| Number |
2026-0016 |
| Issued by |
 Europe |
| Issue date |
2026-01-26 |
| Effective date |
2026-02-09 |
| EASA approval number |
|
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
-
DASSAULT AVIATION
-
Falcon 7X
-
Falcon 7X
-
Falcon 8X (M1000)
|
| Revision |
Not applicable
|
| Correction |
Not applicable
|
| Supersedure |
This AD supersedes EASA AD 2024-0224 dated 26 November 2024.
|
| Publication(s) and related information |
Dassault SB 7X-586, original issue dated 05 September 2024, including related Erratum dated 16 October 2024, and revision 1 dated 03 December 2025.
The use of later approved revisions of the above-mentioned document is acceptable for compliance with the requirements of this AD. |
| PAD number |
25-195 |
| Remarks |
1.
If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2.
This AD was posted on 17 December 2025 as PAD 25-195 for consultation until 14 January 2026. 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.
|
