Number |
2014-0026 |
Issued by |
Europe |
Issue date |
2014-01-28 |
Effective date |
2014-02-11 |
EASA approval number |
|
Contributor |
EASA Large Aeroplane Section |
ATA Chapter |
55 |
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 A310-55-2051 initial issue dated 11 September 2012.
Airbus SB A300-55-6050 initial issue dated 11 September 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
13-051R1 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 03 April 2013 as PAD 13-051 for consultation until 01
EASA AD No.: 2014-0026
TE.CAP.00110-003 © European Aviation Safety Agency. All rights reserved. 3/3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
May 2013 and re-published on 26 August 2013 as PAD 13-051R1 for additional consultation until 09 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.
|