 10324ORB4-600/B4-600RPOST 10325ORB4-600/B4-600RPOST 4741POST 10470(SB 57-6048)From 0 FC/FH toLOVN 572521-01-2A-S 550/650 550/650 BB, DB,EB, FB, GB, HB,JB, KB, LB, MB,NB, PB, QBDetailed inspection of outer wing bottom skin stringers fromrib 14 to rib 27.Th. 42500 FC63600 FHInt. 6800 FC10000 FHB4-600B4-600RFrom 0 FC/FH toLOVR 572525-01-1A-S 550/650 550/650 LB to QB Special detailedinspection (HFEC) of outer wing bottom skinaccess doors and door surrounds from rib 22 to rib 27.Th. 19400 FC29200 FHInt 13200 FCNTM 572525 ALLF4-600R/C4 605R F/From 0 FC/FHto LOVNote : TPS not to be applied to upper surface of wing skin.Int.13200FC19800 FHC4-605R.F/C4-600N 572525-01-2A-S 550/650 550/650 LB to QB Special detailedinspection (HFEC) of outer wing bottom skinaccess doors and door surrounds from rib 22 to rib 27.Note : TPS not to be applied to upper surface of wing skin.Th. 19400 FC29200 FHInt. 10300 FC15500 FHNTM 572525 B4-600B4-600RFrom 0 FC/FH toLOVN 574106-01-2A-S 512/612523/623524/624Slat extended Detailed inspection ofouter wing leading edge "D" nose skinjoint plate (including reinforcing plate and landing reinforcingplate) at slat track cutouts.Th. 45900 FC68800 FHInt. 3500 FC5300 FHB4-600B4-600RFrom 0 FC/FH toLOVN 574111-01-3A-S 512/612523/623512/612 KB, LB523/623 AB, BBDetailed inspection of outerwing fixed leading edge ribsinboard and outboard of pylon.Th. 45900 FC68800 FHInt. 5400 FC8100 FHB4-600B4-600RFrom 0 FC/FH toLOVN 574129-01-2A-S 500/600 N/A Detailed inspection of outer wing bottom skin lower surfacefwd of front spar from root to tip.Th. 51000 FC77400 FHInt. 24800 FC37200 FHB4-600B4-600RFrom 0 FC/FH toLOVIssue: FEB 2011 TR13.1Ref: 95A.1310/07EASA APPROVEDALI Section E© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document.Page : 4 - E

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### A300-600 AIRWORTHINESS LIMITATION ITEMS

ISSUE: FEBRUARY 2011 PAGE: TR13.1- 4

© AIRBUS SAS 2011. All rights reserved. Confidential and proprietary document. 

### NEW DT ALI ILLUSTRATIONS

Introduction:

The "DT ALI ILLUSTRATIONS" appendice provides illustrated information related to the DT ALI.

Each illustration indicates the DT ALI location within its environment together with additional

information, thus to facilitate the understanding of the requirement.

The DT ALI Illustrations are identified by the related DT ALI reference as defined in sub and are

arranged by ATA sequence.

Each DT ALI Illustration provides the following information:

DT ALI Description:

Item description in line with inspection requirement of this document.

DT ALI Reference:

Item ATA reference as defined in section D of this document.

Illustration:

Each illustration compiles with the following rules:

(1) The DT ALI is illustrated by actual photo or by drawing.

(2) The area to be inspected is limited by doted line, as follows:

■ ■ ■ ■ : when the area is visible on the photo/drawing.

□ □ □ □ : when the area is hidden - on the photo/drawing - by other structure or

equipment.

(3) Whenever necessary, several illustrations have been used so as to clearly identify

the DT ALI.

(4) Whenever one photo is used to illustrate several DT ALIs or parts of the same DT

ALI, the information "TYPICAL VIEW" is mentioned.

(5) If due to similarity or symmetry, the illustration shows only a part of the DT ALI, the

information "PART VIEW" is mentioned.

(6) Whenever a photo in "maintenance condition" did not allow a clear identification of

the DT ALI, a photo has been taken at an earlier stage of assembly. Consequently the

information "NOT IN MAINTENANCE CONDITION" is mentioned.

(7) The localization of an DT ALI is defined by the following data:

- Illustration orientation relative to the aircraft.

- Identification of the surrounding frames, stringers, ribs, ...

- Other specific information as deemed necessary.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing front spar AFT face from rib 9 to rib 14. 52108

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 5

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing rear spar fwd face between rib 9 and rib 14 572124

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 6

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing centre spar, pylon fitti ng, forward and aft faces. 572125

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 7

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing centre spar upper and lower booms between rib 8 and

rib 9. 572131

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 8

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing top skin upper surface at attachments to ribs and

stringers from ribs 1 and 14 and fr om front spar to rear spar 572149

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 9

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing bottom skin stringers fr om rib 1 to rib 14 572163

(1/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 10

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing bottom skin stringers fr om rib 1 to rib 14 572163

(2/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 11

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing front spar aft face from rib 14 to rib 27, excluding areas

adjacent to stringer termination plates. 572503

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 12

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing front spar aft face from rib 14 to rib 27 572504

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 13

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing rear spar forward face from rib 14 to rib 27, excluding

area adjacent to stringer terminati on plate from rib 21 to rib 22. 572507

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 14

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing rear spar forward face from rib 14 to rib 27. 572508

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 15

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing bottom skin stringers fr om rib14 to rib 27. 572521

(1/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 16

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing bottom skin stringers from rib14 to rib 27 572521

(2/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 17

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing leading edge ”D” nos e skin joint plate (including

reinforcing plate and landing reinforci ng plate) at slat track cutouts. 574106

(1/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 18

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing leading edge ”D” nos e skin joint plate (including

reinforcing plate and landing reinforci ng plate) at slat track cutouts. 574106

(2/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 19

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing fixed leading edge ribs i nboard and outboard of pylon. 574111

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 20

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing bottom skin lower surfac e forward of front spar from

root to tip. 574129

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 21

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing top skin upper surface and reinforcing at access door

cutouts inboard of rib 6A aft of rear spar. 575135

(1/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 22

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

# A300-600

AIRWORTHINESS LIMITATION ITEMS

DT ALI DESCRIPTION DT ALI Ref.

Outer wing top skin upper surface and reinforcing at access door

cutouts inboard of rib 6A aft of rear spar. 575135

(2/2)

ISSUE : FEBRUARY 2011 DT ALI ILLUSTRATION PAGE : TR13.1 - 23

© AIRBUS SAS 2011. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.