North American B-25 Mitchell vs. Canadair CL-415

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North American B-25 Mitchell versus Canadair CL-415
16.15 m 53 ft 0 in length 19.82 m 65 ft 0 in
5 m 16 ft 4 in height 8.66 m 28 ft 5 in
20.58 m 67 ft 6 in wingspan 28.6 m 93 ft 1
2 x Wright R-2600-92 Twin Cyclone engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
1,700 horsepower thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
3,400 horsepower total thrust 4,300 to 4,760 shaft horsepower
7,484 kg 16,500 lb MTOW 19,733 kg 43,525 lb
1,350 mi 1,175 nm range 1,600 km 864 nm
233 MPH 375 km/h cruise speed 290 km/h 180 mph
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.