Number |
2013-0075 |
Issued by |
Europe |
Issue date |
2013-03-20 |
Effective date |
2013-04-03 |
EASA approval number |
|
Contributor |
EASA Large Aeroplane Section |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300-600
-
A300B4-601
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
-
A300F4-605R
-
A300F4-622R
-
A300-600ST (Beluga)
-
A310
-
A310-203
-
A310-203C
-
A310-204
-
A310-221
-
A310-222
-
A310-304
-
A310-308
-
A310-322
-
A310-324
-
A310-325
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2007-0092 dated 10 April 2007.
|
Publication(s) and related information |
Airbus A300-600 ALS Part 4 Revision 02, approved by EASA on 18 April 2012.
Airbus A310 ALS Part 4 Revision 02, approved by EASA on 30 November 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
12-046R1 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was initially posted on 15 May 2012 as PAD 12-046 for consultation until 12 June 2012, and republished on 28 February 2013 as PAD 12-046R1 for consultation until 14 March 2013. The Comment Response Document can be found at https://ad.easa.europa.eu.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|