Number |
2013-0120 |
Issued by |
Europe |
Issue date |
2013-06-04 |
Effective date |
2013-06-18 |
EASA approval number |
|
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 |
None
|
Publication(s) and related information |
Turbomeca MSB A292 72 0838 version A dated 24 May 2013.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The required actions and the risk allowance have granted the issuance of a Final AD with Request for Comments, postponing the public consultation process after publication.
3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa[dot]eu.
|