| Number |
2023-0003R1 |
| Issued by |
 Europe |
| Issue date |
2024-09-26 |
| Effective date |
2024-10-03 |
| EASA approval number |
|
| Contributor |
EASA General Aviation Department |
| ATA Chapter |
34 |
Approval Holder
/ Type Designation |
-
DASSAULT AVIATION
-
Falcon 7X
-
Falcon 7X
-
Falcon 8X (M1000)
|
| Revision |
This AD revises EASA AD 2023-0003 dated 06 January 2023.
|
| Correction |
Not applicable
|
| Supersedure |
The original issue of this AD superseded EASA AD 2022-0145 dated 12 July 2022.
|
| Publication(s) and related information |
Dassault AFM-CP0177-PUB dated 28 June 2021.
Dassault AFM-CP0178-PUB dated 07 April 2022.
Dassault AFM-CP0185-PUB dated 27 July 2022.
Dassault AFM-CP0186-PUB dated 27 July 2022.
Dassault MMEL-CP0299-PUB dated 14 April 2021.
Dassault OSM-FC DGT 148654 Revision 06 dated 02 July 2021, Revision 07 dated 21 June 2022, or Revision 08 dated 31 January 2023.
Dassault SB 7X-590 original issue dated 19 April 2022, released on 20 June 2022.
Dassault SB 7X-591 original issue dated 15 September 2022, released on 15 December 2022.
Dassault SB 7X-592 original issue dated 15 September 2022, released on 15 December 2022.
Dassault SB 7X-600 original issue dated 07 November 2022, revision 01 dated 23 November 2022, and revision 02 dated 18 December 2023.
Dassault SB 7X-601 original issue dated 24 April 2023, and revision 01 dated 18 December 2023.
Dassault SB 7X-602 original issue dated 03 June 2024.
Falcon 7X/8X OSM-MMEL Revision 15 effective date 01 March 2021, or Revision 16 effective date 01 August 2023.
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD. |
| PAD number |
22-172 |
| Remarks |
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The original issue of this AD was posted on 16 December 2022 as PAD 22-172 for consultation until 30 December 2022. 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.
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