| Number |
2009-0081R1 |
| Issued by |
 Europe |
| Issue date |
2010-07-30 |
| Effective date |
2010-08-13 |
| 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
-
A300C4-620
-
A300F4-605R
|
| Revision |
This AD revises AD 2009-0081, dated 06 April 2009.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus Service Bulletins:
A300-57-0235 original issue up to revision 05
A300-57-6088 original issue up to revision 04
A300-57A0246 Revision 03
A300-57A6101 Revision 03
A300-57-0254 original issue
A300-57-6110 original issue
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The required actions and the risk allowance have granted the issuance of
a Final AD with Request for Comments, postponing the public
consultation process after publication.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA; E-mail ADs[@]easa.europa.eu.
|
