Number |
2010-0070 |
Issued by |
Europe |
Issue date |
2010-04-14 |
Effective date |
2010-04-28 |
EASA approval number |
|
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
-
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 2009-0084 dated 09 April 2009.
|
Publication(s) and related information |
AIRBUS AOT A310-25A2203 Revision 02, AOT A300-25A6215 Revision 02
and AOT A300-25A9010 Revision 02.
AIRBUS Service Bulletin A310-25-2205 Original issue, A300-25-6217 Original
issue, A300-25-9011 Original issue.
SOGERMA Alert Service Bulletin A2510112-25-764 original issue.
SOGERMA Inspection Service Bulletin 2510112-25-807 original issue.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
10-014 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 25 January 2010 as PAD 10-014 for consultation
until 22 February 2010. No comments were received during the
consultation period.
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.
|