Number |
2009-0165 |
Issued by |
Europe |
Issue date |
2009-07-31 |
Effective date |
2009-08-14 |
EASA approval number |
|
ATA Chapter |
53 |
Approval Holder / Type Designation |
-
AIRBUS S.A.S.
-
A300
-
A300B4-102
-
A300B4-103
-
A300B4-120
-
A300B4-203
-
A300B4-220
-
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
-
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 A300-53-0388 original issue,
Airbus SB A310-53-2131 original issue, and
Airbus SB A300-53-6164 original issue.
The use of later approved revisions of these documents is acceptable for
compliance with requirements of this AD. |
PAD number |
09-077 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative
Methods of Compliance for this AD.
2. This AD was posted on 29 May 2009 as PAD 09-077 for consultation until
26 June 2009. 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.
|