| Number |
2009-0246 |
| Issued by |
 Europe |
| Issue date |
2009-11-10 |
| Effective date |
2009-11-24 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2007-0026 dated 1 February 2007 which
superseded DGAC AD (CN) F-2004-139 (EASA Approval number 2004-8594)
dated 18 August 2004.
|
| Publication(s) and related information |
Turboméca Mandatory Service Bulletin n° A292 73 2814 version D dated 16
October 2009.
The use of later approved updates of this document is acceptable for
compliance with the requirement of this AD.
Eurocopter AS 350 B3 Flight Manual: section 8, chapter “Check after engine
or module replacement – Manual Emergency” – Sheet n° 3C. |
| 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 Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail ADs@easa.europa.eu
4. For any question concerning the technical content of the requirements in
this AD, please contact:
TURBOMÉCA S.A.
ARRIEL 2 Customer Support
40220 Tarnos, France
Fax: +33 5 59 74 45 15, or your usual or nearest TURBOMÉCA
technical representative (refer to http://www.turbomeca-support.com)
|
