The Douglas DC-5 was a 16-to-22-seat, twin-engine propeller airliner intended for shorter routes than the Douglas DC-3 or DC-4. The prototype, built at El Segundo, California, with Wright Cyclone engines, first flew on February 20, 1939, and the type was the first airliner to combine shoulder wings with tricycle landing gear, a layout still common in turboprop airliners and military transports. By the time it entered commercial service in 1940 many airlines were cancelling orders and Douglas was already converting to wartime military production, so only five civilian DC-5s were built, although a limited number of military variants followed, including personnel carriers for the Navy.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Douglas DC-5 (Wikipedia)
Of Make
Source Douglas DC-5 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Douglas DC-5 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
With the Douglas Aircraft Company already converting to World War II military production
Originated In
Also in Geography Atlas: where this subject originated.
Source Douglas DC-5 (Wikipedia)Lead, country of originQuote, Lead, country of origin
was built at El Segundo, California
Sources
1. Douglas DC-5 (Wikipedia)
Design and development
The aircraft made its first flight on February 20, 1939
Lead
twin-engine propeller aircraft
Specifications
Wright GR-1820-G102A Cyclone 9-cylinder air-cooled radial piston engine
Specifications, mass
Empty weight: 13,674 lb (6,202 kg)
Specifications, maximum mass
Gross weight: 20,000 lb (9,072 kg)
Lead, manufacturer
With the Douglas Aircraft Company already converting to World War II military production
Lead, country of origin
was built at El Segundo, California
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