| Number |
2022-0128 |
| Issued by |
 Europe |
| Issue date |
2022-06-30 |
| Effective date |
2022-07-14 |
| EASA approval number |
|
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B
-
AS 350 B1
-
AS 350 B2
-
AS 350 B3
-
AS 350 BA
-
AS 350 BB
-
AS 350 D
-
EC 130 B4
-
EC 130 T2
-
AS 355
-
AS 355 E
-
AS 355 F
-
AS 355 F1
-
AS 355 F2
-
AS 355 N
-
AS 355 NP
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2018-0152 dated 18 July 2018.
|
| Publication(s) and related information |
AH EC 130 ASB No. EC130-05A028 original issue dated 16 July 2018, or Revision 1 dated 30 May 2022.
AH AS 350 ASB No. AS350-05.00.92 original issue dated 16 July 2018, or Revision 1 dated 30 May 2022.
AH AS 355 ASB No. AS355-05.00.79 original issue dated 16 July 2018, or Revision 1 dated 30 May 2022.
AH SB EC130-53-045 original issue dated 30 May 2022.
AH SB AS350-53.00.65 original issue dated 30 May 2022.
AH SB AS355-53.00.36 original issue dated 30 May 2022.
The use of later approved revisions of the above-mentioned documents is acceptable for
compliance with the requirements of this AD. |
| PAD number |
22-071 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 31 May 2022 as PAD 22-071 for consultation until 28 June 2022. 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.
|
