| Number |
2007-0288R1 |
| Issued by |
 Europe |
| Issue date |
2012-01-09 |
| Effective date |
2012-01-09 |
| EASA approval number |
|
| ATA Chapter |
05, 63 |
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 C1
-
SA 365 C2
-
SA 365 C3
-
SA 365 N
-
SA 365 N1
|
| Revision |
This AD revises EASA AD 2007-0288-E, dated 19 November 2007, which
superseded DGAC France AD F-2005-181 (EASA approval 2005-6390) and DGAC
France AD F-2005-182 (EASA approval 2005-6391).
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
Eurocopter AS365N ASB No. 05.00.48 Revision 4,
SA366 ASB No. 05.33 Revision 3,
SA365C ASB No. 05.26 Revision 3, and
EC155 ASB No. 05A007 Revision 3, all dated 08 December 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 accept 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.
|
