| Number |
2012-0021 |
| Issued by |
 Europe |
| Issue date |
2012-01-30 |
| Effective date |
2012-02-13 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
AIRBUS S.A.S.
-
A340
-
A340-211
-
A340-212
-
A340-213
-
A340-311
-
A340-312
-
A340-313
-
A340-541
-
A340-542
-
A340-642
-
A340-643
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France ADs F-2001-519(B) dated 31 October 2001,
F-2001-529(B)R1 dated 17 September 2003, F- 2001-549(B)R1 dated 16
October 2002, F-2002-553(B) dated 13 November 2002 and F-2003-141(B)R1
dated 17 March 2004. This AD also supersedes EASA ADs 2006-0158 dated 07
June 2006, 2007-0008 dated 09 January 2007, 2007-0308 dated 18 December
2007, 2009-0138 dated 24 June 2009 and 2010-0205 dated 08 October 2010.
|
| Publication(s) and related information |
Airbus A340 ALS Part 4 revision 02, approved by EASA on 12 October
2011.
The use of later approved variations or revisions of this document is
acceptable for compliance with the requirements of this AD. |
| PAD number |
11-131 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 02 December 2011 as PAD 11-131 for
consultation until 28 December 2011. No comments were received during
the consultation period.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|
