The Douglas DC-1 was the first of the Douglas Commercial airliners and was built as a single aircraft. Douglas designed it for Transcontinental and Western Air, which wanted an all-metal transport after the 1931 crash of a Fokker trimotor with a wooden wing led regulators to restrict wooden wings on passenger airliners. The result was a low-wing, twin-engined monoplane with a crew of two and seats for twelve passengers, able to take off and fly safely on one engine. It first flew on July 1, 1933, and in February 1934 it crossed the United States in a record 13 hours 5 minutes. TWA ordered twenty of the developed DC-2, and the DC-1 itself ended its days in Spain, where it was wrecked in a forced landing in 1940.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Douglas DC-1 (Wikipedia)
Of Make
Source Douglas DC-1 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Douglas DC-1 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
the first model of the famous American DC (Douglas Commercial) commercial transport aircraft series
Originated In
Also in Geography Atlas: where this subject originated.
Source Douglas DC-1 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
the first model of the famous American DC (Douglas Commercial) commercial transport aircraft series
Sources
1. Douglas DC-1 (Wikipedia)
Operational history
The prototype first flew on July 1, 1933
Lead
commercial transport aircraft series
Specifications
Wright SGR-1820F3 Cyclone 9-cylinder air-cooled radial piston engines
Operational history, status
damaged beyond repair
Specifications, mass
Empty weight: 11,780 lb (5,343 kg)
Specifications, maximum mass
Gross weight: 17,500 lb (7,938 kg)
Lead, manufacturer
the first model of the famous American DC (Douglas Commercial) commercial transport aircraft series
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