Number |
2017-0125 |
Issued by |
Europe |
Issue date |
2017-07-21 |
Effective date |
2017-07-28 |
EASA approval number |
|
Contributor |
EASA Rotorcraft Section |
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 2017-0007 dated 13 January 2017.
|
Publication(s) and related information |
Eurocopter AS365 SB 65.00.17 Revision 1 dated 23 February 2011.
Eurocopter SA366 SB 65.04 Revision 1 dated 23 February 2011.
Eurocopter EC155 SB 65-006 Revision 1 dated 23 February 2011.
Airbus Helicopters ASB AS365-01.00.67 original issue dated 04 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 2017.
Airbus Helicopters ASB SA366-01.29 original issue dated 04 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 2017.
Airbus Helicopters ASB EC155-04A014 original issue dated 04 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016, or Revision 3 dated 20 July 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.
|