Dassault Falcon 900EX

The trijet business jet built for intercontinental flexibility.

Overview

Dassault France ICAO: F900 1996–2010 Active $41 million (2009)

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)

📡

Fetching live data…

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
(/) tap to zoom
(/)
Dassault Falcon 900EX ‘M-MNDD’

Live fleet activity details

📡
Fetching live data…
Flight Airline Reg Alt Speed Heading V/S

Operational Context

Dassault Falcon 900EX — long-range trijet business jet

The Falcon 900EX first flew in 1996 and entered service in 1997. It incorporated aerodynamic refinements and updated flight systems compared with earlier variants. The three-engine layout supports operations from shorter runways.

Three Honeywell TFE731 turbofan engines producing approximately 5,000 pounds of thrust (22 kN) each power the aircraft. Cruise speed approaches Mach 0.84. Maximum takeoff weight exceeds 49,000 pounds (22,226 kg), with range near 4,500 nautical miles (8,334 km).

The 900EX became a popular long-range corporate platform. Its flexibility in airport access distinguished it from twin-engine competitors. The aircraft remains active in global business aviation fleets.

Blog mentions