Airbus A320-200 vs. Percival Provost

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Airbus A320-200 versus Percival Provost
38.7 m 127 ft 0 in length 9.0 m 29 ft 6 in
17.4 m 57 ft 1 in height 3.02 m 9 ft 11 in
35.8 m 117 ft 5 in wingspan 12.19 m 40 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 x Alvis Leonides Major 755/1 inline engine
Between 21,000 - 33,000 lbf thrust per engine Approximately 550 hp
Between 42,000 - 66,000 lbf total thrust Approximately 550 hp
77,000 kg 169,800 lb MTOW 5,500 lb 2,495 kg
5,700 km 3,078 nm range 1,127 km 608 nm
530 mph 853 km/h cruise speed 175 mph 282 km/h
Typically between 140-180 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.