Consolidated B-24 Liberator vs. de Havilland Canada DHC-2 Beaver

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Consolidated B-24 Liberator versus de Havilland Canada DHC-2 Beaver
20.42 m 67 ft 0 in length 13.56 m 44 ft 6 in
5.49 m 18 ft height 5 m 16 ft 5 in
33.53 m 110 ft wingspan 16.56 m 54 ft 4 in
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines 2 x Armstrong Siddeley Double Mamba turboprop engines
1,200 hp, 1,200 hp each thrust per engine Approximately 3,100 hp (2,312 kW) each
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust Approximately 6,200 hp (4,624 kW) total
26,580 kg 58,600 lb MTOW 24,200 lb 10,977 kg
2,850 mi 2,481 nm range 2,535 km 1,369 nm
175 mph 282 km/h cruise speed 228 mph 367 km/h
8,000 pounds capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.