| Number |
2018-0248 |
| Issued by |
 Europe |
| Issue date |
2018-11-15 |
| Effective date |
2018-11-29 |
| EASA approval number |
|
| Contributor |
EASA Rotorcraft Section |
| 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
-
SA 330 J
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2018-0042 dated 14 February 2018.
|
| Publication(s) and related information |
Airbus Helicopters ASB AS332-05.01.10 original issue dated 25 October 2018.
Airbus Helicopters ASB SA330-05.105 original issue dated 25 October 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
18-144 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 29 October 2018 as PAD 18-144 for consultation until 12 November
2018. 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.
|
