The C-124 Globemaster II was developed by the Douglas Aircraft Company from 1947 until 1949. It started as a prototype based on C-74 Globemaster and built on acquired lessons throughout the Berlin Blockade. On November 27, 1949, the Globemaster II took to the air for the first time. In May 1950, the delivery of the C-124A commenced. The C-124C version was equipped with an APS-42 weather radar with its distinctive thimble radome.
The aircraft was fitted with four Pratt and Whitney R-4360-63A Wasp Major. It was a 28-cylinder, four-row radial piston engine rated at 3,800 horsepower each with water or alcohol injection. It also had a 3-bladed Curtiss Model C634S-C402 fully-feathering reversible-pitch constant-speed propeller. The C-124 was designed with two sizeable clamshell doors, a ramp hydraulic actuation system located in the nose, and a freight elevator below the rear fuselage. The aircraft could carry a cargo load of 31,100 kg.
The cargo bay was equipped with two overhead hoists that could lift 3,600 kg of load each. The cargo version could bear heavy vehicles such as trucks, as well as guns, tanks, and large equipment.
The passenger version could accommodate two hundred fully equipped troops or one hundred and twenty-seven litter patients with their attendants. The C-124 Globemaster II was the single aircraft during its time that could transport fully assembled outsized equipment like tanks and bulldozers.
The Globemaster II had an exterior length of 39.8 meters, an exterior height of 8.2 meters, a tail height of 14.74 meters, and a fuselage diameter of 4.5 meters. The wheelbase is 9.1 meters, the wingspan is 53.06 meters, and the wing area is 232.8 square meters.
The aircraft had a maximum speed of 264 knots at 20,800 feet, a cruise speed of 200 knots, and a range of 3,500 nautical miles with 1,830 kg of payload. It could fly up to 21,800 feet and could climb at a rate of 760 feet per minute.
Want More of This?
We'll send you our latest and best content straight to your inbox
