Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
24-082R1 |
| Issued by |
 Europe |
| Issue date |
2024-09-27 |
| EASA approval number |
|
| Contributor |
EASA Environment & Propulsion Systems Department |
| ATA Chapter |
73 |
Approval Holder
/ Type Designation |
-
SAFRAN HELICOPTER ENGINES
|
| Revision |
This PAD is revised to include reference to mod TU 173 and EECU software upgrade.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
SAFRAN MSB 319 73 2867 version B dated 05 July 2024 and version C dated 19 August 2024.
SAFRAN MSB 319 73 2868 version A dated 05 July 2024.
SAFRAN MSB 319 73 2173 version A dated 13 August 2024, including ERRATUM dated 10 September 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 11 October 2024.
2. The original issue of this PAD was posted on 11 July 2024 for consultation until 08 August 2024. No comments were received during the consultation period.
3. Enquiries regarding this PAD 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 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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