| Number |
2018-0140R1 |
| Issued by |
 Europe |
| Issue date |
2024-02-14 |
| Effective date |
2024-02-28 |
| EASA approval number |
|
| ATA Chapter |
25, 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
-
AS 332 L2
-
EC 225 LP
|
| Revision |
This AD revises EASA Emergency AD 2018-0140-E dated 29 June 2018.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AH AS 332 ASB 01.00.89 and EC 225 ASB 04A014 (single document), original issue dated 07 June 2018 and Revision 1 dated 28 June 2018, Revision 2 dated 21 January 2021, or Revision 3 dated 02 November 2023.
AH SB AS332-52.00.43 original issue dated 23 June 2015.
AH SB EC225-52-008 original issue dated 23 June 2015.
AH SB AS332-25.03.90 original issue dated 02 November 2023.
AH AS332-25.03.89 original issue dated 02 November 2023.
AH AS332-25.03.88 original issue dated 02 November 2023.
AH EC225-25A277 original issue dated 02 November 2023.
AH EC225-25A278 original issue dated 02 November 2023.
The use of later approved revisions of 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, EASA have decided to issue a 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.
|
