| Number |
2021-0171R1 |
| Issued by |
 Europe |
| Issue date |
2024-07-01 |
| Effective date |
2024-07-08 |
| EASA approval number |
|
| ATA Chapter |
65 |
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 N1
|
| Revision |
This AD revises EASA AD 2021-0171 dated 19 July 2021.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2017-0125 dated 21 July 2017.
|
| Publication(s) and related information |
Eurocopter AS365 SB 65.00.17 Revision 1 dated 23 February 2011.
Eurocopter EC155 SB 65-006 Revision 1 dated 23 February 2011.
Airbus Helicopters ASB AS365-01.00.67 original issue dated 04 May 2016, or Revision 1 dated
03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 2017, or Revision 4 dated 11 December 2019, or Revision 5 dated 25 March 2020, or Revision 6 dated 14 June 2021, or Revision 7 dated 22 September 2021, or Revision 8 dated 10 June 2024.
Airbus Helicopters ASB EC155-04A014 original issue dated 04 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 2017, or Revision 4 dated 11 December 2019, or Revision 5 dated 25 March 2020, or Revision 6 dated 14 June 2021, or Revision 7 dated 22 September 2021, or Revision 8 dated 10 June 2024.
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, the original issue of this AD was posted on 19 July 2021 as 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.
|
