Airbus A220-100 vs. Percival Provost

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Airbus A220-100 versus Percival Provost
35.0 m 114 ft 10 in length 9.0 m 29 ft 6 in
11.5 m 37 ft 9 in height 3.02 m 9 ft 11 in
35.1 m 115 ft 2 in wingspan 12.19 m 40 ft
2 Turbofans (wing mounted) engines 1 x Alvis Leonides Major 755/1 inline engine
21,000–23,000 lb thrust per engine Approximately 550 hp
42,000–46,000 lb total thrust Approximately 550 hp
63,100 kg 139,100 lb MTOW 5,500 lb 2,495 kg
6,390 km 3,451 nm range 1,127 km 608 nm
871 km/h 541 mph cruise speed 175 mph 282 km/h
Typical seating 2-class 100-120 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.