Airbus A310-300 vs. BAC Jet Provost

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Airbus A310-300 versus BAC Jet Provost
46.66 m 153 ft 1 in length 10.36 m 34 ft 0 in
15.8 m 51 ft 10 in height 3.1 m 10 ft 2 in
43.9 m 144 ft wingspan 11.25 m 36 ft 11 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Bristol Siddeley Viper 201
52,000 lb thrust per engine 2,500 lb = 1,134 kg
104,000 lb total thrust 2,500 lb = 1,134 kg
148,768 kg 328,000 lb MTOW 4,173 kg 9,200 lb
8,050 km 4,348 nm range 1,448 km 782 nm
482 knots 279 mph cruise speed 440 mph 708 km/h
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.