North American BT-9 vs. Canadair CL-415

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North American BT-9 versus Canadair CL-415
8.79 m 28 ft 10 in length 19.82 m 65 ft 0 in
2.82 m 9 ft 3 in height 8.66 m 28 ft 5 in
10.97 m 36 ft wingspan 28.6 m 93 ft 1
1 x Wright R-975-3 radial engine engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 440 hp thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 440 hp total thrust 4,300 to 4,760 shaft horsepower
4,300 lb 1,950 kg MTOW 19,733 kg 43,525 lb
917 km 495 nm range 1,600 km 864 nm
150 mph 241 km/h cruise speed 290 km/h 180 mph
Pilot and one passenger 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.