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Douglas DC-2 ✕ Farman F.270 ✕
Manufacturer Douglas Aircraft Corporation Farman
Description The Douglas DC-2 is a retired American 14-passenger twin-engined airliner which was produced by the Douglas Aircraft Company starting in 1934. The Farman F.270 was a prototype French bomber/torpedo-bomber designed and built by the Farman Aviation Works for the French Air Force.
ICAO Code DC2
First Flight 1934-05-11 1933-01-01
Entry Into service 1934-05-18
Designer Douglas Aircraft Corporation Farman
Length (m) 18.5928 18.5
Height (m) 4.8768 6
Max Seating 14
Max Speed (km/h) 337.9622 250
Cruise Speed (km/h) 305.7754
Max Ceiling (m) 6842.76 7500
Rate of Climb (m/s) 5.08
Armament 6 × 7.7mm (0.303in) machine-gun (two each in nose, dorsal and ventral positions); up to 1000kg (2205lb) or one torpedo
Capacity Description 14 passengers
National Origin France
Number Built 192
Powerplant Description 2 × Wright GR-1820-F52 Cyclone 9-cylinder air-cooled radial piston engine, 578 kW (775 hp) each 2 × Gnome-Rhône 14K 14-cylinder radial piston engine, 597 kW (800 hp) each
Primary Users Transcontinental & Western Air (TWA), KLM, Pan American Airways
Status Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Douglas_DC-2 en.wikipedia.org/wiki/Farman_F.270
Flat Wing Span (m) 25.908 26
Flat Wing Area (m²) 87.236 152
Wake Category M
Aircraft Engine Gnome-Rhône Mistral Major
Number of Engines 2 2