Douglas DC-4

Passenger Turbo Props

ICAO aircraft code DC4

Manufacturer Douglas Aircraft Co.

Country United States

The Douglas DC-4 is an American four-engined (piston), propeller-driven airliner developed by the Douglas Aircraft Company.

Specifications

Full description

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Douglas DC-4 specifications

General

ICAO aircraft code

DC4

Manufacturer

Douglas Aircraft Co.

Manufactured

1942 - 1947

Country

United States

Aircraft performance

Engine:

4x Pratt & Whitney R-2000-2SD13-G Twin Wasp
Piston

Power:

1,450 HP

Max Cruise Speed:

240 Kts
444 Km/h

Travel range:

2,900 Nm
5,371 Kilometers

Service Ceiling:

22,300 feet

Rate of Climb:

1200 feet / minute
6.10meter / second

Weight & dimensions

Max Take Off Weight:

33,112 Kg
72,999 lbs

Max Landing Weight:

28,803 Kg
63,499 lbs

Max Payload:

9,980 Kg
22,002 lbs

Fuel Tank Capacity:

2,868 gallon
10,857 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Douglas DC-4

The Douglas DC-4 is an American four-engined (piston), propeller-driven airliner developed by the Douglas Aircraft Company. Military versions of the plane, the C-54 and R5D, served during World War II, in the Berlin Airlift and into the 1960s. From 1945, many civil airlines operated the DC-4 worldwide.