Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
26-056 |
| Issued by |
 Europe |
| Issue date |
2026-04-23 |
| EASA approval number |
|
| ATA Chapter |
04 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0134 dated 10 July 2024.
|
| Publication(s) and related information |
AH AS 355 E AMM Chapter 04 ALS Revision 014 dated 17 October 2025.
AH AS 355 F AMM Chapter 04 ALS Revision 014 dated 17 October 2025.
AH AS 355 F1 AMM Chapter 04 ALS Revision 014 dated 17 October 2025.
AH AS 355 F2 AMM Chapter 04 ALS Revision 015 dated 17 October 2025.
AH AS 355 N AMM Chapter 04 ALS Revision 014 dated 17 October 2025.
AH AS 355 NP AMM Chapter 04 ALS Revision 013 dated 17 October 2025.
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 21 May 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.
|
