| Number |
2023-0187R1 |
| Issued by |
 Europe |
| Issue date |
2025-03-20 |
| Effective date |
2025-03-27 |
| EASA approval number |
|
| ATA Chapter |
76 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B3
-
EC 130 B4
-
EC 130 T2
|
| Revision |
This AD revises EASA AD 2023-0187 dated 27 October 2023.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2023-0133 dated 05 July 2023.
|
| Publication(s) and related information |
Eurocopter AS350 Emergency ASB 05.00.61 and EC130 Emergency ASB 05A009 (published as single document) original issue dated 16 November 2009, or Revision 1 dated 22 November 2012, or Revision 2 dated 13 August 2013, or AH ASB 05.00.61 and EC130 Emergency ASB 05A009 Revision 3 dated 15 June 2015, or AH ASB 05.00.61 and EC130 Emergency ASB 05A009 Revision 4 dated 17 April 2023.
AH AS350 Emergency ASB 05.00.77 and EC130 Emergency ASB 05A014 (published as single document) original issue dated 03 February 2015, or Revision 1 dated 15 June 2015, or Revision 2 dated 17 April 2023.
Eurocopter ASB AS350-80.00.09 original issue dated 22 November 2012, and Revision 1 dated 13 August 2013.
Eurocopter ASB EC130-80A005 original issue dated 22 November 2012, and Revision 1 dated 13 August 2013.
AH ASB AS350-76.00.33 original issue dated 17 April 2023 and Revision 1 dated 25 October 2023.
AH ASB EC130-76A013 original issue dated 17 April 2023 and Revision 1 dated 25 October 2023.
The use of later approved revisions of the above-mentioned documents (that may be published by Airbus Helicopters, the current design approval holder) 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 27 October 2023 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.
|
