| Number |
2021-0196 |
| Issued by |
 Europe |
| Issue date |
2021-08-23 |
| Effective date |
2021-09-06 |
| EASA approval number |
|
| ATA Chapter |
11 |
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 |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0003 dated 06 January 2021.
|
| Publication(s) and related information |
AH ASB AS332-11.00.06 original issue dated 09 September 2020, or Rev. 1 dated 08 January 2021, or Rev. 2 dated 22 July 2021.
AH ASB EC225-11A002 original issue dated 09 September 2020, or Rev. 1 dated 08 January 2021, or Rev. 2 dated 22 July 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
21-107 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. This AD was posted on 23 July 2021 as PAD 21-107 for consultation until 20 August 2021. 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.
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.
|
