Dassault Falcon 50 Civil Aircraft Model Details

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General Information of Dassault Falcon 50

Developed From : Dassault Falcon 20

First Flight : 28071

Manufacturer : Dassault Aviation

Number Built : 352

Primary Users : Armee de l'Air; South African Air Force; Italian Air Force

Produced : 1976–2008[1]

Role : Business jet

Status : Active

Variants : Dassault Falcon 900

General characteristics of Dassault Falcon 50

Capacity : 8 to 9 passengers

Crew : Two

Empty Weight : 20,200 lb (9,163 kg)

Height : 22 ft 10½ in (6.98 m)

Length : 60 ft 9¼ in (18.52 m)

Max Takeoff Weight : 38,800 lb (17,600 kg) Falcon 50; 40,780 lbs (18,500 kb) Falcon 50EX ()

Powerplant : 3 × Garrett TFE731-3-1C on Falcon 50 / 3 x Honeywell TFE731-40 on Falcon 50EX models turbofan engines, 16.5 kN (3,700 lbf) each

Wing Area : 504.1 ft² (46.83 m²)

Wingspan : 61 ft 10½ in (18.86 m)

Performance of Dassault Falcon 50

Cruise Speed : Mach 0.80 Indicated Mach (0.786 True Mach) (837 km/h, 452 knots, 520 mph)

Maximum Speed : Mach 0.86 Indicated Mach (0.842 True Mach) (900 km/h, 484 knots, 557 mph)

Range : 3,000NM, 3,450 sm / 5,555 km (Falcon 50); 3,220NM, 3,700 sm / 5,965 km (Falcon 50EX) ()

Service Ceiling : 49,000 ft (14,935 m) - Typical Cruise Altitude 37,000 ft Falcon 50; 41,000-43,000 ft Falcon 50EX

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