Number |
2013-0204 |
Issued by |
Europe |
Issue date |
2013-09-06 |
Effective date |
2013-09-20 |
EASA approval number |
|
Contributor |
EASA Large Aeroplane Section |
ATA Chapter |
29 / 24 |
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
-
A300-600ST (Beluga)
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2011-0084 dated 24 May 2011.
|
Publication(s) and related information |
Airbus SB A300-24-0106 original issue dated 09 July 2010 or Revision 01 dated 26 March 2013.
Airbus SB A300-24-6108 original issue dated 09 July 2010 or Revision 01 dated 26 March 2013.
Airbus SB A300-24-9016 original issue dated 09 July 2010 or Revision 01 dated 26 March 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
13-105 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 25 July 2013 as PAD 13-105 for consultation until 22 August 2013. No comments were received during the consultation period.
3. Enquiries regarding this PAD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|