| Number |
2014-0204 |
| Issued by |
 Europe |
| Issue date |
2014-09-12 |
| Effective date |
2014-09-25 |
| EASA approval number |
|
| ATA Chapter |
11 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C1
-
AS 332 L1
-
AS 332 L2
-
EC 225 LP
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
|
| Revision |
Not applicable
|
| Correction |
This AD is re-published to correct the AD number in the header of the document.
|
| Supersedure |
None
|
| Publication(s) and related information |
Airbus Helicopters ASB AS332-01.00.85 original issue, dated 26 August 2014,
Airbus Helicopters ASB EC225-04A012 original issue, dated 26 August 2014,
Airbus Helicopters ASB AS365-01.00.66 original issue, dated 26 August 2014,
Airbus Helicopters ASB EC155-04A013 original issue, dated 26 August 2014.
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. Based on the required actions and the compliance time, EASA have
decided to issue a Final AD with Request for Comments, postponing the
public consultation process until after publication.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail: ADs[at]easa.europa.eu.
|
