| Number |
2021-0282R1 |
| Issued by |
 Europe |
| Issue date |
2025-01-08 |
| Effective date |
2024-07-17 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
64 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 B3
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
-
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 2021-0282 dated 17 December 2021.
|
| Correction |
This AD is republished to correct typographical errors in the numbers of the ADs mentioned in the Reason section, and to remove the word "repetitive" from the title of paragraphs (4) and (5).
|
| Supersedure |
None
|
| Publication(s) and related information |
AH ASB AS350-05.01.03 original issue dated 16 December 2021, or Revision 1 dated 08 July 2024.
AH ASB AS355-05.00.86 original issue dated 16 December 2021, or Revision 1 dated 08 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 after publication.
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.
|
