| Number |
2023-0064 |
| Issued by |
 Europe |
| Issue date |
2023-03-20 |
| Effective date |
2023-04-03 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
62 |
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
-
EC 130 B4
-
EC 130 T2
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 C1
-
SA 365 C2
-
SA 365 C3
-
SA 365 N
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0048 dated 16 February 2021.
|
| Publication(s) and related information |
AH ASB AS350-05.01.01 original issue dated 09 February 2021, or Revision 1 dated 15 March 2023.
AH ASB EC130-05A037 original issue dated 09 February 2021, or Revision 1 dated 15 March 2023.
AH ASB AS355-05.00.85 original issue dated 09 February 2021, or Revision 1 dated 24 March 2021,
or Revision 2 dated 15 March 2023.
AH ASB SA365-05.34 original issue dated 09 February 2021, or Revision 1 dated 15 March 2023.
AH ASB AS365-05.00.82 original issue dated 09 February 2021, or Revision 1 dated 15 March 2023.
AH SB AS350-62.00.46 original issue dated 15 March 2023.
AH SB AS355-62.00.41 original issue dated 15 March 2023.
AH SB EC130-62-020 original issue dated 15 March 2023.
AH SB AS365-62.00.28 original issue dated 15 March 2023.
AH SB SA365-62.01 original issue dated 15 March 2023.
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.
|
