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ADs [at] easa.europa [dot] eu
|
| Number |
21-058R1 |
| Issued by |
 Europe |
| Issue date |
2021-06-25 |
| EASA approval number |
|
| Contributor |
EASA General Aviation & VTOL Department |
| ATA Chapter |
31 |
Approval Holder
/ Type Designation |
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
AS 350 B2
-
AS 350 B3
-
EC 130 B4
-
EC 120 B
|
| Revision |
This PAD is revised to expand the Applicability for EC 120 B helicopters, and republished for
additional consultation.
|
| Correction |
Not applicable
|
| Supersedure |
None
|
| Publication(s) and related information |
AH ASB EC130-05A036 original issue dated 31 March 2021.
AH ASB No. AS350-05.01.00 original issue dated 31 March 2021.
AH ASB EC120-05A023 original issue dated 31 March 2021.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. This Proposed AD will be closed for consultation on 09 July 2021.
2. Enquiries regarding this PAD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs[at]easa.europa.eu.
3. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this PAD, and which may occur, or have occurred
on a product, part or appliance not affected by this PAD, 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 PAD 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.
|
