| Number |
2014-0036 |
| Issued by |
 Europe |
| Issue date |
2014-02-11 |
| Effective date |
2014-02-25 |
| 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
-
ARRIEL 2
-
ARRIEL 2B
-
ARRIEL 2B1
-
ARRIEL 2B1A
-
ARRIEL 2B1B
-
ARRIEL 2C
-
ARRIEL 2C1
-
ARRIEL 2C2
-
ARRIEL 2S1
-
ARRIEL 2S2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Turbomeca MSB 292 72 0839 version B dated 25 November 2013.
Turbomeca MSB 292 72 2849 version B dated 25 November 2013.
Turbomeca Technical Instruction (TI) X 292 72 0839 update 1.
Turbomeca TI X 292 72 2849 update 1.
Turbomeca TI X 292 72 0840 original issue.
Turbomeca TI X 292 72 2850 original issue.
Turbomeca Internal Directive (ID) 383952 version C.
Turbomeca Repair Technical Directive (RTD) X 292 65 327 2.
Turbomeca Engine Test Bed Acceptance Test Specifications (CCT) as listed in Appendix 2 of this AD.
Turbomeca Maintenance Manuals (MM) as listed in Appendix 3 of this AD.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
14-007 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 09 January 2014 as PAD 14-007 for consultation until 06 February 2014. 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.eu.
|
