| Number |
2017-0061 |
| Issued by |
Europe |
| Issue date |
2017-04-07 |
| Effective date |
2017-04-21 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder / Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2015-0064R1 dated 29 July 2015.
|
| Publication(s) and related information |
Turbomeca MSB 292 72 0842 version A dated 20 March 2015, or version B dated 08 July 2015, or SAFRAN Helicopter Engines version C dated 03 January 2017.
The use of later approved revisions of this document is acceptable for compliance with the
requirements of this AD. |
| PAD number |
17-015R1 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 26 January 2017 as PAD 17-015 for consultation until 23 February 2017 and republished on 07 March 2017 as PAD 17-015R1 for additional consultation until 05 April 2017. The Comment Response Documents can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|