Dassault Falcon 50EX Private F-HCEF
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Aircraft Data
The 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 |
Power
Uses TFE731-3-1C turbofan engines, rated at 3700lb thrust.
Engine Count | 3 | |
Engine Variations | ||
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Engine Name |
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Engine Class |
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Engine Power |
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Dimensions
Length | 18.49 m. 60 ft. 8 in. |
Wing Span | 18.85 m. 61 ft. 10 in. |
Height | 6.96 m. 22 ft. 10 in. |
Empty Weight |
9157 kg.
20170 lbs.
Weights for the baseline Falcon 50 |
Max Weight | 17615 kg. 38800 lbs. |
Performance
Max Speed |
764 kph
475 mph
Performance for the baseline Falcon 50 |
Cruise Speed | 595 kph 370 mph |
Ceiling | 13716 m. 45000 ft. |
Normal Range | 5834 3150 nm km. |
Max Range |
6621
3575
nm
km.
Range with 8 passengers and normal reserves. |
Display data using: Metric Imperial
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