Airbus A300-600 vs. Percival Provost

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Airbus A300-600 versus Percival Provost
54.10 m 177 ft 6 in length 9.0 m 29 ft 6 in
16.5 m 54 ft 2 in height 3.02 m 9 ft 11 in
44.84 m 147 ft 1 in wingspan 12.19 m 40 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 x Alvis Leonides Major 755/1 inline engine
56,000lb to 61,500lb thrust per engine Approximately 550 hp
112,000–123,000 lb total thrust Approximately 550 hp
171,700 kg 378,600 lb MTOW 5,500 lb 2,495 kg
7,500 km 4,052 nm range 1,127 km 608 nm
897 km/h 557 mph cruise speed 175 mph 282 km/h
210-250 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.