Number |
2010-0251 |
Issued by |
Europe |
Issue date |
2010-11-29 |
Effective date |
2010-12-13 |
EASA approval number |
|
ATA Chapter |
57 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
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)
-
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 Service Bulletins:
A300-57-0249 original issue or revision 01
A310-57-2090 original issue or revision 01
A300-57-6106 original issue or revision 01
A300-57-9019 original issue or revision 01
Airbus Repair Instruction R57249121 or R57240221
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
10-002, 07-206 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative
Methods of Compliance for this AD.
2. This AD was posted on 05 January 2010 as PAD 10-002 for consultation
until 02 February 2010. The Comment Response Document can be found
at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|