| Number |
2022-0005 |
| Issued by |
 Europe |
| Issue date |
2022-01-11 |
| Effective date |
2022-01-25 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
SAFRAN Arrius 1A1 Maintenance Manual, reference X 319 U1 451 2, update no. 17, Chapter 05-10 approved on 24 March 2021 (Major Change 10075940).
SAFRAN Arrius 1A1 Overhaul Manual, reference X 319 U1 500 2, update no. 21, Chapter 05-10 approved on 24 March 2021 (Major Change 10075940).
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-175 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 01 December 2021 as PAD 21-175 for consultation until 29 December 2021. 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.
|
