Airbus A321LR vs. Percival Provost

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Airbus A321LR versus Percival Provost
44.51 m 146 ft 0 in length 9.0 m 29 ft 6 in
11.76 m 38 ft 7 in height 3.02 m 9 ft 11 in
35.8 m 117 ft 5 in wingspan 12.19 m 40 ft
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Alvis Leonides Major 755/1 inline engine
Over 33,000 lbs (147 kN) thrust per engine Approximately 550 hp
66,000 lbs (294 kN) total thrust Approximately 550 hp
97,000 kg 213,800 lb MTOW 5,500 lb 2,495 kg
7,400 km 4,000 nm range 1,127 km 608 nm
832 km/h 517 mph cruise speed 175 mph 282 km/h
180-220 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.