DOUGLAS C-54 Civil Aircraft Model Details

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General Information of DOUGLAS C-54

Developed From : Douglas DC-4

Introduction : 1942

Manufacturer : Douglas Aircraft Company

Number Built : 1170

Primary Users : United States Army Air Forces; United States Navy; United States Air Force

Produced : 1942–1947

Retired : 1975

Role : Military transport aircraft

General characteristics of DOUGLAS C-54

Capacity : 50 troops

Crew : 4

Empty Weight : 38,930 lb (17,660 kg)

Height : 27 ft 6 in (8.38 m)

Length : 93 ft 10 in (28.6 m)

Loaded_Weight : 62,000 lb (28,000 kg)

Max Takeoff Weight : 73,000 lb (33,000 kg)

Powerplant : 4 × Pratt & Whitney R-2000-9 radial engines, 1,450 hp (1,080 kW) each

Wing Area : 1,460 ft² (136 m²)

Wingspan : 117 ft 6 in (35.8 m)

Performance of DOUGLAS C-54

Cruise Speed : 190 mph (165 kn, 310 km/h)

Maximum Speed : 275 mph (239 kn, 442 km/h)

Power/Mass : 0.094 hp/lb (160 W/kg)

Range : 4,000 mi (6,400 km)

Service Ceiling : 22,300 ft (6,800 m)

Wing Loading : 42.5 lb/ft² (207 kg/m²)

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