DOUGLAS DC-4E Civil Aircraft Model Details

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General Information of DOUGLAS DC-4E

Developed Into : Douglas DC-4; Nakajima G5N

First Flight : June 7, 1938[1]

Manufacturer : Douglas Aircraft Company

Number Built : 1[3]

Primary Users : United Airlines[2]; Imperial Japanese Airways

Role : Experimental airliner

General characteristics of DOUGLAS DC-4E

Capacity : 42 passengers

Crew : three

Empty Weight : 42,564 lb (19,307 kg)

Gross Weight : 61,500 lb (27,896 kg)

Height : 24 ft 6 in (7.48 m)

Length : 97 ft 7 in (29.74 m)

Max Takeoff Weight : 66,500 lb (30,164 kg)

Powerplant : 4 × Pratt & Whitney R-2180-S1A1-G Twin Hornet 14-cyl. two-row air-cooled radial piston engines, 1,450 hp (1,080 kW) each

Propellers : 3-bladed metal variable-pitch propellers

Wing Area : 2,155.01 sq ft (200.207 m2)

Wingspan : 138 ft 3 in (42.14 m)

Performance of DOUGLAS DC-4E

Cruise Speed : 200mph; 174kn (322km/h)

Maximum Speed : 245mph; 213kn (394km/h) at 7,000ft (2,134m)

Power/Mass : 0.0943 hp/lb (4.8kW/kg)

Range : 2,200mi (1,912nmi; 3,541km)

Rate Of Climb : 1,175ft/min (5.97m/s)

Service Ceiling : 22,900ft (6,980m)

Wing Loading : 28.5lb/sqft (139kg/m2)

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