Number |
2017-0226 |
Issued by |
Europe |
Issue date |
2017-11-17 |
Effective date |
2017-12-01 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
ATA Chapter |
11 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
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 |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2014-0204 dated 11 September 2014, including its Correction dated 12 September 2014.
|
Publication(s) and related information |
Airbus Helicopters ASB AS332-01.00.85 original issue dated 26 August 2014, or Revision 01 dated 07 September 2017.
Airbus Helicopters ASB EC225-04A012 original issue dated 26 August 2014, or Revision 01 dated 07 September 2017.
Airbus Helicopters ASB AS332-25.03.16 original issue dated 07 September 2017.
Airbus Helicopters ASB AS332-25.03.41 original issue dated 07 September 2017.
Airbus Helicopters ASB AS332-25.03.42 original issue dated 07 September 2017.
Airbus Helicopters ASB EC225-25A179 original issue dated 07 September 2017.
Airbus Helicopters ASB EC225-25A203 original issue dated 07 September 2017.
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 EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|