Number |
2015-0118 |
Issued by |
Europe |
Issue date |
2015-06-24 |
Effective date |
2015-07-08 |
EASA approval number |
|
Contributor |
EASA Large Transport Aeroplanes |
ATA Chapter |
35 |
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 |
This AD supersedes EASA AD 2014-0280 dated 19 December 2014.
|
Publication(s) and related information |
Airbus AOT A35W008-14 dated 18 December 2014.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator. |
PAD number |
15-063 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 May 2015 as PAD 15-063 for consultation until 19 June 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.
|