Number |
2017-0089R1 |
Issued by |
Europe |
Issue date |
2020-06-23 |
Effective date |
2020-06-30 |
EASA approval number |
|
Contributor |
EASA VTOL Department |
ATA Chapter |
62 |
Approval Holder / Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 B3
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
-
EC 130 B4
-
EC 130 T2
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
|
Revision |
This AD revises EASA AD 2017-0089 dated 17 May 2017.
|
Correction |
Not applicable
|
Supersedure |
None
|
Publication(s) and related information |
Airbus Helicopters EASB AS350-62.00.39 original issue dated 15 May 2017, or Revision 01 dated 19 May 2017, or Revision 02 dated 25 June 2019.
Airbus Helicopters EASB AS355-62.00.36 original issue dated 15 May 2017, or Revision 01 dated 19 May 2017, or Revision 02 dated 25 June 2019.
Airbus Helicopters EASB EC130-62A015 original issue dated 15 May 2017, or Revision 01 dated 19 May 2017, or Revision 02 dated 25 June 2019.
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 Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.
|