A330 AIRWORTHINESS LIMITATIONS SECTION 

Variation to Issue 19 

Of 

ALI Document 

(referenced in ALS Part 2) 

- 

Damage Tolerant Airworthiness 

Limitation Items (DT ALI) 

© AIRBUS SAS 2013. 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. 

ISSUE: MAR 26/13 Variation ref.: 0GVLG130002/C01 
A330 AIRWORTHINESS LIMITATIONS SECTION 

The European Aviation Safety Agency (EASA) Certification Directorate approves the ALI 

Document referenced in the ALS Part 2. Variations must also be approved. 

Approval references:

A330 ALI Document: 

ISSUE 

NUMBER SUB-PARTS APPROVED BY 

EASA 

APPROVAL 

REFERENCE 

INSERTION IN 

MAINT. PROG. 

19 N/A JUN 08/12 10040023 

Variation: 

This Variation to the issue 19 of the A330 ALI Document is covered by the Certification 

Document 0GVLG130002/C01: 

ISSUE 

NUMBER 

AFFECTED 

SUB-PARTS 

APPROVED BY 

EASA 

APPROVAL 

REFERENCE 

INSERTION IN 

MAINT. PROG. 

01 N/A MAR 26/13 10044208 Rev 01 

Reason:

The current procedure for task 712204-01-01 has been revised to provide improved detectability of 

the possible failure indication, (activation of secondary load path). This change, which requires the 

use of a borescope, causes the task to be re-identified as a special detailed inspection. 

Consequently, a new task number is required. This variation introduces that number. The existing 

inspection intervals remain valid for this procedure. 

Applicability:

This variation is applicable to A330-243, A330-243F, A330-341, A330-342, and A330-343 

aircraft. 

Compliance:

It is mandatory to comply with the instructions and airworthiness limitations specified in this 

variation. It is intended to include the content of this variation in a subsequent revision of the 

A330 ALI Document. 

Validity:

Airworthiness limitations stated in this Variation may be negated when airworthiness limitation 

changes are published in a revision of the following document(s) subsequent to the approval 

date of this Variation: 

− A330 ALI Document issue 19. 

In such case, the validity of this Variation is suspended.

ISSUE: MAR 26/13 EASA APPROVAL REF. 10044208 Rev 01 PAGE: 1/2 

© AIRBUS SAS 2013. All rights reserved. Confidential and proprietary document.
A330 AIRWORTHINESS LIMITATIONS SECTION 

Description:

The EASA requires the use of the task 712204-03-01 in lieu of A330 ALI Document Issue 19 task 712204-01-0The new procedure (AMM TASK 71-22-41-200-804-A) was published by TEMPORARY REVISION N°71-006 o

February 18th 2013. 

The A330 ALI Document Issue 19 Section 2.2.1 is revised as follows: Standard Range (SR) 

REV 

CODE 

TASK 

REFERENCE ACCESS TASK DESCRIPTION THRESHOLD INTE

D 712204-01-01 TASK DELETED 

N 712204-03-01 417AL 418AR 

427AL 428AR 

SPECIAL DETAILED INSPECTION OF AFT ENGINE MOUNT FAIL-SAFE LINK. NOTE: INSPECTION FOR ACTIVATION OF SECONDARY LOAD PATH. 

4130 FC OR 42600 FH 

4130 OR 4260

Operators who have accomplished this new task prior to approval of this variation may take credit for that acc

to show compliance with this variation. The following grace period can be applied; If the engine mount has already been inspected by ALI task 712204-01-01 since the last engine installation or ALI task, 712204-03-01, has to be performed prior to 6880 FC since the last engine removal or since new. 

ISSUE: MAR 26/13 EASA APPROVAL REF. 10044208 Rev 01 

© AIRBUS SAS 2013. All rights reserved. Confidential and proprietary document.