Airbus A220-100 vs. North American BT-9

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Airbus A220-100 versus North American BT-9
35.0 m 114 ft 10 in length 8.79 m 28 ft 10 in
11.5 m 37 ft 9 in height 2.82 m 9 ft 3 in
35.1 m 115 ft 2 in wingspan 10.97 m 36 ft
2 Turbofans (wing mounted) engines 1 x Wright R-975-3 radial engine
21,000–23,000 lb thrust per engine Approximately 440 hp
42,000–46,000 lb total thrust Approximately 440 hp
63,100 kg 139,100 lb MTOW 4,300 lb 1,950 kg
6,390 km 3,451 nm range 917 km 495 nm
871 km/h 541 mph cruise speed 150 mph 241 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.