| Number |
2021-0139R1 |
| Issued by |
 Europe |
| Issue date |
2023-05-10 |
| Effective date |
2023-05-17 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
52 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
AS 332 L1
|
| Revision |
This AD revises EASA AD 2021-0139 dated 11 June 2021.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2019-0064R1 dated 19 December 2019.
|
| Publication(s) and related information |
Eurocopter AS 332 SB No. 52.00.28 original issue dated 15 December 1994, or Revision 1 dated 29 April 1998.
AH ASB AS332-52.00.56 original issue dated 30 January 2017, or Revision 1 dated 11 April 2019.
AH ASB AS332-52.00.59 original issue dated 19 December 2018, or Revision 1 dated 22 February 2019, or Revision 2 dated 21 June 2019, or Revision 3 dated 17 December 2019, or Revision 4 dated 05 May 2021, or Revision 5 dated 01 December 2022, or Revision 6 dated 04 May 2023.
Aerospatiale AS 332 SB No. 52.26 original issue dated 31 October 1991.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-069 |
| 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 10 May 2021 as PAD 21-069 for consultation until 07 June 2021. No comments were received during the consultation period.
2. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. 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.
|
