| Douglas DC-4 |
| Role |
Cargo, Commercial Transport |
| Entered service |
1938 |
| Manufacturer |
Douglas |
The designation DC-4 was used by Douglas Aircraft Company when developing the DC-4E as a large, four-engined type to complement its forthcoming DC-3 design. It was intended to fulfill United Airlines' requirement for a long-range passenger airliner. The DC-4E (E stands for experimental) emerged as a 40-passenger airliner with a fuselage of unusually wide cross-section for its day and a triple fin tail unit, similar to that later used by Lockheed on its Constellation.
The DC-4E first flew on June 7, 1938, and was used by United Air for test flights. But the type proved to be ahead of its time - it was complicated to maintain and uneconomical to operate. The sponsoring airlines, Eastern and United, decided to ask instead for a smaller and simpler derivative but before the definitive DC-4 could enter service the outbreak of the Second World War meant production was channelled to the US Army Air Force and the type given the military designation C-54.
The DC-4 had a notable innovation in that its nose-wheel landing gear allowed it to introduce a fuselage of constant cross-section. This lent itself to easy stretching into the later DC-6 and DC-7. The original DC-4 entered production in 1941 and 1,162 were ordered by the United States services. Nine military versions were produced but Douglas continued to develop the type in preparation for a return to airline services when peace returned. But the type's sales prospects were hit by the offloading of 500 wartime C-54s, and R5D US Navy, machines on to the civil market.
Douglas built just 74 new-build aircraft before production switched to the upgraded DC-6. All were unpressurised, as were the DC-4s built by Victory Aircraft, later Canadair, in Canada with Rolls-Royce Merlin engines. Canadair did build the pressurised DC-4M Argonaut for BOAC.
The DC-4 proved a popular type and several remain in service today, particularly in the USA where it proved popular as charter/freight plane.
Douglas DC-4 Specifications
- Country: United States of America
- Designation: DC-4/C-54
- Gross weight: 73,000 lb (33,112 kg)
1 External links
Specifications (variant described)
General characteristics
- Crew: 3
- Capacity:
- Length: 93 ft 11 in (28.6 m)
- Wingspan:117 ft 6 in (35.8 m)
- Height: 27 ft 6.25 in (8.39 m)
- Wing area: m² ( ft²)
- Empty: 40,806 lb (18,509 kg)
- Loaded: kg ( lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 4 x Pratt & Whitney R-2000 reciprocating, 1,450 hp (1,081 kW)
Performance
- Maximum speed: 280 mph (450 km/h)
- Range: 4,250 miles (6,839 km)
- Service ceiling: 22,300 ft (6,800 m)
- Rate of climb: m/min ( ft/min)
- Wing loading: kg/m² ( lb/ft²)
- Power/mass:
External links
Boeing McDonnell Douglas page on DC-4
Last updated: 07-31-2005 21:33:18
