AD 2007-12-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Falcon 2000EX and Falcon 900EX | Airworthiness Directives; Dassault Model Falcon 2000EX and Falcon 900EX Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Model Falcon 2000EX and Falcon 900EX Airplanes |
Unsafe Condition
Some stringer reinforcements (F900DX) and some rivets (F900DX/F2000EX) are missing from the skin panels on each side of the fuselage between frames 9 and 10 on certain Falcon 900DX and Falcon 2000EX EASy aircraft, affecting the structural integrity of the fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and repair the aircraft in accordance with Dassault Service Bulletin F900EX-308 for version F900DX, S/Ns 601 through 605, and Dassault Service Bulletin F2000EX-133 for Model F2000EX, S/N 82. Inspect the area, including holes and structure, where missing rivets are found, and contact the manufacturer if holes are out-of-round beyond tolerance or if cracks are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3 months after the effective date of this AD
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Affected Aircraft
Dassault Model Falcon 2000EX airplanes, S/N 82; and Model Falcon 900EX (version F900DX) airplanes, S/Ns 601 through 605, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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