| Number |
2011-0204R1 |
| Issued by |
 Europe |
| Issue date |
2013-03-20 |
| Effective date |
2013-03-27 |
| EASA approval number |
|
| ATA Chapter |
29 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA AD 2011-0204 dated 14 October 2011.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus SB A330-29-3114 original issue dated 18 May 2011.
Airbus SB A340-29-4089 original issue dated 18 May 2011.
Airbus SB A340-29-5018 original issue dated 18 May 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Hamilton Sundstrand SB No. ERPS06M-29-18 original issue dated 08 March 2011 or Revision 1 dated 26 August 2011 or Revision 2 dated 10 February 2012.
Hamilton Sundstrand SB No. ERPS33T-29-5, original issue dated 08 March 2011 or Revision 1 dated 30 November 2011 or Revision 2 dated 19 June 2012. |
| PAD number |
11-095 |
| 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 September 2011 as PAD 11-095 for consultation until 11 October 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.
|
