| Number |
2016-0004R1 |
| Issued by |
 Europe |
| Issue date |
2022-04-22 |
| Effective date |
2022-04-29 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
This AD revises EASA AD 2016-0004 dated 06 January 2016, including its Correction dated 05 February 2016.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2013-0079R1 dated 27 January 2014.
|
| Publication(s) and related information |
Turbomeca MSB A292 73 2847 Version A dated 29 May 2012, or Version B dated 06 March 2013, or Version C dated 03 December 2013, or Version D dated 24 June 2016, or Version E dated 14 April 2022.
Turbomeca MSB A292 73 2851 Version A dated 03 December 2013, or Version B dated 22 October 2015, or Version C dated 23 May 2019, or Version D dated 20 May 2021, or Version E dated 14 April 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
15-137 |
| 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 04 November 2015 as PAD 15-137 for consultation until 02 December 2015. The Comment Response Document can be found at https://ad.easa.europa.eu.
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.
|
