Airbus A220-300 vs. North American BT-9

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Airbus A220-300 versus North American BT-9
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 4,300 lb 1,950 kg
6,297 km 3,402 nm range 917 km 495 nm
Mach 0.82 101,3 km/h cruise speed 150 mph 241 km/h
Typical seating 2-class 120-150 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.