| Number |
2011-0182R1 |
| Issued by |
 Europe |
| Issue date |
2012-02-03 |
| Effective date |
2012-02-06 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
This AD is revised to address the engines that were already inspected and
corrected in accordance with the instructions of Turbomeca Mandatory
Service Bulletin (MSB) N° 319 75 4810 issue A.
|
| Correction |
Not applicable
|
| Supersedure |
This AD revises EASA AD 2011-0182 dated 22 September 2011. EASA AD
2011-0182 superseded EASA AD 2008-0134R1 dated 17 February 2009.
|
| Publication(s) and related information |
TURBOMECA Mandatory Service Bulletin N°. 319 75 4810 issue B, dated
25 January 2011.
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD. |
| PAD number |
11-076 |
| 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 22 July 2011 as PAD
11-076 for consultation until 19 August 2011. The Comment
Response Document can be found at https://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety
Information Section, Certification Directorate, EASA.
E-mail: ADs[at]easa.europa.eu.
|
