| Number |
2009-0241-E |
| Issued by |
 Europe |
| Issue date |
2009-12-10 |
| Effective date |
2009-11-07 |
| 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 |
Not applicable
|
| Correction |
This AD correction is issued to correct an helicopter model in the AD applicability (it was AS365 N1, it is SA365 N1) and to clarify a statement in the Reason section of this AD.
|
| Supersedure |
This AD supersedes EASA AD 2008-0195-E dated 23 October 2008
|
| Publication(s) and related information |
Eurocopter EASB AS365 No. 01.00.61 Revision 1 dated 26 October 2009.
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 safety assessment has requested not to implement the full consultation
process and an immediate publication and notification.
3. Enquiries regarding this AD should be referred to the Airworthiness
Directives, Safety Management & Research Section, Certification Directorate,
EASA. E-mail: ADs@easa.europa.eu.
4. For any question concerning the technical content of the requirements in this
AD, please contact: EUROCOPTER (STDI) – Aéroport de Marseille Provence
13725 Marignane Cedex – France
Telephone +33 (0)4 42 85 97 97, Fax +33 (0)4 42 85 99 66
E-mail: Directive.technical-support@eurocopter.com.
|
