| Number |
2020-0287 |
| Issued by |
 Europe |
| Issue date |
2020-12-21 |
| Effective date |
2021-01-04 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| 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 C1
-
SA 365 C2
-
SA 365 C3
-
SA 365 N
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2020-0212 dated 05 October 2020.
|
| Publication(s) and related information |
AH ASB AS365-63.00.18 original issue dated 09 July 2014, or Revision 1 dated 07 March 2016, or Revision 2 dated 31 January 2019, or Revision 3 dated 22 July 2020.
AH ASB SA365-65.50 original issue dated 09 July 2014, or Revision 1 dated 07 March 2016, or Revision 2 dated 22 July 2020.
AH ASB EC155-63A012 Revision 1 dated 21 July 2014, or Revision 2 dated 07 March 2016.
AH ASB AS365-63.00.19 original issue dated 22 January 2018, or Revision 1 dated 31 January 2019.
AH ASB EC155-63A013 original issue dated 22 January 2018, or Revision 1 dated 31 January 2019.
AH ASB SA365-65.52 original issue dated 22 January 2018, or Revision 1 dated 22 July 2020.
AH ASB AS365-63.00.26 original issue dated 22 July 2020.
The use of later approved revisions of the above-mentioned 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@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. This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. Such components may be installed under an FAA Parts Manufacturer Approval (PMA), Supplemental Type Certificate (STC) or other modification.
|
