Hawker 800

The Raytheon Hawker 800 is a twin-engined mid-size business jet. It is a low-wing monoplane with retractable landing gear and a pressurized cabin. The development was originally performed in the 1960s at Hawker Siddeley. The machine was called the Hawker Siddeley HS.125. After the establishment of British Aerospace, the machine was further produced as a BAe 125. In 1993, Raytheon British Aerospace Corporate Jets. The new company Raytheon Aircraft (now Hawker Beechcraft ) drove the aircraft as the Hawker 800 and developed it further.

The current version is fitted over its predecessors with improved avionics and revised interior and fitted with winglets Hawker 850XP, which was admitted in March 2006.

Technical data ( Hawker 850XP )

  • Crew: 2
  • Passengers: 8, 15 maximum
  • Length: 15,60 m
  • Wingspan: 16.56 m
  • Height: 5.51 m
  • Empty weight: 7108 kg
  • Off weight max. 12,701 kg
  • Cabin length: 6.50 m
  • Cabin height: 1.75 m
  • Cabin width: 1,83 m
  • Engines: 2 × Honeywell TFE731 - 5BR, each with 20.73 kN thrust
  • Maximum speed: 824 km / h
  • Range: 4893 km with 4 passengers
  • Service ceiling: 12,500 m
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