Number |
2024-0207R1 |
Issued by |
Europe |
Issue date |
2024-12-12 |
Effective date |
2024-12-18 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
72 |
Approval Holder / Type Designation |
-
SAFRAN HELICOPTER ENGINES
-
ARRIEL 1
-
ARRIEL 1A1
-
ARRIEL 1A2
-
ARRIEL 1B
-
ARRIEL 1C
-
ARRIEL 1C1
-
ARRIEL 1C2
-
ARRIEL 1D
-
ARRIEL 1D1
-
ARRIEL 1E2
-
ARRIEL 1K
-
ARRIEL 1K1
-
ARRIEL 1S
-
ARRIEL 1S1
|
Revision |
This AD revises EASA AD 2024-0207 dated 24 October 2024, including its Correction dated 12 November 2024.
|
Correction |
This AD is republished to correct a typographical error in the effective date.
|
Supersedure |
None
|
Publication(s) and related information |
SAFRAN SB 292 72 0867 version A dated 14 October 2024, or version B dated 09 December 2024.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. Based on the required actions and the compliance time, the original issue of this AD was posted on 24 October 2024 as Final AD with Request for Comments, postponing the public consultation process until 21 November 2024. 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.
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