| Number |
2025-0079 |
| Issued by |
 Europe |
| Issue date |
2025-04-10 |
| Effective date |
2025-04-24 |
| EASA approval number |
|
| ATA Chapter |
05 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 2
-
ARRIEL 2D
-
ARRIEL 2E
-
ARRIEL 2H
-
ARRIEL 2L2
-
ARRIEL 2N
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2022-0083 dated 11 May 2022.
|
| Publication(s) and related information |
SAFRAN ARRIEL 2 Chapter 05-10 Overhaul Manual X292 R1 500 2, up to update 29 dated 30 December 2024.
SAFRAN ARRIEL 2D Chapter 05-10 MM X292 R1 450 2, up to update 29 dated 30 December 2024.
SAFRAN ARRIEL 2E Chapter 05-10 MM X292 R2 300 2, up to update 25 dated 30 December 2024.
SAFRAN ARRIEL 2H Chapter 05-10 MM X292 2H 450 2, up to update 14 dated 30 December 2024.
SAFRAN ARRIEL 2L2 Chapter 05-10 MM X292 2L 450 2, up to update 7 dated 30 December 2024.
SAFRAN ARRIEL 2N Chapter 05-10 MM X292 N2 450 2, up to update 20 dated 30 December 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-045 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 12 March 2025 as PAD 25-045 for consultation until 09 April 2025. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
