Douglas
DC-3
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Photo: Robert Deering 1977
Smithsonian National Air and Space Museum
Washington, DC
The Douglas DC-3 is an American fixed-wing propeller-driven airliner, the speed and range of which revolutionized air transport in the 1930s and 1940s. Its lasting impact on the airline industry and World War II makes it one of the most significant transport aircraft ever made. The major military version was designated the C-47 Skytrain, of which more than 10,000 were produced. Many DC-3 / C-47s are still used in all parts of the world.

The DC-3 was the culmination of a development effort that originated out of an inquiry from Transcontinental and Western Airlines (TWA) to Donald Douglas. TWA's rival in transcontinental air service, United Airlines, was inaugurating service with the Boeing 247 and Boeing refused to sell any 247s to other airlines until United's order for 60 aircraft had been filled.  TWA asked Douglas to design and build an aircraft that would enable TWA to compete with United. Douglas' resulting design, the 1933 DC-1, was promising, and led to the DC-2 in 1934. While the DC-2 was a success, there was still room for improvement.

The DC-3 was the result of a marathon telephone call from American Airlines CEO C. R. Smith to Donald Douglas, during which Smith persuaded a reluctant Douglas to design a sleeper aircraft based on the DC-2 to replace American's Curtiss Condor II biplanes. Douglas agreed to go ahead with development only after Smith informed him of American's intention to purchase twenty aircraft. The new aircraft was engineered by a team led by chief engineer Arthur E. Raymond over the next two years, and the prototype DST (for Douglas Sleeper Transport) first flew on December 17, 1935 (the 32nd anniversary of the Wright Brothers' flight at Kitty Hawk, North Carolina). A version with 21 passenger seats instead of the sleeping berths of the DST was also designed and given the designation DC-3. There was no prototype DC-3; the first DC-3 built followed seven DSTs off the production line and was delivered to American.

The amenities of the DC-3 and DST popularized air travel in the United States. With only three refueling stops, eastbound transcontinental flights crossing the U.S. in approximately 15 hours became possible. Westbound trips took 171/2 hours due to prevailing headwinds—still a significant improvement over the competing Boeing 247. During an earlier era, such a trip would entail short hops in slower and shorter-range aircraft during the day, coupled with train travel overnight.

A variety of radial engines were available for the DC-3 throughout the course of its development. Early-production civilian aircraft used Wright R-1820 Cyclone 9s, but later aircraft (and most military versions) used the Pratt & Whitney R-1830 Twin Wasp which offered better high-altitude and single engine performance. Three DC-3S Super DC-3s with Pratt & Whitney R-2000 Twin Wasps were built in the late 1940s.

Total production of all derivatives was 16,079.  More than 400 remained in commercial service in 1998. Production was as follows:

607 civil variants of the DC-3.
10,048 military C-47 derivatives were built at Santa Monica, California, Long Beach, California, and Oklahoma City.
4,937 were built under license in Russia as the Lisunov Li-2 (NATO reporting name: Cab).
487 Mitsubishi Kinsei-engined aircraft were built under license by Showa and Nakajima in Japan from 1940 -1945, as the L2D2–L2D5 Type 0 transport (Allied codename Tabby).

Production of civil DC-3s ceased in 1942, military versions were produced until the end of the war in 1945. In 1949, a larger, more powerful Super DC-3 was launched to positive reviews; however, the civilian market was flooded with second-hand C-47s, many of which were converted to passenger and cargo versions and only three were built and delivered the following year. The prototype Super DC-3 served the US Navy with the designation YC-129 alongside 100 C-47s that had been upgraded to the Super DC-3 specification.

From the early 1950s, some DC-3s were modified to use Rolls-Royce Dart engines, as in the Conroy Turbo Three. Other conversions featured Armstrong Siddeley Mamba and Pratt & Whitney PT6A turbines.

SPECIFICATIONS: PERFORMANCE:
Span:  95 ft 2 in (29.0 m) Maximum speed:  200 kn; 370 km/h (230 mph) at 8,500 ft (2,590 m)
Length:  64 ft 8 in (19.7 m) Cruising speed:  180 kn; 333 km/h (207 mph)
Height:  16 ft 11 in (5.16 m) Range: 
Empty Weight:  16,865 lb (7,650 kg) Service ceiling:  23,200 ft (7,100 m)
Gross Weight:  25,199 lb (11,430 kg)  
Crew:  2 with 21–32 passengers
Engines:  2 × Wright R-1820 Cyclone 9-cyl. air-cooled radial piston engine, 1,100 hp (820 kW) each
   
SOURCE:  Wikipedia