EASA AD No : 2009-0155

EASA Form 110 Page 1/2 

## EASA AIRWORTHINESS DIRECTIVE

AD No.: 2009-0155

Date: 17 July 2009

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in th e activities of EASA under Article 66 of that Regulation.
This AD is issued in accordance with EC 1702/2003, Part 21A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may opera te an aircraft to which an AD applies, except in accordance with t he requirements of that AD, unless otherwise specified by the Ag ency [EC 2042/2003 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemptio n]. 

### Type Approval Holder’s Name :

AIRBUS SAS Type/Model designation(s) :
A300, A310 and A300-600 aeroplanes

TCDS Number : France TCDS No 145

Foreign AD : Not applicable

Supersedure : This AD su persedes EASA AD No. 2006-0071 dated 30 March 2006, EASA AD No. 2006-0260 dated 25 August 2006 and EASA AD No. 2006-0374 dated 15 December 2006.



### ATA 05 Time Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – Amendment

Manufacturer(s): Airbus (formerly Airbus Industrie)

Applicability: A300, A310 and A300-600 aeroplane s, all certified models, all serial numbers.

Reason: The airworthiness limitations applicable to the Damage Tolerant Airworthiness Limitation Items (DT ALI) are currently listed in Airbus ALI Documents, which are referenced in the A300, A310 and A300-600 Airworthiness Limitations Section (ALS) Part 2. Airbus has rece ntly revised the ALI Documents, which have been approved by the European Aviation Safety Agency (EASA): - AIRBUS A300 ALI Document issue 04, - AIRBUS A310 ALI Document issue 07 and - AIRBUS A300-600 ALI Document issue 12. The actions contained in these revised documents, which introduce more restrictive maintenance requirements and/or airworthiness limitations, have been identified as mandat ory actions for continued airworthiness. EASA issued ADs 2006-0071, 2006-0260 and 2006-0374 to require compliance with the maintenance requirements and asso ciated airworthiness limitations defined in previous issues of these Airbus ALI Documents. For the reason described above, th is EASA AD supersed es existing EASA ADs 2006-0071, 2006-0260 and 2006-0374 and requires an update to the approved aircraft maintenance programme and compliance with the maintenance requirements and associated ai rworthiness limitations defined in the Airbus ALI Documents listed above.EASA AD No : 2009-0155

EASA Form 110 Page 2/2 Effective Date: 31 July 2009

Required Action(s) and Compliance Time(s): From the effective date of this AD, the following measures are required as indicated: Within the compliance times defined in the Record Of Revisions (ROR) pages of each document, each Operator must: - Review and assess the content of AIRBUS A300 ALI Document issue 04, reference AI/SE-M2/95A.1308/07 and/or AIRBUS A310 ALI Document issue 07, reference AI/SE-M2/95A. 1309/07 and/or AIRBUS A300-600 ALI Document issue 12, refere nce AI/SE-M2/95A.1310/07,
and - Incorporate into the approved maintenance programme all applicable changes to maintenance requirements or associated airworthiness limitations included in AIRBUS A300 ALI Document issue 04, reference AI/SE-M2/95A.1308/07 and/or AIRBUS A310 ALI Document issue 07, reference AI/SE-M2/95A.1309/07 and/or AIRBUS A300-600 ALI Document issue 12, reference AI/SE-M2/95A.1310/07,
and - Comply with any action required by AIRBUS A300 ALI Document issue 04, reference AI/SE-M2/95A.1308/07 and/or AIRBUS A310 ALI Document issue 07, reference AI/SE-M2/95A. 1309/07 and/or AIRBUS A300-600 ALI Document issue 12, refere nce AI/SE-M2/95A.1310/07.

Ref. Publications: Airbus A300 ALI Document issue 04, reference AI/SE-M2/95A.1308/07 approved under reference EASA.A. C.10909 on 02 December 2008. Airbus A310 ALI Document issue 07, reference AI/SE-M2/95A.1309/07 approved under reference EASA.A. C.10907 on 02 December 2008.
Airbus A300-600 ALI Document iss ue 12, reference AI/SE-M2/95A.1310/07 approved under reference EASA.A. C.10908 on 09 December 2008. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

Remarks : 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 23 April 2009 as PAD 09-029 for consultation until 14 May 2009. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the Airworthiness Directives, Safety Management & Re search Section, Certification Directorate, EASA. E-mail ADs@easa.europa.eu

. 4. For any question concerning the tec hnical content of the requirements in this AD, please contact: AIRBUS SAS – EAW Airworthiness Office, telephone: + 33 5 61 93 36 96, facsimile: + 33 5 61 93 44 51.