Douglas DC-2

DC-2
DC-2 PH-AJU Uiver came second in the MacRobertson Air Race
Role Passenger & military transport
Manufacturer Douglas Aircraft Company
First flight May 11, 1934
Introduced May 18, 1934
Primary users United States
Australia
Germany
United Kingdom
Number built 156
Developed from Douglas DC-1
Developed into Douglas DC-3

The Douglas DC-2 was a 14-seat, twin-propeller airliner produced by the American company Douglas Aircraft Corporation starting in 1934. It competed with the Boeing 247. In 1935 Douglas produced a larger version called the DC-3, which became one of the most successful aeroplanes in history.

Contents

Design and development

In the early 1930s, fears about the safety of wooden aircraft structures (responsible for the crash of a Fokker Trimotor) compelled the American aviation industry to develop all-metal types. With United Airlines having a monopoly on the Boeing 247, rival Transcontinental and Western Air issued a specification for an all-metal trimotor.

The response of the Douglas Aircraft Company was more radical. When it flew on July 1, 1933, the prototype DC-1 had a highly robust tapered wing, a retractable undercarriage, and only two 690 hp (515 kW) Wright radial engines driving variable-pitch propellers. It seated 12 passengers.

TWA accepted the basic design and ordered 20, with more powerful engines and seating for 14 passengers, as DC-2s. The design impressed a number of American and European airlines and further orders followed. Those for European customers KLM, LOT, Swissair, CLS and LAPE were assembled by Fokker in the Netherlands after that company bought a licence from Douglas.[1] Airspeed Ltd. took a similar licence for DC-2s to be delivered in Britain and assigned the company designation Airspeed AS.23, but although a registration for one aircraft was reserved none were actually delivered.[1] Another licence was taken by the Nakajima Aircraft Company in Japan; unlike Fokker and Airspeed, Nakajima built five aircraft as well as assembling at least one Douglas-built aircraft.[1] A total of 156 DC-2s were built.

Operational history

Although overshadowed by its ubiquitous successor, it was the DC-2 that first showed that passenger air travel could be comfortable, safe and reliable. As a token of this, KLM entered their first DC-2 PH-AJU Uiver (Stork) in the October 1934 MacRobertson Air Race between London and Melbourne. Out of the 20 entrants, it finished second behind only the purpose built de Havilland DH.88 racer Grosvenor House. During the total journey time of 90 h 13 min, it was in the air for 81 h, 10 min, and won the handicap section of the race. (The DH.88 finished first in the handicap section, but the crew was by regulations allowed to claim only one victory.)

Variants

DC-2A
Two civil DC-2s, powered by two Pratt & Whitney R-1690 "Hornet" radial piston engines.
DC-2B
Two DC-2s sold to LOT Polish Airlines, fitted with two 750 hp (560 kW) Bristol Pegasus VI radial piston engines.[2]

Modified DC-2s built for the United States Army Air Corps under several military designations:

XC-32
16-seat transport aircraft, one built,[3] later a flying command post,.
C-32A
Designation for 24 commercial DC-2s impressed at the start of World War II.[3]
C-33
Cargo transport aircraft powered by 750 hp R-1820-25 engines, with larger vertical tail surfaces, a reinforced cabin floor and a large cargo door in the aft fuselage, 18 built.[3]
YC-34
VIP transport, basically similar to XC-32, later designated C-34, 2 built.[4]
C-38
The first C-33 was modified with a DC-3 style tail section and two Wright R-1820-45 radial piston engines of 975 hp (727 kW) each. Originally designated C-33A but redesignated as prototype for C-39 variant, one built.[5]
C-39
A composite of DC-2 & DC-3 components, with C-33 fuselage and wings and DC-3 type tail, centre-section and undercarriage. Powered by two Wright R-1820-55 radial piston engines, of 975 hp (727 kW) each, 35 built.[6]
C-41
A single aircraft similar to the C-39, but with 1,200 hp (895 kW) Wright R-1820-21 engines, built as a VIP transport for General Hap Arnold, the US Army Air Corps Chief of Staff.[7] (The Douglas C-41A was a VIP version of the DC-3A)[8]
C-42
VIP transport, Powered by two Wright R-1820-53 radial piston engines, of 1,000 hp (746 kW) each, one built in 1939 for the commanding general, GHQ Air Force, plus two similarly-converted C-39s procured in 1943.[8]
R2D
One transport aircraft for the US Navy.
R2D-1
Four transport aircraft for the US Navy.

Operators

Civil operators

 Brazil
 Republic of China
 Czechoslovakia
 Finland
 Honduras
 Germany
 Japan
 Manchukuo
 Mexico
 Netherlands
 Poland
Spain Spanish Republic
 Switzerland
 United States
 Uruguay

Military operators

Douglas C-39 transport, the military version of the DC-2
 Argentina
 Australia
 Finland
 Germany
 Japan
Spain Spanish Republic
 United Kingdom
 United States

Survivors

DC-2 - c/n 1404
DC-2 - c/n 1368

There are currently no DC-2s in commercial service. However, several aircraft made it into the 21st century:

Specifications (DC-2)

General characteristics

Performance

See also

Related development

Comparable aircraft

Related lists

References

Notes
  1. 1.0 1.1 1.2 O'Leary, Michael. "Douglas Commercial Two." Air Classics magazine, May 2003 (online version at www.findarticles.com). Retrieved: March 1, 2010.
  2. Francillon 1979, p. 180.
  3. 3.0 3.1 3.2 Francillon 1979, p. 181.
  4. Francillon 1979, pp. 181–182.
  5. Francillon 1979, p. 182.
  6. Francillon 1979, pp. 182–183.
  7. Francillon 1979, p. 183.
  8. 8.0 8.1 Francillon 1979, p. 239.
  9. "Transportes Navales." histarmar.com. Retrieved: August 5, 2010.
  10. Francillon 1970, p. 499.
  11. "Douglas DC-2-118B." airliners.net.
  12. DC-2." Finnish Aviation Museum. Retrieved: August 5, 2010.
  13. "Accident description, 7 February 1951." aviation-safety.net. Retrieved: August 5, 2010.
  14. "DC-2." The Australian National Aviation Museum. Retrieved: August 5, 2010.
  15. United States Air Force Museum 1975, p. 24.
Bibliography
  • Francillon, René J. Japanese Aircraft of the Pacific War. London: Putnam, 1970. ISBN 0 370 00033 1.
  • Francillon, René J. McDonnell Douglas Aircraft since 1920. Longon:Putnam, 1979. ISBN 0-370-00050-1.
  • United States Air Force Museum Guidebook. Wright-Patterson AFB, Ohio: Air Force Museum Foundation, 1975.

External links