Airbus A321-200 vs. North American BT-9

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Airbus A321-200 versus North American BT-9
44.51 m 146 ft 0 in length 8.79 m 28 ft 10 in
11.76 m 38 ft 7 in height 2.82 m 9 ft 3 in
35.8 m 117 ft 5 in wingspan 10.97 m 36 ft
2 GE CFM56-5B3 engines 1 x Wright R-975-3 radial engine
31,600 lbs thrust per engine Approximately 440 hp
63,200 lbs total thrust Approximately 440 hp
89,000 kg 196,200 lb MTOW 4,300 lb 1,950 kg
4,000 nmi 7,408 km range 917 km 495 nm
871 km/h 541 mph cruise speed 150 mph 241 km/h
185 to 220 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.