| Number |
2014-0034 |
| Issued by |
Europe |
| Issue date |
2014-02-05 |
| Effective date |
2014-02-19 |
| EASA approval number |
|
| ATA Chapter |
24 |
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 |
None
|
| Publication(s) and related information |
Airbus SB A300-24-6103 Revision 02 dated 07 February 2013.
Airbus SB A300-24-9014 original issue dated 17 June 2010, or Revision 01 dated 23 April 2013.
Airbus SB A310-24-2105 original issue dated 20 March 2013 or Revision 01 dated 11 December 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-157 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 11 October 2013 as PAD 13-157 for consultation until 08 November 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.
|