| Number |
2010-0100R1 |
| Issued by |
 Europe |
| Issue date |
2010-08-11 |
| Effective date |
2010-08-18 |
| EASA approval number |
|
| ATA Chapter |
34 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
SA 365 N1
|
| Revision |
This AD revises EASA Emergency AD 2010-0100-E dated 26 May 2010, which
superseded EASA AD 2009-0241-E dated 05 November 2009 and its correction
dated 10 December 2009.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter AS365 ASB No.01.00.61 Revision 3 dated 28 July 2010.
Eurocopter AS365 ASB No.34.00.31 Revision 1 dated 28 July 2010.
The use of later approved revisions of these 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. 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 Airworthiness
Directives, Safety Management & Research Section, Certification
Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|
