| Number |
2009-0258 |
| Issued by |
 Europe |
| Issue date |
2009-12-10 |
| Effective date |
2009-12-24 |
| EASA approval number |
|
| ATA Chapter |
29 |
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
-
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 AOT A300-29A6062 at original issue.
Airbus AOT A310-29A2098 at original issue.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Hamilton Sundstrand SB 730816-29-15.
Hamilton Sundstrand SB 732365-29-7. |
| PAD number |
09-120 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 October 2009 as PAD 09-120 for consultation until 04 November. 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@easa.europa.eu.
4. For any question concerning the technical content of the requirements in
this AD, please contact: AIRBUS SAS – EAW (Airworthiness Office,
Telephone: + 33 5 61 93 36 96, Fax: + 33 5 61 93 44 51).
|
