Number |
2019-0109 |
Issued by |
Europe |
Issue date |
2019-05-20 |
Effective date |
2019-06-03 |
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 L
-
AS 332 L1
|
Revision |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes EASA AD 2015-0153R1 dated 09 November 2015.
|
Publication(s) and related information |
AH ASB AS332-05.01.02 original issue dated 22 July 2015, or Revision 1 dated 05 November 2015, or
Revision 2 dated 16 April 2019.
AH ASB AS332-30.00.85 original issue dated 16 April 2019.
AH ASB AS332-30.90.86 original issue dated 16 April 2019.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
PAD number |
19-070 |
Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 18 April 2019 as PAD 19-070 for consultation until 16 May 2019. 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.
|