AIRBUS

Customer Services 

© AIRBUS SAS 2011. 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 

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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ISSUE: FEBRUARY 2011 PAGE: 1-ROR 

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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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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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©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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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 rules, 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 Airworthiness 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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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. 
CUSTOMER SERVICES

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). 
Rev 

Code Task Reference Zone Access Task Description Th. Int. NTM Ref. 

N 572108-01-3A 543/643 543/643 AB to DB Detailed inspection of outer wing front spar AFT face from rib 9 

to rib 14 

Th. 49500 FC

 89000 FH

Int. 3500 FC

 7500 FH

N 572124-01-2A 543/643 543/643 AB to DB Detailed inspection of outer wing rear spar fwd face between rib 

9 and rib 14.

Th. 47200 FC

89000 FH

Int. 7900 FC

 17000 FH

N 572125-01-3A 541/641 

542/642 

541/641CB 542/642 DB

Special detailed inspection (Ultrasonic) of outer wing center spar, pylon fitting, fwd and aft faces.

Th. 45200 FC

89000 FH

Int. 4400 FC 

9500 FH

NTM 57212

N 572131-01-2A 541/641

542/642 

542/642 EB Detailed inspection of outer wing center spar upper and lower 

booms between rib 8 and rib 9.

Th. 49500 FC

89000 FH

Int. 7200 FC

 15500 FH

N 572149-01-3A 500/600 N/A Detailed inspection of outer wing top skin upper surface at 

attachments to ribs and stringers from ribs 1 to 14 and from 

Th. 39700 FC

85700 FH

A300-600

Airworthiness Limitations Items 

g

front spar to rear spar. Int. 6400 FC

13800 FH

N 572163-01-2A 541/641

542/642 543/643 

541/641 AB,BB, CB542/642 CB, DB543/643 AB, BB, CB, DB

Detailed inspection of outer wing bottom skin stringers from rib 1 to rib 14.

Th. 39300 FC

84800 FH

Int. 19600 FC

42400 FH

R 572164-01-3A 543/643

550/650

543/643 DB550/650 BB

Special detailed inspection (HFEC) of outer wing bottom skin stringers adjacent to rib 14.

Th. 23100FC

49900FH

Int. 4400FC

9500FH

NTM 572

N 572503-01-2A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27, excluding areas adjacent to stringer termination plates.

Th. 39300 FC

 84800 FH

Int. 4300 FC

 9200 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section D

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

Code Task Reference Zone Access Task Description Th. Int. NTM Ref. 

A300-600

Airworthiness Limitations Items 

N 572503-01-3A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27, excluding areas adjacent to stringer termination plates.

Th. 43200 FC

89000 FH

Int. 15200 FC

 32800 FH

N 572504-01-2A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27.

Th. 39300 FC

84800 FH

Int. 4300 FC

 9200 FH

N 572504-01-3A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27.

Th. 43200 FC

89000 FH

Int. 15200 FC

 32800 FH

N 572507-01-2A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27, excluding area adjacent to stringer termination plate from rib 21 to rib 22.

Th. 36100 FC

 77900 FH

Int. 7900 FC

 17000 FH

N 572507-01-3A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27, excluding area adjacent to stringer termination plate from rib 21 to rib 22.

Th. 39800 FC

 85900 FH

Int. 19900 FC

 42900 FH

N 572508-01-2A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27.

Th. 36100 FC

77900 FH

Int. 7900 FC

 17000 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section D

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

Code Task Reference Zone Access Task Description Th. Int. NTM Ref. 

A300-600

Airworthiness Limitations Items 

N 572508-01-3A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27.

Th. 39800 FC

 85900 FH

Int. 19900 FC

 42900 FH

N 572521-01-2A 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB 

Detailed inspection of outer wing bottom skin stringers from rib 14 to rib 27.

Th. 39300 FC

 84800 FH

Int. 6200 FC

 13300 FH

R 572525-01-1A 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skin 

access doors and door surrounds from rib 22 to rib 27.

Th. 18000 FC 

38900 FH

Int. 12200 FC 

NTM 5725

Note : TPS not to be applied to upper surface of wing skin. 26300 FH 

N 572525-01-2A 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skin 

access doors and door surrounds from rib 22 to rib 27.Note : TPS not to be applied to upper surface of wing skin.

Th. 18000 FC 

38900 FH

Int. 9600 FC 

20700 FH

NTM 5725

N 574106-01-2A 512/612

523/623524/624

Slat extended Detailed inspection of outer wing leading edge "D" nose skin 

joint plate (including reinforcing plate and landing reinforcing plate) at slat track cutouts.

Th. 42500 FC

89000FH

Int. 3300 FC

 7100 FH

N 574111-01-3A 512/612

523/623

512/612 KB, LB523/623 AB, BB

Detailed inspection of outer wing fixed leading edge ribs inboard and outboard of pylon.

Th. 42500 FC

 89000FH

Int. 5000 FC

 10800 FH

N 574129-01-2A 500/600 N/A Detailed inspection of outer wing bottom skin lower surface fwd 

of front spar from root to tip.

Th. 47800 FC

89000FH

Int. 23000 FC

 49600 FH

N 575135-01-2A 500/600

575/675

575/675 AT, BT Detailed inspection of outer wing top skin upper surface and 

reinforcing at access door cutouts inboard of from rib 6A aft of rear spar.

Th. 42500 FC

 89000FH

Int. 10400 FC

 23400 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section D

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

Code Task 

Reference Zone Access Task Description Th. Int. NTM Ref. 

N 572108-01-3A-S 543/643 543/643 AB to DB Detailed inspection of outer wing front spar AFT face from rib 

9 to rib 14 

Th. 51000 FC

 80100 FH

Int. 3700 FC

 5600 FH

N 572124-01-2A-S 543/643 543/643 AB to DB Detailed inspection of outer wing rear spar fwd face between 

rib 9 and rib 14.

Th. 51000 FC

 76400 FH

Int. 8500 FC

 12700 FH

N 572125-01-3A-S 541/641

542/642 

541/641CB 542/642 DB

Special detailed inspection (Ultrasonic) of outer wing center spar, pylon fitting, fwd and aft faces.

Th. 48800 FC

 73200 FH

Int. 4800 FC

 7100 FH

NTM 572125 

N 572131-01-2A-S 541/641

542/642

542/642 EB Detailed inspection of outer wing center spar upper and lower 

booms between rib 8 and rib 9.

Th. 51000 FC

80100 FH

Int. 7800 FC

 11600 FH

N 572149-01-3A-S 500/600 N/A Detailed inspection of outer wing top skin upper surface at 

attachments to ribs and stringers from ribs 1 and 14 and from 

Th. 42800 FC

 64300 FH

A300-600

Airworthiness Limitations Items

front spar to rear spar. Int. 6900 FC

 10300 FH

N 572163-01-2A-S 541/641

542/642543/643

541/641AB, BB, CB 542/642 CB, DB, EB543/643 AB, BB, CB, DB

Detailed inspection of outer wing bottom skin stringers from rib 1 to rib 14.

Th. 42500 FC

63600 FH

Int. 21200 FC

31800 FH

R 572164-01-3A-S 543/643

550/650

543/643 DB550/650 BB

Special detailed inspection (HFEC) of outer wing bottom skin stringers adjacent to rib 14.

Th. 24900FC

37400FH

Int. 4800FC

7100FH

NTM 572

N 572503-01-2A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27, excluding areas adjacent to stringer termination plates.

Th. 42400 FC

 63600 FH

Int. 4700 FC

6900 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section E

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

Code Task 

Reference Zone Access Task Description Th. Int. NTM Ref. 

A300-600

Airworthiness Limitations Items

N 572503-01-3A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27, excluding areas adjacent to stringer termination plates.

Th. 46700 FC

 69900 FH

Int. 16400 FC

 24600 FH

N 572504-01-2A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27.

Th. 42400 FC 

63600 FH

Int. 4700 FC 

6900 FH

N 572504-01-3A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing front spar aft face from rib 14 to rib 27.

Th. 46700 FC 

69900 FH

Int. 16400 FC 

24600 FH

N 572507-01-2A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27, excluding area adjacent to stringer termination plate from rib 21 to rib 22.

Th. 39000 FC

 58400 FH

Int. 8500 FC

 12700 FH

N 572507-01-3A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27, excluding area adjacent to stringer termination plate from rib 21 to rib 22.

Th. 43000 FC

 64400 FH

Int. 21500 FC

 32200 FH

N 572508-01-2A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27.

Th. 39000 FC 

58400 FH

Int. 8500 FC

 12700 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section E

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

Code Task 

Reference Zone Access Task Description Th. Int. NTM Ref. 

A300-600

Airworthiness Limitations Items

N 572508-01-3A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB

Detailed inspection of outer wing rear spar fwd face from rib 14 to rib 27.

Th. 43000 FC

 64400 FH

Int. 21500 FC

 32200 FH

N 572521-01-2A-S 550/650 550/650 BB, DB, 

EB, FB, GB, HB, JB, KB, LB, MB, NB, PB, QB 

Detailed inspection of outer wing bottom skin stringers from rib 14 to rib 27.

Th. 42500 FC

 63600 FH

Int. 6800 FC

 10000 FH

R 572525-01-1A-S 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skin 

access doors and door surrounds from rib 22 to rib 27.

Th. 19400 FC 

29200 FH

Int 13200 FC

NTM 5725

Note : TPS not to be applied to upper surface of wing skin.

Int. 13200 FC

19800 FH

N 572525-01-2A-S 550/650 550/650 LB to QB Special detailed inspection (HFEC) of outer wing bottom skin 

access doors and door surrounds from rib 22 to rib 27.Note : TPS not to be applied to upper surface of wing skin.

Th. 19400 FC 

29200 FH

Int. 10300 FC 

15500 FH

NTM 5725

N 574106-01-2A-S 512/612

523/623524/624

Slat extended Detailed inspection of outer wing leading edge "D" nose skin 

joint plate (including reinforcing plate and landing reinforcing 

plate) at slat track cutouts.

Th. 45900 FC

 68800 FH

Int. 3500 FC

 5300 FH

N 574111-01-3A-S 512/612

523/623

512/612 KB, LB523/623 AB, BB

Detailed inspection of outer wing fixed leading edge ribs 

inboard and outboard of pylon.

Th. 45900 FC

 68800 FH

Int. 5400 FC

 8100 FH

N 574129-01-2A-S 500/600 N/A Detailed inspection of outer wing bottom skin lower surface 

fwd of front spar from root to tip.

Th. 51000 FC

 77400 FH

Int. 24800 FC

 37200 FH

Issue: FEB 2011 TR13.1Ref: 95A.1310/07

EASA APPROVED

ALI Section E

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

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 fitting, 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 from 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 from 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 from 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 termination 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 from 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” nose skin joint plate (including 

reinforcing plate and landing reinforcing 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” nose skin joint plate (including 

reinforcing plate and landing reinforcing 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 inboard 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 surface 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.