| Number |
2020-0033R1 |
| Issued by |
 Europe |
| Issue date |
2021-12-10 |
| Effective date |
2021-12-17 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIUS 2
-
ARRIUS 2B1
-
ARRIUS 2B1A
-
ARRIUS 2B2
-
ARRIUS 2G1
-
ARRIUS 2K1
-
ARRIUS 2K2
|
| Revision |
This AD revises EASA AD 2020-0033 dated 25 February 2020, which superseded EASA AD 2013-0082 dated 02 April 2013.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Turbomeca MSB 319 73 2825 version G dated 24 January 2013, or version H dated 01 September 2014, or version I dated 26 April 2016; and SAFRAN MSB 319 73 2825 version J dated 15 March 2019 or version K dated 16 November 2021.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-014 |
| 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 22 January 2020 as PAD 20-104 for consultation until 19 February 2020. 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.
|
