A330 AIRWORTHINESS LIMITATIONS SECTION



# Variation to Issue 19

Of

ALI Document (referenced in ALS Part 2)

- Damage Tolerant Airworthiness Limitation Items (DT ALI)

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ISSUE: MAR 26/13 Variation ref.: 0GVLG130002/C01A330 AIRWORTHINESS LIMITATIONS SECTION

The European Aviation Safety Agency (EASA) Certification Directorate approves the A LI 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 Vari ation 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 SECTIONDescription:The EASA requires the use of the task 712204-03-01 in lieu of A330 ALI Document Issue 19 task 712204-01-01.The new procedure (AMM TASK 71-22-41-200-804-A) was published byTEMPORARY REVISION N°71-006 of the AMM, datedFebruary 18th2013.The A330 ALI Document Issue 19 Section 2.2.1 is revised as follows:Standard Range (SR)REVCODETASKREFERENCEACCESSTASK DESCRIPTIONTHRESHOLDINTERVALAPPLICABILITYD712204-01-01TASK DELETEDN712204-03-01417AL 418AR427AL428ARSPECIAL DETAILED INSPECTION OF AFT ENGINEMOUNT FAIL-SAFE LINK.NOTE: INSPECTION FOR ACTIVATION OFSECONDARY LOAD PATH.4130 FCOR42600 FH4130 FCOR42600 FHRROperators who have accomplished this new task prior to approval ofthis variation may take credit for that accomplishment in orderto 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 since new, the newALI task, 712204-03-01, has to be performed prior to 6880 FC since the last engine removal or since new.ISSUE: MAR 26/13EASA APPROVAL REF. 10044208 Rev 01PAGE: 2/2© AIRBUS SAS 2013. All rights reserved. Confidentialand proprietary document.