| Number |
2012-0071 |
| Issued by |
 Europe |
| Issue date |
2012-04-26 |
| Effective date |
2012-05-10 |
| EASA approval number |
|
| Contributor |
EASA Propulsion Section |
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 1
-
ARRIEL 1A1
-
ARRIEL 1A2
-
ARRIEL 1B
-
ARRIEL 1C
-
ARRIEL 1C1
-
ARRIEL 1C2
-
ARRIEL 1D
-
ARRIEL 1D1
-
ARRIEL 1E2
-
ARRIEL 1K
-
ARRIEL 1K1
-
ARRIEL 1S
-
ARRIEL 1S1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD 1990-064(A) R1 dated 21 March 2001.
|
| Publication(s) and related information |
Turboméca MSB A292 72 0230 Version C dated 29 February 2012.
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD. |
| PAD number |
12-021 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 23 March 2012 as PAD 12-021 for consultation
until 20 April 2012. 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[dot]eu.
|
