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ADs [at] easa.europa [dot] eu
|
Number |
24-072 |
Issued by |
Europe |
Issue date |
2024-06-27 |
EASA approval number |
|
Contributor |
EASA Environment & Propulsion Systems Department |
ATA Chapter |
05 |
Approval Holder / Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes DGAC France AD F-2005-063R1 dated 25 May 2005 and EASA
AD 2008-0133 dated 17 July 2008.
|
Publication(s) and related information |
SAFRAN Arrius 1A MM, reference X 319 D6 300 1, update no. 33 (French version), and reference X 319 D6 300 2, update no. 34 (English version), both dated 30 March 2024.
SAFRAN Arrius 1A OM, reference X 319 H6 500 1, update no. 35 (French version), and reference X 319 H6 500 2, update no. 35 (English version), both dated 06 May 2024.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
Remarks |
1. This Proposed AD will be closed for consultation on 25 July 2024.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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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