| Number |
2009-0112R1 |
| Issued by |
 Europe |
| Issue date |
2009-07-30 |
| Effective date |
2009-06-01 |
| EASA approval number |
|
| ATA Chapter |
72 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 1
-
ARRIEL 1B
-
ARRIEL 1D
-
ARRIEL 1D1
-
ARRIEL 2
-
ARRIEL 2B
-
ARRIEL 2B1
-
ARRIEL 2B1A
|
| Revision |
This AD revises EASA AD 2009-0112, dated 18 May 2009.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2009-0068-E, dated 25 March 2009.
|
| Publication(s) and related information |
Turboméca MSB A292 72 0827 - version C; and MSB A292 72 2833 - version C, both dated 15 July 2009. The use of later approved revisions of these documents 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 [dot] europa.eu.
|
