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The launch of the Raytheon Hawker 800XP extended performance mid-size business jet was announced in 1995. The aircraft is in service both as a business / VIP jet and also in special mission versions. The XP features uprated engine, enhanced aerodynamics, increased weight and system upgrades. In December 2006, Raytheon announced the sale of Raytheon Aircraft to GS Capital Partners. The new company is called Hawker Beechcraft Inc and the sale was completed in March 2007.
The Hawker 800XP business jet is derived from the design of the UK-built de Havilland / Hawker Siddely and British Aerospace 125, first built in 1962, which evolved into the Series 400 to 800 produced up to the early 1990s. Raytheon purchased the Series 800 program in 1993 and the aircraft took the name Hawker 800.
Over 275 of the Hawker 800 were built until final production in 1995 when the 800XP entered service.
Design
The Hawker 800XP is of all-metal construction with low sweptback one-piece wings, a high tailplane and rear-mounted engines. The leading edges of the wings and tailplane are fitted with a TKS liquid de-icing and anti-icing system.
BAE Systems Aerostructures supplies the doors, fuel tanks, flaps and elevators, and from September 2004, the rudder and tailplane assemblies.
Flight deck
The flight deck of the Hawker 800XP accommodates two crew with a third seat for an observer or crew member. The windscreen is fitted with an electrical anti-icing system.
Since 2002, the Hawker 800XP has been equipped with the Rockwell Collins Pro Line 21 avionics suite. The suite includes four 10in x 8in active matrix liquid crystal displays, dual FMS 6000 flight management system, digital autopilot, GPS-4000A global positioning system, TCAS 4000 traffic alert and collision avoidance system, TWR 850 turbulence-detection weather radar system, Terrain Awareness Warning System (TAWS) and dual Attitude Heading Reference System (AHRS) that uses a digital quartz gyro. Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) is also fitted.
Cabin
The 17.1m³ (604ft³) cabin can accommodate up to 14 seats, with typical seating layouts for six to ten passengers in a variety of configurations. A VIP cabin layout provides seating for eight passengers with four club seats at the front of the cabin, a three-seat settee and a single seat at the rear of the cabin. The luggage compartment is accessible in flight.
In 1999, Raytheon restyled the interior: the interior window frames were restyled from square to oval, passenger seats were restyled and retailored, sidewall lighting was added and the side panel worktables were redesigned for easier access.
Engines
The aircraft is powered by two rear-mounted Honeywell TFE731-5BR-1H turbofan engines each rated at 20.73kN. The engines, fitted with Dee Howard thrust reversers, are mounted in Northrop Grumman pods on either side of the rear fuselage. The engines are fitted with BCF engine fire extinguishers and engine bleed air ice protection.
The aircraft has integral fuel tans in the wings and a rear underfuselage tank, of total capacity 5,700l.
Landing gear
The aircraft is equipped with twin-wheeled hydraulically retractable tricycle-type landing gear.
The landing gear is fitted with Dunlop wheels, Dunlop triple disc hydraulically operated brakes and a Maxaret anti-skid system. The main gear retracts inward into the wings and the nose unit retracts forward.
Dimensions
Length
15.6m
Height to Top of Tail
5.36m
Wingspan
15.66m
Span of Tailplane
6.1m
Wing Area
34.75m²
Length
6.5m
Width
1.83m
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