Number |
2013-0014 |
Issued by |
Europe |
Issue date |
2013-01-16 |
Effective date |
2013-01-30 |
EASA approval number |
|
ATA Chapter |
54 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
A300B4-2C
-
A300C4-203
-
A300F4-203
-
A300-600
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-620
-
A310
-
A310-221
-
A310-222
-
A310-322
-
A310-324
-
A310-325
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD 1992-049-130(B) R4 dated 02 June 1999 and
EASA AD 2008-0008 dated 11 January 2008.
|
Publication(s) and related information |
AIRBUS SB A300-54-0071 Revision 03 dated 05 October 2012;
AIRBUS SB A310-54-2016 Revision 05 dated 05 October 2012;
AIRBUS SB A300-54-6011 Revision 03 dated 23 June 2011;
AIRBUS SB A300-54-0079 Revision 01 dated 09 July 2002;
AIRBUS SB A310-54-2022 Revision 02 dated 09 July 2002;
AIRBUS SB A300-54-6019 Revision 02 dated 07 April 2003.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
12-157 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 04 December 2012 as PAD 12-157 for consultation until 01 January 2013. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|