| Number |
2026-0202R1 |
| Issued by |
 Europe |
| Issue date |
2026-11-06 |
| Effective date |
2026-11-09 |
| EASA approval number |
|
| ATA Chapter |
55 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
|
| Revision |
This AD revises EASA AD 2026-0202 dated 26 October 2026.
|
| Correction |
Not applicable
|
| Supersedure |
This original issue of this AD superseded EASA AD 2024-0139 dated 12 July 2024.
|
| Publication(s) and related information |
AH AS355 ASB 05.00.76 original issue dated 27 June 2017, Revision 1 dated 22 July 2020, Revision 2 dated 04 March 2021, Revision 3 dated 06 April 2023, Revision 4 dated 02 May 2023, Revision 5 dated 09 July 2024, and Revision 6 dated 19 October 2026.
AH ASB AS355-55.00.18 original issue dated 07 December 2023, Revision 1 dated 06 June 2024, Revision 02 dated 28 April 2025, Revision 03 dated 18 December 2025 and Revision 04 dated 22 October 2026.
AH AS350 ASB 05.00.90 original issue dated 27 June 2017, Revision 1 dated 22 July 2020, Revision 2 dated 04 March 2021, Revision 3 dated 06 April 2023, Revision 4 dated 02 May 2023, Revision 5 dated 09 July 2024 and Revision 6 dated 19 October 2026.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. All interested persons may send their comments, referencing the AD Number, to the E-mail address specified in below Remark 3, prior to 23 November 2026. A Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file, attached to the record for this AD.
Only if any further comment is received during the consultation period, an additional Comment Response Document will be published in the EASA Safety Publications Tool, in a 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.
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