| Number |
2012-0108R1 |
| Issued by |
 Europe |
| Issue date |
2019-09-19 |
| Effective date |
2019-10-03 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 N
-
SA 365 N1
|
| Revision |
This AD revises EASA Emergency AD 2012-0108-E dated 15 June 2012.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter AS365 Emergency ASB 05.00.63 original issue dated 12 June 2012, or Revision 1 dated 18 June 2012, or AH AS365 Emergency ASB 05.00.63 Revision 2 dated 20 December 2018.
AH SB AS365-53.00.57 original issue dated 20 December 2018.
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, 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 Programming and Continued
Airworthiness 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.
|
