Dassault Falcon 900

Development of intercontinental business jet announced at Paris Air Show on 27 May 1983.Derived from the Falcon 50, but substantially revised, the prototype Falcon 900 powered by Garrett TFE731 turbofan engines first flew on 21 September 1984. First customer deliveries took place in December 1986. Total delivered: 275.

Specifications: 900EX
Accommodation: 2 + 19
Cargo/baggage: 3.6 m³ (127 cu. ft)
Max Speed: MO. 84 (481 kt; 891 km/h)
Range: 3,810nm (7,056 km)

Wingspan: 19.3m (63 ft 5 in)
Length: 20.2m (66 ft 3 in)
Height: 7.6m ( 24 ft 10 in)

Low/swept wing; three Honeywell TFE731 turbofans, two mounted on side of rear fuselage, the third atop and at base of tail; 12 cabin windows; swept tailfin and mid-mounted tailplane.