Number |
2021-0101R2 |
Issued by |
Europe |
Issue date |
2022-12-21 |
Effective date |
2022-12-28 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
52 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
-
SA 365 N
-
SA 365 N1
|
Revision |
This AD revises EASA AD 2021-0101R1 dated 25 February 2022.
|
Correction |
Not applicable
|
Supersedure |
The orginial issue of this AD superseded EASA AD 2021-0041 dated 28 January 2021.
|
Publication(s) and related information |
AH ASB AS365-52.00.29 original issue dated 10 February 2021 or Revision 01 dated 09 February 2022.
AH ASB AS365-52.00.27 original issue dated 17 November 2020 (including Erratum to
ASB AS365-52.00.27 original issue dated 21 January 2021), Revision 01 dated 04 June 2021, Revision 02 dated 17 October 2022 or Revision 03 dated 15 November 2022.
AH ASB EC155-52A033 original issue dated 30 September 2020.
AH SUP.10.4 NR7, date code 20-40 approved on 26 October 2020 (SA 365 N).
AH SUP.10.4 NR9, date code 20-40 approved on 26 October 2020 (SA 365 N1).
AH SUP.14 NR6, date code 20-40 approved on 26 October 2020 (AS 365 N2).
AH SUP.14 NR12, date code 20-28 approved on 08 September 2020 (AS 365 N3).
AH SUP.14 NR7, date code 20-11 approved on 01 April 2020 (EC 155 B).
AH SUP.14 NR8, date code 20-11 approved on 01 April 2020 (EC 155 B1).
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.
|