| Number |
2024-0148 |
| Issued by |
 Europe |
| Issue date |
2024-07-30 |
| Effective date |
2024-08-13 |
| EASA approval number |
|
| 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. |
| PAD number |
24-072 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 27 June 2024 as PAD 24-072 for consultation until 25 July 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.
|
