| Number |
2022-0051 |
| Issued by |
 Europe |
| Issue date |
2022-06-09 |
| Effective date |
2022-04-05 |
| EASA approval number |
|
| ATA Chapter |
53 |
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 |
Not applicable
|
| Correction |
This AD is re-published to correct typos in the referenced AD numbers in the Reason section.
|
| Supersedure |
This AD supersedes EASA AD 2014-0076R3 dated 30 November 2021.
|
| Publication(s) and related information |
AH AS350 Emergency ASB No. 05.00.70 dated 24 March 2014, or Revision 1 dated 27 July 2020 or Revision 2 dated 24 November 2021.
AH AS355 Emergency ASB No. 05.00.62 dated 24 March 2014, or Revision 1 dated 27 July 2020, or Revision 2 dated 24 November 2021, or Revision 3 dated 18 March 2022.
AH AS350 SB No. 53.00.58 Revision 1 dated 27 July 2020.
AH AS355 SB No. 53.00.34 dated 27 July 2020.
The use of later approved revisions of these 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.
|
