| Number |
2014-0236R1 |
| Issued by |
 Europe |
| Issue date |
2018-06-28 |
| Effective date |
2018-06-28 |
| EASA approval number |
|
| ATA Chapter |
33 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
SA 365 N1
|
| Revision |
This AD revises EASA AD 2014-0236 dated 28 October 2014.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus Helicopters ASB AS365-33.00.25 original issue dated 23 September 2014, or Revision 1 dated 04 December 2015, or Revision 2 dated 18 June 2018.
Airbus Helicopters ASB EC155-33A013 original issue dated 23 September 2014, or Revision 1 dated 04 December 2015.
Airbus Helicopters AS365-33.00.26 original issue dated 06 December 2017, or Revision 1 dated 18 June 2018.
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.
|
