| Number |
2024-0018 |
| Issued by |
 Europe |
| Issue date |
2024-01-11 |
| Effective date |
2024-01-25 |
| EASA approval number |
|
| ATA Chapter |
31 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B2
-
AS 350 B3
-
EC 130 B4
-
EC 120 B
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0168 dated 16 July 2021.
|
| Publication(s) and related information |
AH ASB EC130-05A036 original issue dated 31 March 2021, or Revision 1 dated 25 October 2023.
AH ASB No. AS350-05.01.00 original issue dated 31 March 2021, or Revision 1 dated 25 October
2023.
AH ASB EC120-05A023 original issue dated 31 March 2021, or Revision 1 dated 25 October 2023.
AH ASB EC130-25A158 original issue dated 25 October 2023.
AH ASB AS350-25.04.87 original issue dated 25 October 2023.
AH ASB EC120-25A031 original issue dated 25 October 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
23-125 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 17 November 2023 as PAD 23-125 for consultation until 15 December 2023. No comments were received during the consultation period.
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.
|
