Number |
2023-0003 |
Issued by |
Europe |
Issue date |
2023-01-06 |
Effective date |
2023-01-20 |
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 |
Not applicable
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes 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.
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.
Falcon 7X/8X OSM-MMEL Revision 15 effective date 01 March 2021.
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. 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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