The Hawker 800 was first flown as the B.Ae. 125
Series 800 powered by 2x 4300lb.s.t (19.13kN) Garrett TFE731-5’s in
1983. It was an improved version of the H.S.125 Series 700 and was built
in several variants including the Series 800A which was for sale to
North America only, and the Series 800B for sale to the rest of the
world. In 1993 Raytheon purchased the corporate jets division of B.Ae.
and the type was re-designated Raytheon Hawker 800. Production in the US
began in 1996 under the designation Hawker 800 XP (Extended
Performance). The Hawker 800Xpi was introduced in 2005 and features
upgraded avionics. The Hawker 850XP (120+ built) was introduced in 2006
and is an upgraded version of the Hawker 800Xpi with a 4% increase in
range and an improved maintenance schedule. Two other versions were also
introduced in 2006. The Hawker 750 has a baggage compartment installed
in place of the ventral fuel tank giving a range of 2533miles(4074km).
The Hawker 900XP (30+ built) has an increased wingspan of 54’4"(16.56m)
and a range of 3397miles(5463km).
N345BR
c/n 258308
USA
16 seat executive jet first flown in 1983
Engines:2x 4660lb.s.t.(20.7kN)AlliedSignal TFE7315BR
Length: 51’2"(15.6m)
Height: 17’7"(5.36m)Wingspan: 51’5"(15.66m)
No.built: 860+ Range: 3400miles(5472km)
Cruising speed: 461mph(741kmh) Empty weight: 16,270lb(7380kg)
Maximum take-off weight: 28,000lb(12,701kg) |