| Number |
2013-0230 |
| Issued by |
 Europe |
| Issue date |
2013-09-24 |
| 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
-
A300F4-605R
-
A300F4-622R
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A300-57-0204 Revision 01 dated 02 April 1999.
Airbus SB A300-57-6047 Revision 06 dated 17 October 2011.
Airbus ALI Document Issue 4, approved 02 December 2008.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-117 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 09 August 2013 as PAD 13-117 for consultation until 06 September 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.eu.
|
