| Number |
2020-0021 |
| Issued by |
 Europe |
| Issue date |
2020-02-06 |
| Effective date |
2020-02-20 |
| EASA approval number |
|
| ATA Chapter |
64 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA 330 / AS 332 / EC 225
-
AS 332 C
-
AS 332 C1
-
AS 332 L
-
AS 332 L1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes DGAC France AD F-2004-031 R1 (EASA approval 2005-2582) dated 30 March 2005.
|
| Publication(s) and related information |
AH AS 332 ASB 64.00.31 original issue dated 07 March 2005, or Revision 1 dated 20 January 2014.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
20-001 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 07 January 2020 as PAD 20-001 for consultation until 04 February 2020. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD.
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.
|
