Airbus A310-300 vs. Percival Provost

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Airbus A310-300 versus Percival Provost
46.66 m 153 ft 1 in length 9.0 m 29 ft 6 in
15.8 m 51 ft 10 in height 3.02 m 9 ft 11 in
43.9 m 144 ft wingspan 12.19 m 40 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Alvis Leonides Major 755/1 inline engine
52,000 lb thrust per engine Approximately 550 hp
104,000 lb total thrust Approximately 550 hp
148,768 kg 328,000 lb MTOW 5,500 lb 2,495 kg
8,050 km 4,348 nm range 1,127 km 608 nm
482 knots 279 mph cruise speed 175 mph 282 km/h
190-230 passengers capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.