| Number |
2021-0012R1 |
| Issued by |
 Europe |
| Issue date |
2023-02-25 |
| Effective date |
2023-02-25 |
| EASA approval number |
|
| ATA Chapter |
56 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
AS 332 L1
-
AS 332 L2
-
EC 225 LP
|
| Revision |
This AD revises EASA AD 2021-0012 dated 11 January 2021.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AH ASB AS332-56.00.16 original issue dated 10 February 2020.
AH ASB AS332-56.00.18 original issue dated 23 September 2020, or Revision 1 dated 28 April 2021, or Revision 2 dated 03 March 2022, or Revision 3 dated 24 February 2023.
AH ASB AS332-56.00.20 original issue dated 23 September 2020, or Revision 1 dated 03 March 2022, or Revision 2 dated 24 February 2023.
AH ASB AS332-56.00.21 original issue dated 23 September 2020, or Revision 1 dated 03 March 2022, or Revision 2 dated 24 February 2023.
AH ASB AS332-56.90.14 original issue dated 10 April 2019.
AH ASB EC225-56A013 Revision 1 dated 10 February 2020.
AH ASB EC225-56A015 original issue dated 10 February 2020.
AH ASB EC225-56A016 original issue dated 10 February 2020.
AH ASB EC225-56A017 original issue dated 10 February 2020.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-146 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.The original issue of this AD was posted on 25 September 2020 as PAD 20-146 for consultation until 23 October 2020. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
