| Number |
2012-0138 |
| Issued by |
 Europe |
| Issue date |
2012-07-26 |
| Effective date |
2012-08-09 |
| EASA approval number |
|
| ATA Chapter |
57 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD 94-208-169(B)R2 dated 08 October 1997.
|
| Publication(s) and related information |
Airbus SB A300-57-6037 Original issue dated 01 August 1994, or Revision 1 dated 31 August 1995, or Revision 2 dated 9 January 2001, or Revision 3 dated 11 January 2002, or Revision 4 dated 24 February 2011.
Airbus SB A300-57-6039 Original issue dated 01 August 1994, or Revision 1 dated 26 October 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-044 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 14 May 2012 as PAD 12-044 for consultation until 11 June 2012. 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.
|
