Douglas DC-4 / C-54
passenger
1942


     
   
     

 

     
   
     

Developed during WWII, the DC-4 was commandeered by the U.S. Army Air Forces in 1942 (as the C-54), delaying its use in commercial service until 1946.

After WWII, many many C-54s entered civil service, along with new production DC-4s. One interesting fact of the DC-4's design was that it was the first airliner to introduce a circular section, constant diameter fuselage, which made stretching the basic aircraft relatively simple.



Crew: 4
Passengers: 40-44
Engine: 4 x P+W R-2000-25, 1065kW
Wingspan: 35.8m
Length: 28.6m
Height: 8.4m
Wing area: 136.0m2
Start mass: 33140kg
Empty mass: 20000kg
Max speed: 450kph
Cruise speed: 365kph
Ceiling: 6900m
Range w/max.fuel: 6000km
Range w/max.payload: 2200km

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