| Number |
2011-0145 |
| Issued by |
 Europe |
| Issue date |
2011-08-02 |
| Effective date |
2011-08-16 |
| EASA approval number |
|
| ATA Chapter |
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 2011-0117 dated 24 June 2011.
|
| 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 5 dated 25 July 2011,
Eurocopter ASB AS365 No. 05.00.61 Revision 1 dated 13 July 2011,
Eurocopter ASB SA366 No. 05.41 Revision 1 dated 13 July 2011,
Eurocopter ASB EC155 No. 05A022 Revision 1 dated 13 July 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 Safety Information
Section, Certification Directorate, EASA. E-mail: ADs[@]easa.europa[dot]eu.
|
