Douglas DC-3

Length
19.7 m
Flat Wing Span
29 m
Height
5.16 m
Flat Wing Area
91.6953 m²
Flat Wing Aspect Ratio
9.17
Max Seating
32
Cruise Speed
338.9157 km/h
Max Speed
412.9956 km/h
Max Ceiling
7071.36 m
Number of Engines
2
First Flight
1935-12-17
Entry Into service
1936-01-01
Number Built
607
Total Fuel Capacity
3111.608
Maximum Range
2537.24 km

Pictures

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Aircraft Weight Variants

Aircraft Total Fuel Capacity Maximum Range (km)
Douglas DC-3 3111.608 2537.24

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All data (27 fields)
Name
Douglas DC-3
Manufacturer
Airtech Canada
Description
The Douglas DC-3 is a propeller-driven airliner that was manufactured by the Douglas Aircraft Company.
ICAO Code
DC3
First Flight
1935-12-17
Entry Into service
1936-01-01
Production End
1942-01-01
Designer
Airtech Canada
Length (m)
19.7
Height (m)
5.16
Max Seating
32
Max Speed (km/h)
412.9956
Cruise Speed (km/h)
338.9157
Min Speed (km/h)
125.9
Max Ceiling (m)
7071.36
Rate of Climb (m/s)
5.7912
Capacity Description
21–32 passengers
National Origin
United States of America
Number Built
607
Powerplant Description
2 × Pratt & Whitney R-1830-S1C3G Twin Wasp 14-cyl. air-cooled two row radial piston engine, 895 kW (1200 hp) each
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Douglas_DC-3
Flat Wing Span (m)
29
Flat Wing Area (m²)
91.6953
Flat Wing Aspect Ratio
9.17
Wake Category
M
Number of Engines
2