| Number |
2021-0283R1 |
| Issued by |
 Europe |
| Issue date |
2022-02-25 |
| Effective date |
2022-02-18 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
53 |
Approval Holder
/ Type Designation |
|
| Revision |
This AD revises EASA Emergency AD 2021-0283-E dated 17 December 2021.
|
| Correction |
This AD is re-published to correct the issue date.
|
| Supersedure |
The original issue of this AD superseded EASA Emergency AD 2021-0235-E dated 28 October 2021.
|
| Publication(s) and related information |
AH Emergency ASB EC130-05A039 original issue dated 27 October 2021, or Revision 1 dated 16 December 2021, or Revision 2 dated 09 February 2022.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication.
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.
|
