| Number |
2026-0101 |
| Issued by |
 Europe |
| Issue date |
2026-05-26 |
| Effective date |
2026-06-09 |
| EASA approval number |
|
| ATA Chapter |
04 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B2
-
AS 350 B3
-
EC 130 B4
-
EC 130 T2
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2025-0137 dated 27 June 2025, including its Correction dated 29 October 2025.
|
| Publication(s) and related information |
AH AS 350 B2 AMM Chapter 04, ALS Revision 019 dated 19 December 2025.
AH AS 350 B3 AMM Chapter 04, ALS Revision 019 dated 19 December 2025.
AH EC 130 B4 AMM Chapter 04, ALS Revision 017 dated 19 December 2025.
AH EC 130 T2 AMM Chapter 04, ALS Revision 015 dated 19 December 2025.
AH ASB AS350-62-00-0001 original issue dated 19 May 2025.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
26-054 |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 23 April 2026 as PAD 26-054 for consultation until 21 May 2026. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
