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ADs [at] easa.europa [dot] eu
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| Number |
26-072 |
| Issued by |
 Europe |
| Issue date |
2026-06-03 |
| EASA approval number |
|
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0195R1 dated 22 October 2024.
|
| Publication(s) and related information |
SAFRAN MSB 319 73 2867 version B dated 05 July 2024 and version C dated 19 August 2024 and version D dated 28 July 2025 and version E dated 16 February 2026.
SAFRAN MSB 319 73 2868 version A dated 05 July 2024 and version B dated 28 July 2025 and version C dated 25 February 2026.
SAFRAN MSB 319 73 2173 version A dated 13 August 2024, including ERRATUM dated 10 September 2024 and version B dated 16 February 2026.
SAFRAN MSB 319 73 2172 version C dated 17 March 2026.
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 01 July 2026.
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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