de Havilland Canada DHC-2 Beaver vs. Canadair CL-415

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de Havilland Canada DHC-2 Beaver versus Canadair CL-415
13.56 m 44 ft 6 in length 19.82 m 65 ft 0 in
5 m 16 ft 5 in height 8.66 m 28 ft 5 in
16.56 m 54 ft 4 in wingspan 28.6 m 93 ft 1
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 6,200 hp (4,624 kW) total total thrust 4,300 to 4,760 shaft horsepower
24,200 lb 10,977 kg MTOW 19,733 kg 43,525 lb
2,535 km 1,369 nm range 1,600 km 864 nm
228 mph 367 km/h cruise speed 290 km/h 180 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.