AD 2014-12-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault | Aviation | Airworthiness Directives; Dassault Aviation Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Dassault Aviation Airplanes |
Unsafe Condition
During a test flight on a Falcon 2000EX equipped with winglets, the airplane experienced unsatisfactory control characteristics under specific combined conditions of loading, slat-flap setting, and horizontal tailplane trim setting. This could result in an erratic takeoff path and reduced control of the airplane.
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Required Actions
Revise the airplane flight manual (AFM) to include procedures to advise the flightcrew of new center of gravity (CG) limits applicable during takeoff with a Slat/Flap SF2 setting.
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Compliance Time
Before further flight
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Affected Aircraft
Dassault Aviation Model FALCON 2000 and FALCON 2000EX airplanes, excluding those modified by Aviation Partners Incorporated STC ST01987SE and those on which Dassault Service Bulletin F2000EX-300, Revision 1, has been embodied.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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