Hawker 800 British Mid-Size Business Jet
Mid-Size Business Jet
Other
Basic Information
Name
Hawker 800 British Mid-Size Business Jet
Designation
—
Alternate Designation
—
Equipment Type
Mid-Size Business Jet
Manufacturer
British Aerospace (1983-1994) Raytheon (1994-2007) Hawker Beechcraft (2007-2013)
Date of Introduction
1983
Description
The Hawker 800 is a mid-size twinjet corporate aircraft. It is a development of the British Aerospace BAe 125, and was assembled by Hawker Beechcraft.
Air & Air Defense Specifications
Crew
2
Engine
Turbofan (4300 hp)
Max Speed
456.0 km/h
Cruise Speed
400.0 km/h
Variants
Hawker 750
With 48 built, this lower-cost, lighter-weight and shorter-range version of the 800XP competes with the Citation XLS and Learjet 60. In November 2017, used prices range from $2.2 million for early 2008 models to 3.8 million for late 2011 models. Its larger 604 cu ft (17.1 m3) cabin is typically configured with eight seats in double club or a four chair club followed by a three-place divan facing a single seat, and is pressurized by 8.5 psi (0.59 bar) to provides a 7,500 ft (2,300 m) cabin altitude at FL 410. Its 1,500 lb (680 kg) ventral fuel tank is replaced with a 47 cu ft (1.3 m3) external baggage compartment, leaving 8,500 lb (3,900 kg) of fuel in the wet wings.
Hawker 800XP
Able to fly nine passengers over 2,400 nmi, 475 Hawker 800XP have been sold for $10–13.5 million between 1995 and 2005. By July 2018, 467 were still in service, valued $1.4–2.4 million.
System
Alternate Designation(s)
Hawker 800
Type
Mid-Size Business Jet
Manufacturer
British Aerospace (1983–1994)
Raytheon (1994–2007)
Hawker Beechcraft (2007–2013)
Crew
2 + jump seat
Cargo Capacity
907 kg maximum payload
Number of Engines
2
Number of Hard Points
INA
Dimensions
Length
15.60 m
Width (Wing Span)
5.659 m
Wing Area
34.7 m2
Height
5.36 m
Empty Weight
7,076 kg
Operating Weight
7,257 kg
Maximum Ramp Weight
12,483 kg
Maximum Zero-Fuel Weight
8,165 kg
Maximum Takeoff Weight
12,428 kg
Maximum Landing Weight
10,591 kg
Automotive
Engine Name
2 × Honeywell TFE731-5BR
Engine Type
Turbofan
Engine Power
4,300 lbf (19 kN) thrust each
Fuel Capacity
1,248 imp gal (1,499 US gal; 5,674 l) total ; 1,060 imp gal (1,273 US gal; 4,819 l) in wing integral tanks + 188 imp gal (226 US gal; 855 l) in rear under-fuselage tank
Maximum Speed
456 kn (525 mph, 845 km/h) max level speed and max cruising speed at 29,000 ft (8,839 m) / M0.87
Cruise Speed
400 kn (460 mph, 740 km/h) economical cruise at 39,000–43,000 ft (11,887–13,106 m)
Stall Speed
92 kn (106 mph, 170 km/h) in landing configuration at typical landing weight
Range
2,580 nmi (2,970 mi, 4,780 km) with max payload; 2,825 nmi (3,251 mi; 5,232 km) with max fuel and NBAA VFR reserves
Service Celling
43,000 ft (13,000 m)
Rate of Climb
3,100 ft/min (16 m/s)
Protection
Stealth Properties
None
Heat Signature Reduction
No
Add on Armor
INA
NBC Protection
INA
EW Counter Measures
No
Chaffs/Flares
No
Details
Country of Origin
United Kingdom
Category
Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
15.6 m
Width
5.66 m
Height
5.36 m
Weight
12483 kg
Operators (7)
United States
United Kingdom
Japan
South Korea
Pakistan
Mozambique
United Nations
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