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Raytheon Hawker 1000   


The Hawker 1000 was originally the B.Ae. 125-1000 and was a stretched version of the B.Ae.125-800 (Hawker 800) intended for intercontinental service. Production ended in 1997.

Raytheon Hawker 1000 G-BUIX

G-BUIX                  c/n 259024                       USA

17 seat executive jet first flown in 1990

Engines: 2x 5200lb.s.t.(23.1kN) P&W PW305                                                                                Length: 53’10"(16.42m)                                                                                      Height: 17’1"(5.21m)Wingspan: 51’4"(15.66m)                                                                                                No.built: 52 Range: 3850miles(6195km)                                                           Cruising speed: 462mph(743kmh) Empty weight: 17,220lb(7810kg)                                     Maximum take-off weight: 31,000lb(14,060kg)

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