Dassault Falcon 10

Dassault Falcon 10 F-ZACB Banc D'Essais Larzac
Dassault Falcon 10 F-ZACB Banc D'Essais Larzac

The Dassault Mystère/Falcon 10 is an early corporate jet aircraft developed by French aircraft manufacturer Dassault Aviation. Despite its numbering sequence it was actually developed after the Falcon 20, and although it is sometimes considered as a scaled-down version of that aircraft, it was totally redesigned with a non-circular fuselage, a new wing with slotted flaps, a split passenger door and many simplified circuits compared to the Falcon 20.

Role Business jet
Manufacturer Dassault Aviation
First flight 1 December 1970
Introduction 1971
Status Active service, not in production
Primary user Corporate owners
Produced 1970–1989
Number built 226
Developed from Dassault Falcon 20

Specifications

General characteristics

  • Crew: 2
  • Capacity: 4–7
  • Length: 13.85 m (45 ft 5 in)
  • Wingspan: 13.08 m (42 ft 11 in)
  • Height: 4.61 m (15 ft 1 in)
  • Wing area: 24.1 m2 (259 sq ft)
  • Aspect ratio: 7.1:1
  • Empty weight: 4,880 kg (10,759 lb)
  • Max takeoff weight: 8,500 kg (18,739 lb)
  • Fuel capacity: 3,340 L (730 imp gal; 880 US gal)
  • Powerplant: 2 × Garrett TFE731-2 turbofans, 14.4 kN (3,230 lbf) thrust each

Performance

  • Cruise speed: 915 km/h (569 mph, 494 kn) (max cruise)
  • Never exceed speed: 650 km/h (400 mph, 350 kn) at sea level;
  • Max Mach Number: 0.87
  • Range: 3,555 km (2,209 mi, 1,920 nmi)

 

Dassault Falcon 10MER 101 French Navy
Dassault Falcon 10MER 101 French Navy

Photos Rob Vogelaar and Marcel van Leeuwen