| Number |
2011-0105 |
| Issued by |
 Europe |
| Issue date |
2011-05-31 |
| Effective date |
2011-06-14 |
| EASA approval number |
|
| ATA Chapter |
05, 65 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2009-0247 dated 13 November 2009.
|
| Publication(s) and related information |
Eurocopter ASB AS365 No. 05.00.54 Revision 4 dated 16 May 2011,
Eurocopter ASB SA366 No. 05.37 Revision 4 dated 16 May 2011,
Eurocopter ASB EC155 No. 05A015 Revision 4 dated 16 May 2011,
Eurocopter ASB AS365 No. 05.00.61 Original issue dated 16 May 2011,
Eurocopter ASB SA366 No. 05.41 Original issue dated 16 May 2011,
Eurocopter ASB EC155 No. 05A022 Original issue dated 16 May 2011,
Eurocopter SB AS365 No. 65.00.17 Revision 1 dated 21 March 2011,
Eurocopter SB SA366 No. 65.04 Revision 1 dated 21 March 2011, and
Eurocopter SB EC155 No. 65-006 Revision 1 dated 21 March 2011.
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.
|
