Douglas DC-2

Airplanes

Length

18.5928 m

Flat Wing Span

25.908 m

Height

4.8768 m

Flat Wing Area

87.236 m²

Max Seating

Cruise Speed

305.7754 km/h

Max Speed

337.9622 km/h

Max Ceiling

6842.76 m

Number of Engines

First Flight

1934-05-11

Entry Into service

1934-05-18

Number Built

192

Maximum Range

1609.344 km

Pictures

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Aircraft	Maximum Range (km)
Douglas DC-2	1609.344

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Huff-Daland XB-1		18.7	25.9		Compare
Farman F.270	Gnome-Rhône Mistral Major	18.5	26		Compare
SPCA 20		18.62	26.22		Compare
Douglas DC-1		18.288	25.908	12	Compare
Dornier Do 23		18.8	25.6		Compare
Dornier Do 11		18.8	26.3		Compare

All data (24 fields)

Name: Douglas DC-2
Manufacturer: Douglas Aircraft Corporation
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.
ICAO Code: DC2
First Flight: 1934-05-11
Entry Into service: 1934-05-18
Designer: Douglas Aircraft Corporation
Length (m): 18.5928
Height (m): 4.8768
Max Seating: 14
Max Speed (km/h): 337.9622
Cruise Speed (km/h): 305.7754
Max Ceiling (m): 6842.76
Rate of Climb (m/s): 5.08
Capacity Description: 14 passengers
Number Built: 192
Powerplant Description: 2 × Wright GR-1820-F52 Cyclone 9-cylinder air-cooled radial piston engine, 578 kW (775 hp) each
Primary Users: Transcontinental & Western Air (TWA), KLM, Pan American Airways
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Douglas_DC-2
Flat Wing Span (m): 25.908
Flat Wing Area (m²): 87.236
Wake Category: M
Number of Engines: 2