| Number |
2019-0008 |
| Issued by |
 Europe |
| Issue date |
2019-01-22 |
| Effective date |
2019-02-05 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
SA/AS 365 / EC 155
-
AS 365 N2
-
AS 365 N3
-
EC 155 B
-
EC 155 B1
-
SA 365 N
-
SA 365 N1
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2017-0055 dated 31 March 2017.
|
| Publication(s) and related information |
AH ASB AS365-53.00.55 original issue dated 13 March 2017.
AH ASB EC155-53A035 original issue dated 13 March 2017.
AH ASB AS365-53.00.62 original issue dated 20 December 2018.
AH ASB EC155-53A038 original issue dated 20 December 2018.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD.
|
| PAD number |
18-188 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 21 December 2018 as PAD 18-188 for consultation until 18 January
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.
|
