HAWKER SIDDELEY H.S.125 Civil Aircraft Model Details

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General Information of HAWKER SIDDELEY H.S.125

First Flight : 22871

Manufacturer : de Havilland (design); Hawker Siddeley (to 1977); British Aerospace (1977–1993); Raytheon (1993–2007); Hawker Beechcraft (Since 2007)

Number Built : 1,000+

Produced : 1962-present

Role : Mid-size business jet

Status : in production

Variants : Hawker 800

General characteristics of HAWKER SIDDELEY H.S.125

Capacity : 8 passengers (normal layout), 14 passengers in high density layout

Crew : 2

Empty Weight : 12,530 lb (5,683 kg)

Height : 17 ft 3 in (5.26 m)

Length : 50 ft 6 in (15.39 m)

Max Takeoff Weight : 25,000 lb (11,340 kg)

Powerplant : 2 × Rolls-Royce Viper 601-22 turbojets, 3,750 lbf (16.7 kN) each

Wing Area : 353.0 ft² (32.8 m²)

Wingspan : 47 ft 0 in (14.33 m)

Performance of HAWKER SIDDELEY H.S.125

Cruise Speed : 464 mph (403 knot, 747 km/h) at 39,000 ft (11,900 m) (Econ cruise)

Maximum Speed : 522 mph (454knot, 840 km/h) at 28,000 ft (8,500 m) (Max cruise)

Range : 1,796 mi (1,560nmi, 2,891 km)max fuel and payload

Rate Of Climb : 4,900 ft/min (24.9 m/s)

Service Ceiling : 41,000 ft (12,500 m)

Stall Speed : 96 mph (83 knots, 155 km/h) (flaps down)

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