| Number |
2013-0234R2 |
| Issued by |
 Europe |
| Issue date |
2013-10-07 |
| Effective date |
2013-10-08 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-102
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
A300B4-220
-
A300B4-2C
-
A300C4-203
-
A300F4-203
-
A300-600
-
A300B4-601
-
A300B4-603
-
A300B4-605R
-
A300B4-620
-
A300B4-622
-
A300B4-622R
-
A300C4-605R variant F
-
A300C4-620
|
| Revision |
This AD revises EASA AD 2013-0234R1 dated 02 October 2013.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A300-57-0116 Revision 07 dated 19 September 2011.
Airbus SB A300-57-6005 Revision 05 dated 25 April 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-121 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 20 August 2013 as PAD 13-121 for consultation until 17 September 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.
|
