| Number |
2012-0067 |
| Issued by |
 Europe |
| Issue date |
2012-04-24 |
| Effective date |
2012-05-08 |
| EASA approval number |
|
| ATA Chapter |
64 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD F-2004-116 (EASA approval 2004-7515)
dated 21 July 2004.
|
| Publication(s) and related information |
Eurocopter AS 365 ASB No. 05.00.17 Revision 2 dated 16 April 2012.
The use of later approved revisions of this document 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. The required actions and the risk allowance have granted the issuance of a
Final AD with Request for Comments, postponing the public consultation
process after publication.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa[dot]eu.
|
