Airbus A220-100 vs. BAC Jet Provost

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Airbus A220-100 versus BAC Jet Provost
35.0 m 114 ft 10 in length 10.36 m 34 ft 0 in
11.5 m 37 ft 9 in height 3.1 m 10 ft 2 in
35.1 m 115 ft 2 in wingspan 11.25 m 36 ft 11 in
2 Turbofans (wing mounted) engines 1 x Bristol Siddeley Viper 201
21,000–23,000 lb thrust per engine 2,500 lb = 1,134 kg
42,000–46,000 lb total thrust 2,500 lb = 1,134 kg
63,100 kg 139,100 lb MTOW 4,173 kg 9,200 lb
6,390 km 3,451 nm range 1,448 km 782 nm
871 km/h 541 mph cruise speed 440 mph 708 km/h
Typical seating 2-class 100-120 capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.