Number |
2015-0090R1 |
Issued by |
Europe |
Issue date |
2020-06-16 |
Effective date |
2020-06-23 |
EASA approval number |
|
Contributor |
EASA Environment and Propulsion Systems Department |
ATA Chapter |
76 |
Approval Holder / Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
RTM 322
-
RTM 322-01/9
-
RTM 322-01/9A
|
Revision |
This AD revises EASA AD 2015-0090 dated 22 May 2015.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Turbomeca MSBP-M3-A-76-10-10-02A-A-A Issue 1 dated 24 March 2015.
SAFRAN SB M3-A-76-00-00-02A-A-A original issue dated 20 January 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
PAD number |
15-045 |
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 16 April 2015 as PAD 15-045 for consultation until 14 May 2015. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness 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.
|