| Number |
2017-0102R2 |
| Issued by |
 Europe |
| Issue date |
2022-08-29 |
| Effective date |
2022-09-05 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 2
-
ARRIEL 2B
-
ARRIEL 2B1
-
ARRIEL 2B1A
|
| Revision |
This AD revises EASA AD 2017-0102R1 dated 16 February 2022.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2010-0215R1 dated 26 January 2016.
|
| Publication(s) and related information |
Turbomeca MSB A292 73 2830 Version B dated 10 July 2009, or SAFRAN MSBA292 73 2830 Version C dated 05 April 2017.
Turbomeca MSB A292 73 2836 Version A dated 17 August 2010, or SAFRAN MSB A292 73 2836 Version B dated 05 April 2017.
Turbomeca MSB 292 73 2178 Version A dated 01 April 2015, or SAFRAN MSB 292 73 2178 Version B dated 23 March 2017, or Version C dated 19 October 2018, or Version D dated 08 February 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
17-057 |
| 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 May 2017 as PAD 17-057 for consultation until 31 May 2017. 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.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
|
