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Aircraft DataThe Dassault Falcon 50 is a three engined super mid-sized, long-range corporate jet. It is a three engined development of the earlier Falcon 20, the final, definitive version is the Falcon 50EX, production finished in 2007.
|Country of origin||First flight||No. built||No. in service||Crew||Passengers|
|France||1976||356||356||2||8 - 12|
3 x Honeywell TFE 731 (3500 - 4750 lbf) turbofan engines.
Uses TFE731-3-1C turbofan engines, rated at 3700lb thrust.
|Length||60 ft. 8 in.|
|Wing Span||61 ft. 10 in.|
|Height||22 ft. 10 in.|
|Empty Weight||20,170 lbs. (Weights for the baseline Falcon 50)|
|Max Weight||38,800 lbs.|
|Max Speed||475 kts (Performance for the baseline Falcon 50)|
|Cruise Speed||370 kts|
|Max Range||3,575nm (Range with 8 passengers and normal reserves.)|
Updated 22nd January 2009Show using: Metric | Imperial
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Dassault Falcon 50EX
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