Please feel free to send us your comments by email at
ADs [at] easa.europa [dot] eu
|
| Number |
24-112 |
| Issued by |
 Europe |
| Issue date |
2024-09-26 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
64 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2021-0069 dated 11 March 2021.
|
| Publication(s) and related information |
AH Emergency ASB EC120-05A020 original issue dated 29 October 2019, or Revision 1 dated 08 November 2019, or Revision 2 dated 08 February 2021, or Revision 3 dated 19 September 2024.
AH ASB EC120-64-21-0001 original issue dated 19 September 2024.
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 24 October 2024.
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.
|
