Bombardier CRJ1000 vs. North American BT-9

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Bombardier CRJ1000 versus North American BT-9
39.1 m 128 ft 5 in length 8.79 m 28 ft 10 in
7.5 m 24 ft 7 in height 2.82 m 9 ft 3 in
26.2 m 86 ft wingspan 10.97 m 36 ft
2 GE CF34-8C5A1 turbofans engines 1 x Wright R-975-3 radial engine
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine Approximately 440 hp
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust Approximately 440 hp
41,640 kg 91,800 lb MTOW 4,300 lb 1,950 kg
3,004 km 1,623 nm range 917 km 495 nm
515 mph 829 km/h cruise speed 150 mph 241 km/h
100 (common) 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.