Vehicle

Hawker 800

General Aviation and Light Aircraft

The Hawker 800 is a mid-size twinjet corporate aircraft, the 800 series development of the British Aerospace 125 business jet. The British Aerospace board sanctioned the improvement programme in April 1981 and the new aircraft was ready for its first test flight by May 1983. Compared with the 700 series it has a redesigned cockpit windscreen, a modified rear fuselage fairing, a glass cockpit, more powerful Garrett TFE731-5R-1H engines and wingtip devices to reduce drag. Raytheon, which had bought Beech Aircraft Corporation in 1980, acquired BAe Corporate Jets in 1994 and sold its aircraft manufacturing business to Hawker Beechcraft in 2007, so the type was assembled in Wichita, Kansas, from fuselage sections, wings and control surfaces built in the United Kingdom. The 800XP, 850XP, 900XP and 750 followed, and Japan uses a search and rescue version as the U-125A. After the 2013 bankruptcy of Hawker Beechcraft, the surviving company, Beechcraft, discontinued its business jets, including the 800 series.

Facts
Year
1983 1
Engine Class
Jet 1
Status
Out of production 1
Top Speed (km/h)
845 1
Mass (kg)
7076 2
Maximum Mass (kg)
12,428 2
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Hawker 800 (Wikipedia)

Of Make

Source Hawker 800 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Hawker 800 (Wikipedia)Development, end of production
Quote, Development, end of production
After the 2013 bankruptcy of Hawker Beechcraft, the surviving company, Beechcraft, discontinued its business jet range, including the 800 series.

Originated In

Also in Geography Atlas: where this subject originated.

Source Hawker 800 (Wikipedia)Development, origin
Quote, Development, origin
In April 1981, the British Aerospace (BAe) board sanctioned the programme to improve the British Aerospace 125-700 series.
Sources
1. flugzeuginfo.net: BAe, British Aerospace / Raytheon / Hawker Beechcraft BAe 125-800 / Hawker 800
flugzeuginfo.net
  • Data table, first flight
    First Flight 26.05.1983 (HS 125-800)
  • Lead, type
    is a series of twin-engined corporate jet aircraft
  • Data table, propulsion
    Propulsion 2 Turbofan Engines
  • Data table, production status
    Production Status out of production
  • Data table, speed
    Speed 845 km/h 456 kts
View the Source
2. Hawker 800 (Wikipedia)
  • Development, first flight
    By May 1983, the new aircraft was ready for its first test flight.
  • Lead, type
    The Hawker 800 is a mid-size twinjet corporate aircraft.
  • Specifications, powerplant
    Powerplant: 2 × Honeywell TFE731-5BR turbofan engines, 4,300 lbf (19 kN) thrust each
  • Development, end of production
    After the 2013 bankruptcy of Hawker Beechcraft, the surviving company, Beechcraft, discontinued its business jet range, including the 800 series.
  • Specifications, empty weight
    Empty weight: 15,600 lb (7,076 kg) basic
  • Specifications, maximum take-off weight
    Max takeoff weight: 27,400 lb (12,428 kg)
  • Specifications, maximum speed
    Maximum speed: 456 kn (525 mph, 845 km/h)
  • Development, origin
    In April 1981, the British Aerospace (BAe) board sanctioned the programme to improve the British Aerospace 125-700 series.
  • Exemplifies: Aviation, Lead, mode
    The Hawker 800 is a mid-size twinjet corporate aircraft.
View the Source
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