| Number |
2006-0301R2 |
| Issued by |
 Europe |
| Issue date |
2009-09-10 |
| Effective date |
2006-10-19 |
| EASA approval number |
Not applicable |
| ATA Chapter |
32 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
|
| Revision |
This AD revises EASA AD 2006-0301R1 dated 10 October 2006
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A340-32-4212 Original issue or SB A340-32-4212 Revision 1 or SB
A340-32-4212 Revision 02 or SB A340-32-4212 Revision 03 or SB A340-32-
4212 Revision 04;
Airbus Service Bulletin A340-32-4222 Revision 01;
Airbus Service Bulletin A340-32-4213 Revision 01.
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
06-146 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 13 June 2006 as PAD
06-146 for consultation until 27 June 2006.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@easa.europa.eu.
4. For any questions concerning the technical content of the requirements in
this AD, please contact:
AIRBUS – Airworthiness Office – EAL; Fax: +33 5 61 93 45 80.
E-mail: airworthiness.A330-A340@Airbus.com .
|
