Raytheon Hawker 800
| Raytheon Hawker 800 | |
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| Type: | Twin-engine business jet |
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The Raytheon Hawker 800 is a twin-engine, mid-range business jet . It is a low-wing aircraft with retractable landing gear and a pressurized cabin .
development
The development was originally carried out at Hawker Siddeley in the 1960s . The machine was named Hawker Siddeley HS.125 . After the founding of British Aerospace , the machine continued to be produced as the BAe 125. In 1993 Raytheon took over British Aerospace Corporate Jets. The new company Raytheon Aircraft (now Beechcraft Cooperation ) sold the aircraft as the Hawker 800 and developed it further.
In March 2006, the Hawker 850XP received its approval with improved avionics , modified interior fittings and new winglets .
In 2012 Hawker Beechcraft had to file for bankruptcy, but was able to resume business in early 2013 as the greatly reduced Beechcraft Corporation. The company is now focusing on the turboprop models and is discontinuing production of the jets. For the Hawker 800XP, however, an update program to the Hawker 800XPR version is offered, which is upgraded with more economical Honeywell TFE 731-50R engines and winglets .
Technical data (Hawker 850XP)
| Parameter | Data |
|---|---|
| crew | 2 |
| Passengers | 8, 15 maximum |
| length | 15.60 m |
| span | 16.56 m |
| height | 5.51 m |
| Empty mass | 7,108 kg |
| Takeoff mass | Max. 12,701 kg |
| Cabin length | 6.50 m |
| Cabin height | 1.75 m |
| Cabin width | 1.83 m |
| Engines | 2 × Honeywell TFE731 -5BR with 20.73 kN thrust each |
| Top speed | 824 km / h |
| Range | 4893 km with 4 passengers |
| Service ceiling | 12,500 m |
See also
Web links
- Hawker 800XPR website
- EASA-TCDS-A.085 (PDF; 254 kB) - Type certification of the Hawker series
Individual evidence
- ↑ Beechcraft starts the propellers , Handelsblatt , August 21, 2013
- ↑ Hawker 800XPR ( memento from September 23, 2014 in the Internet Archive ) on the Beechcraft website, accessed on August 30, 2014 (English)