| Number |
2011-0212 |
| Issued by |
 Europe |
| Issue date |
2011-10-31 |
| Effective date |
2011-11-14 |
| EASA approval number |
|
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A330
-
A330-201
-
A330-202
-
A330-203
-
A330-223
-
A330-223F
-
A330-243
-
A330-243F
-
A330-301
-
A330-302
-
A330-303
-
A330-321
-
A330-322
-
A330-323
-
A330-341
-
A330-342
-
A330-343
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus A330 ALS Part 1 revision 05, approved on 29 July 2010;
Messier-Dowty Service Letter A33-34 A20 revision 05 dated 31 July 2009.
|
| 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 Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa[dot]europa[dot]eu.
4. For any questions concerning the technical content of the requirements in this AD, please contact: AIRBUS – Airworthiness Office – EAL;
E-mail: airworthiness[dot]A330-A340[at]airbus[dot]com.
|
