Douglas Dc-4 Article Index for
Douglas
Shopping
DC-4
Articles about
Douglas Dc-4
Website Links For
Douglas
 

Information About

Douglas Dc-4






The DC-4 is a four-engined airliner developed by the Douglas Aircraft Company . It served extensively during the Second World War in a military role, and after the war for civilian airlines.


DEVELOPMENT

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 Air Lines ' requirement for a long-range passenger airliner. The DC-4E (E stands for experimental) emerged as a 52-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 Lines 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 United States Army Air Forces and the type given the military designation C-54 . Additional versions used by the US Navy were designated '''R5D'''. The first aircraft, a C-54, flew from Clover Field in Santa Monica, California on February 14 , 1942 .


PRODUCTION

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 '''. 1,163 DC-4s were built for the United States military services between 1942 and 1946. Douglas continued to develop the type during the war in preparation for a return to airline services when peace returned. However, the type's sales prospects were hit by the offloading of 500 wartime C-54s and R5Ds onto the civil market.

Douglas built just 74 new-build aircraft before production ceased on August 9 , 1947 . Pressurization was available as an option, but all civilian DC-4s were built unpressurised.


DERIVATIVES

DC4M North Star/Argonaut. 71 DC-4s were built by Canadair under the designations '''North Star''', '''DC-4M''', '''C-4''', and '''C-5'''. With the exception of the single C-5, these were all powered by Rolls-Royce Merlin engines and 51 of them were pressurized. The Royal Canadian Air Force , Trans-Canada Air Lines , Canadian Pacific Air Lines and BOAC operated these aircraft, the latter under the type name "Argonaut".

Starting in 1959, 20 DC-4s found new life as ATL-98 Carvairs . The Carvair was designed to carry 22 passengers and 5 automobiles. This was accomplished by extending the fuselage, moving the cockpit above the fuselage, adding a side-opening nose, and enlarging the vertical stabilizer to offset the larger forward fuselage. These planes served as flying ferries well into the seventies.

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.


Other versions

  • DC-4-1009 Postwar passenger model. This civil model could carry up to 86 passengers.

  • DC-4-1037 Postwar freight model.



Specifications (DC-4-1009)

  • Country: United States of America

  • Designation: DC-4/C-54/R5D



General characteristics

  • Crew: 4

  • Capacity: Up to 86 passengers

  • Length: 93 ft 10 in (28.6 m)

  • Wingspan:117 ft 6 in (35.8 m)

  • Height: 27 ft 6 in (8.38 m)

  • Wing area: 1,460ft² (135.6 m²)

  • Empty: 43,300 lb (19,640 kg)

  • Loaded: 63,500 lb (28,800 kg)

  • Maximum takeoff: 73,000 lb (33,100 kg)

  • Powerplant: 4 × Pratt & Whitney R-2000 reciprocating, 1,450 hp (1,081 kW)



Performance

  • Maximum speed: 280 mph (450 km/h)

  • Cruising speed: 227 mph (365 km/h)

  • Range: 4,250 miles (6,839 km)

  • Service ceiling: 22,300 ft (6,800 m)

  • Wing loading: 43.5 lb/ft² (212.4 kg/m²)

  • Power loading: 10.9 lb/hp (6.6 kg/kW)



REFERENCES

  • Francillon, RenĂ© (1979). ''McDonnell Douglas Aircraft Since 1920: Volume I.'' London: Putnam. ISBN 0-87021-428-4

  • Yenne, Bill (1985). ''McDonnell Douglas: A Tale of Two Giants.'' Greenwich, CT: Bison Books. ISBN 0-517-442876

  • Pearcy, Arthur (1995). ''Douglas Propliners: DC-1 - DC-7.'' Shrewsbury: Airlife Publishing. ISBN 1-85310-261X



EXTERNAL LINKS



RELATED CONTENT

  has Sequence yes
  has Relations yes
  links yes
  has Lists yes
  see Also no