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| The 125-800 evolved from the HS125-700 and introduced a number of improvements. Aerodynamic changes included a re-profiled nose and windscreen, extended fin leading edge, and greater span wing which decreased drag and increased lift and fuel capacity. Range was boosted further by a larger ventral fuel tank. More powerful TFE731s improved field performance, while a redesigned interior made more efficient use of the space available. The 800 was also the first corporate jet to feature an EFIS cockpit. The 800A was specifically aimed at the US market, the 800B for non US markets. The 125-800 became the Hawker 800 from mid 1993 when Raytheon purchased BAe\'s Corporate Jets division. Production has been transferred to Wichita in the USA (the first US built 800 flew on November 5 1996, the last UK built 800 on April 29 1997). Current production is of the 800XP (Extended Performance) which was certificated in 1995 and has improved engines for better climb and cruise performance. A new interior was introduced in 1999. |
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| Seating (normal) |
8 |
Max Takeoff (lbs) |
27,400 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
41,000 |
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| Engines |
2 Hon TFE731-5R-1H |
To (Sealevel, ISA Temp) (ft) |
5,600 |
| Output lbs ea. Flat Rating |
4,300 |
Landing Distance (ft) |
2,325 |
| Maximum Mach No. |
0.80 |
Max Range (fuel) (nm) |
2,449 |
| High Speed Cruise (Kts) |
442 |
Max Range (payload) (nm) |
2,219 |
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| Flight Time 300nm |
0 + 50 |
Flight Time 1000nm |
2 + 28 |
| Flight Time 600nm |
1 + 31 |
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| External |
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Internal |
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| Length (ft) |
51.10 |
Length (ft) |
21.30 |
| Height (ft) |
17.40 |
Height (ft) |
5.80 |
| Span (ft) |
51.40 |
Width: Max floor (ft) |
6.00 |
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