Overview
The Falcon 50EX evolved from the original Falcon 50 with upgraded engines and avionics. Entering service in the mid-1990s, it offered improved fuel efficiency and range. The aircraft continued Dassault’s emphasis on long-range capability.
Live Fleet Activity (FA50)
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Specifications
Units
- Engine
- 3 × Honeywell TFE731-40 turbofans
- Engine type
- Turbofan
- Thrust
- 3 × 3,700 lbf · 16 kN
- Avionics
- Collins Pro Line 4 Avionics Suite
- Wing tips
- No winglets
- Seats
- 10
- Crew
- —
- Cabin width
- 6 ft 1 in · 1.86 m
- Cabin height
- 5 ft 11 in · 1.80 m
- Cabin length
- 23 ft 6 in · 7.16 m
- Exterior length
- 60 ft 8 in · 18.50 m
- Tail height
- 22 ft 11 in · 6.98 m
- Fuselage diameter
- 8 ft 2 in · 2.50 m
- Wing span
- 61 ft 10 in · 18.85 m
- Baggage volume
- 106 ft³ · 3.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 40,800 lb · 18,500 kg
- Max landing weight
- 35,700 lb · 16,200 kg
- Max payload
- 3,300 lb · 1,500 kg
- Fuel capacity
- 2,300 gal · 8,800 L · 7,000 kg (Jet A)
- Max cruise speed
- 481 kt · 554 mph · 891 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 95 kt · 109 mph · 176 km/h
- Range
- 3,200 nm · 3,680 mi · 5,930 km
- Fuel burn
- 1.33 nm/gal · 0.65 km/L
- Ceiling
- 49,000 ft · 14,900 m
- Rate of climb
- 3,500 ft/min · 18 m/s
- Takeoff distance
- 4,950 ft · 1,500 m
- Landing distance
- 2,250 ft · 690 m
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