Technical Details

• Manufacturer: Dassault Aviation, France
• Engines: 3 turbofans Honeywell TFE731-60,
  each with 2'270 kp (5'000 lb) static thrust.
  The middle engine is equipped with a thrust reverser.
• Wingspan: 19.33 m (63 ft 5 in)
• Length: 20.21 m ( 66 ft 4 in )
• Height: 7.55 m (24 ft 9 in)
• Max. take-off weight: 22'200 kg (49'200 Ib)
• Basic operating weight: 11'745 kg (26'100 Ib)
• Fuel capacity: 11'865 l (21'000 Ib)
• Take-off run*: 1'563 m (5'215 ft) at max. take-off weight
• Landing run*: 1'074 m (3'522 ft) at max. landing weight
• Range*: max. 8'330 km (4'500 nm)
• Cruising speed: 830 to a max. 870 km/h
  (450 to 470 kt), Mach .87
• Service ceiling: 15'500 m (51'000 ft)
• Crew: 2 pilots and 1 cabin attendant
• Passengers: 
  • max. 14 at reduced range
  • max. 8 at max. range
  • max. 5 fully-equipped sleeping berths
• The aircraft is licensed for nonstop ocean crossings as well as landings in very bad weather conditions (ILS Category II).

*Dependent on weight, flight speed and wind conditions.