AD 2007-25-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Mystere-Falcon 50 | Airworthiness Directives; Dassault Model Mystere-Falcon 50, Mystere-Falcon 900, Falcon 900EX, Falcon 2000, and Falcon 2000EX Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Model Mystere-Falcon 50, Mystere-Falcon 900, Falcon 900EX, Falcon 2000, and Falcon 2000EX Airplanes |
Unsafe Condition
Failure of the rotating rod in the control linkage of the trailing edge flap and consequent flap asymmetry during the approach to landing, which could result in reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Verify the correct assembly of the flap rotating rods and associated brackets, inspect the rod for damage, and replace the rod if any damage is found. If the rod orientation or bracket positioning is incorrect, correct it prior to next flight. Label the rods and associated retaining brackets as required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 330 flight hours or 7 months after the effective date of this AD, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Dassault Model Mystere-Falcon 50, Mystere-Falcon 900, Falcon 900EX, Falcon 2000, and Falcon 2000EX airplanes on which specific modifications (M2996, M5007, or M2465) have not been implemented.
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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