Douglas
Douglas DC-2
The Douglas DC‑2, introduced in 1934 by the Douglas Aircraft Company, was a landmark twin‑engine airliner that reshaped commercial aviation during the interwar era. Born from the success of the DC‑1 prototype, the DC‑2 incorporated a more powerful Pratt & Whitney R‑985 Wasp Junior radial engine on each wing, a sleek all‑metal monocoque fuselage, and a retractable landing gear system that reduced drag and increased speed. With a cruising velocity of roughly 210 mph, a range of about 1,085 miles and seating for 14‑17 passengers, the aircraft offered a blend of reliability, comfort, and operational efficiency previously unseen on a regular schedule. Its debut on routes such as the New York–Chicago–Los Angeles corridor demonstrated superior performance over contemporary biplanes, prompting airlines worldwide to replace older fleets. The DC‑2 also proved its versatility in military service, being adapted as a transport and reconnaissance platform for several air forces. Its most celebrated achievement came in 1934 when a DC‑2 named “the “Flagship of the Air” won the MacRobertson Air Race from London to Melbourne, outperforming more advanced competitors and cementing its reputation. The DC‑2’s design principles directly informed the development of the iconic DC‑3, making it a pivotal stepping stone in the evolution of modern air transport.
Classification
Production & History
- Units Produced
- 198
Design & Classification
- Country of Origin
- Manufacturer
- Douglas
- Military Designation
- C-32A
- Engine
- R-1820
- Operator
-
Swissair Trans World Airlines KLM
- Wikidata ID
- Q15428008