| Number |
2013-0170R1 |
| Issued by |
 Europe |
| Issue date |
2017-04-18 |
| Effective date |
2017-04-25 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 2
-
ARRIEL 2B
-
ARRIEL 2B1
-
ARRIEL 2B1A
-
ARRIEL 2B1B
-
ARRIEL 2C
-
ARRIEL 2C1
-
ARRIEL 2C2
-
ARRIEL 2S1
-
ARRIEL 2S2
|
| Revision |
This AD revises EASA AD 2013-0170 dated 30 July 2013, which superseded EASA AD 2007-0044 dated 21 February 2007.
|
| Correction |
Not applicable
|
| Supersedure |
This original issue of this AD superseded EASA AD 2007-0044 dated 21 February 2007.
|
| Publication(s) and related information |
Turbomeca MSB 292 73 2812 version G dated 24 June 2013, or SAFRAN Helicopter Engines MSB 292 73 2812 version H dated 28 February 2017.
Turbomeca MSB 292 73 2822 version F dated 21 June 2013, or SAFRAN Helicopter Engines MSB 292 73 2822 version G dated 28 February 2017.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
13-093 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 03 July 2013 as PAD 13-093 for consultation until 24 July 2013. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|
