| Number |
2024-0007-E |
| Issued by |
 Europe |
| Issue date |
2024-01-08 |
| Effective date |
2024-01-10 |
| EASA approval number |
|
| Contributor |
EASA VTOL Department |
| ATA Chapter |
67 |
Approval Holder
/ Type Designation |
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA Emergency AD 2023-0204-E dated 20 November 2023.
|
| Publication(s) and related information |
HG SB 23-006 (A) original issue dated 24 July 2023, or 23-006 B (Revision B) dated 14 November 2023, or 23-006 C (Revision C) dated 22 November 2023, or 23-006 D (Revision D) dated 05 January 2024.
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. The results of the safety assessment have indicated the need for immediate publication and
notification, without the full consultation process.
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.
|
