| Number |
2024-0139 |
| Issued by |
 Europe |
| Issue date |
2024-07-12 |
| Effective date |
2024-07-26 |
| EASA approval number |
|
| ATA Chapter |
11, 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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2023-0089 dated 04 May 2023.
|
| 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, and Revision 5 dated 09 July 2024.
AH ASB AS355-55.00.18 original issue dated 07 December 2023 and Revision 1 dated 06 June 2024.
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 and Revision 05 dated 09 July 2024.
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 09 August 2024. No comments were received during the consultation period.
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.
|
