Number |
2015-0146 |
Issued by |
Europe |
Issue date |
2015-07-24 |
Effective date |
2015-08-05 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes Section |
ATA Chapter |
25 |
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
-
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 |
This AD is republished to correct a typographical error in the Reason.
|
Supersedure |
This AD supersedes EASA Emergency AD 2012-0245-E dated 16 November 2012.
|
Publication(s) and related information |
Airbus AOT A25W003-12 Revision 1 dated 14 November 2012.
Airbus SB A300-25-6222 original issue dated 25 February 2015.
Airbus SB A310-25-2210 original issue dated 25 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
|
PAD number |
15-083 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 11 June 2015 as PAD 15-083 for consultation until 09 July 2015. 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.
|