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Start | Douglas | C-124 Globemaster II



Douglas C-124 Globemaster II


General information


ManufacturerDouglas
ModelC-124 Globemaster II
ModificationС-124С
CountryUSA
Years1949
TypeTransport aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan53.1 m
Length39.8 m
Height14.7 m
Wing area233.1 m2
Zero fuel weight-
Empty weight45888 kg
Maximum takeoff weight88200 kg
Normal takeoff weight84000 kg
Flight duration-
Engine4 Pratt Whitney R-4360-63
Power4 x 3748 HP
Thrust-
Maximum speed520 km/h
Cruising speed429 km/h
Rate of climb-
Practical range11000 km
Service ceiling8000 m
Hovering ceiling-
Crew8
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