Overview
The Dassault Falcon 900EX entered service in the late 1990s as an enhanced version of the Falcon 900. Designed for improved range and avionics capability, it maintained the Falcon family’s distinctive trijet configuration. The aircraft targeted global corporate operators.
Live Fleet Activity (F900)
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Specifications
Units
- Engine
- 3 × Honeywell TFE731-60
- Engine type
- Turbofan
- Thrust
- 3 × 5,000 lbf · 22 kN
- Avionics
- Dassault 3D EASy Cockpit
- Wing tips
- No winglets
- Seats
- 19
- Crew
- —
- Cabin width
- 7 ft 9 in · 2.37 m
- Cabin height
- 6 ft 2 in · 1.88 m
- Cabin length
- 33 ft 2 in · 10.11 m
- Exterior length
- 66 ft 4 in · 20.21 m
- Tail height
- 24 ft 9 in · 7.55 m
- Fuselage diameter
- 8 ft 2 in · 2.50 m
- Wing span
- 63 ft 5 in · 19.33 m
- Baggage volume
- 141 ft³ · 4.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 48,300 lb · 21,900 kg
- Max landing weight
- 42,000 lb · 19,100 kg
- Max payload
- 6,150 lb · 2,800 kg
- Fuel capacity
- 3,150 gal · 11,800 L · 9,500 kg (Jet A)
- Max cruise speed
- 565 kt · 650 mph · 1,046 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 110 kt · 127 mph · 204 km/h
- Range
- 4,500 nm · 5,180 mi · 8,330 km
- Fuel burn
- 1.28 nm/gal · 0.63 km/L
- Ceiling
- 51,000 ft · 15,500 m
- Rate of climb
- 3,880 ft/min · 20 m/s
- Takeoff distance
- 5,200 ft · 1,590 m
- Landing distance
- 2,400 ft · 740 m
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Live fleet activity details
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