| Number |
2008-0024R1 |
| Issued by |
 Europe |
| Issue date |
2009-10-22 |
| Effective date |
2008-11-05 |
| EASA approval number |
|
| ATA Chapter |
04 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
This AD revises EASA AD 2008-0024 dated 12 February 2008.
AD 2008-0024 Revision 1: 05 November 2009
AD 2008-0024 Original Issue: 26 February 2008
|
| Correction |
N/A
|
| Supersedure |
None
|
| Publication(s) and related information |
Rolls-Royce Turbomeca Emergency Mandatory Service Bulletin EMSBPM3-
A-04-30-00-01A-A-A Issue 002
The use of later approved revisions of this document is acceptable for
compliance with the requirements of this AD.
RTM322-01/9 Engine Base Maintenance Manual M3-A-EBM-00-D, data
module DM M3-04-30-72-42A-000A-A |
| PAD number |
08-001 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. The original AD was posted on 11 January as PAD 08-001 for
consultation until 08 February 2008. No comments were received during
this period.
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:
Rolls-Royce plc, PO Box 3, Filton, Bristol, BS34 7QE, England.
Telephone: +44 (0) 117 97 90700; Fax: +44 (0) 117 97 95498
|
