| Number |
2018-0039R1 |
| Issued by |
 Europe |
| Issue date |
2020-09-25 |
| Effective date |
2020-10-02 |
| EASA approval number |
|
| ATA Chapter |
56 |
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
|
| Revision |
This AD revises EASA AD 2018-0039 dated 09 February 2018.
|
| Correction |
The original issue of this AD was re-published to correct the model versus ASB reference in the definition of Group 2 helicopters.
|
| Supersedure |
The original issue of this AD superseded EASA AD 2016-0049 dated 10 March 2016.
|
| Publication(s) and related information |
AH ASB EC225-05A046 original issue dated 08 March 2016, or Revision 1 dated 08 February 2018, or Revision 2 dated 10 April 2019, or Revision 3 dated 10 February 2020.
AH ASB AS332-05.01.05 original issue dated 08 March 2016, or Revision 1 dated 08 February 2018, or Revision 2 dated 10 April 2019, or Revision 3 dated 10 February 2020, or Revision 4 dated 23 September 2020.
AH ASB EC225-56C012 original issue dated 08 February 2018.
AH ASB AS332-56.90.13 original issue dated 08 February 2018.
AH AS332-56.00.18 original issue dated 23 September 2020.
AH ASB AS332-56.00.20 original issue dated 23 September 2020.
AH ASB AS332-56.00.21 original issue dated 23 September 2020.
AH ASB AS332-56.00.16 original issue dated 10 February 2020.
AH ASB AS332-56.90.14 original issue dated 10 April 2019.
AH ASB EC225-56A013 original issue dated 10 April 2019, or Revision 1 dated 10 February 2020.
AH ASB EC225-56A015 original issue dated 10 February2020.
AH ASB EC225-56A016 original issue dated 10 February 2020.
AH ASB EC225-56A017 original issue dated 10 February 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[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. 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.
|
