Number |
2017-0007 |
Issued by |
Europe |
Issue date |
2017-01-13 |
Effective date |
2017-01-27 |
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 2016-0097R1 dated 25 May 2016.
|
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 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016.
Airbus Helicopters ASB SA366-01.29 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016.
Airbus Helicopters ASB EC155-04A014 original issue dated 4 May 2016, or Revision 1 dated 03 June 2016, or Revision 2 dated 28 October 2016.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD. |
PAD number |
16-167 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 December 2016 as PAD 16-167 for consultation until 04 January 2017. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
|