de Havilland Canada DHC-2 Beaver vs. Douglas C-54 Skymaster

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de Havilland Canada DHC-2 Beaver versus Douglas C-54 Skymaster
13.56 m 44 ft 6 in length 28.60 m 93 ft 10 in
5 m 16 ft 5 in height 8.38 m 27 ft 6 in
16.56 m 54 ft 4 in wingspan 35.81 m 117 ft 6 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 4 x Pratt & Whitney R-2000 Twin Wasp radial engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 1,200 to 1,450 horsepower (895 to 1,080 kW)
Approximately 6,200 hp (4,624 kW) total total thrust 4,800 to 5,800 horsepower
24,200 lb 10,977 kg MTOW 29,484 kg 65,000 lb
2,535 km 1,369 nm range 6,500 km 3,510 nm
228 mph 367 km/h cruise speed 340 km/h 211 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity Up to 50 passengers or 28,500 lb cargo
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.