| Number |
2013-0001 |
| Issued by |
 Europe |
| Issue date |
2013-01-04 |
| Effective date |
2013-01-18 |
| EASA approval number |
|
| ATA Chapter |
75 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
RTM 322
-
RTM 322-01/9
-
RTM 322-01/9A
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2010-0203R1 dated 22 March 2011.
|
| Publication(s) and related information |
Rolls Royce Turboméca Emergency MSB SB SBP-M3-A-75-09-00-01A-A-A.
Rolls-Royce Turboméca MSB SB SBP-M3-A-75-09-00-02A-A-A.
Rolls-Royce Turboméca MSB SB SBP-M3-A-72-42-00-03A-A-A
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
12-149 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 26 November 2012 as PAD 12-149 for consultation until 24 December 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.
|
