Douglas C-74 Globemaster
| C-74 Globemaster | |
|---|---|
 |
|
| C-74 Globemaster at Long Beach, California. | |
| Role | Strategic airlifter |
| Manufacturer | Douglas Aircraft Company |
| First flight | 5 September 1945 |
| Retired | 1969 (last operational flight) |
| Status | Retired – 1959 (military), 1969 (civilian) |
| Primary users |
United States Army Air Forces United States Air Force |
| Produced | 1945–1947 |
| Number built | 14 (one converted to C-124 prototype) |
| Developed into | C-124 Globemaster II |
The Douglas C-74 Globemaster was a United States heavy-lift cargo aircraft built by the Douglas Aircraft Company in Long Beach, California. The aircraft was developed after the Japanese attack on Pearl Harbor. The long distances across the Atlantic and, especially, Pacific oceans to combat areas indicated a need for a transoceanic heavy-lift military transport aircraft. Douglas Aircraft Company responded in 1942 with a giant four-engined design. Development and production modifications issues with the aircraft caused the first flight to be delayed until 5 September 1945, and production was limited to 14 aircraft when the production contract was canceled following V-J Day.
Although not produced in large numbers, the C-74 did fill the need for a long-range strategic airlifter, in which the subsequent Douglas C-124 Globemaster II was used by the Air Force for many years.
The Douglas Aircraft Company began studies at their Santa Monica division in early 1942 for a transport capable of fulfilling the global logistical needs of the U.S. military. Its "C-74 Project Group" used their company's DC-4 as a basis and concentrated on enlarging its capabilities. The group's design philosophy was to build a "no-frills" aircraft able to accommodate much of the Army's large equipment including light tanks, two 105-millimeter (4.1 in) howitzers with their towing vehicles, two angle bulldozers, and smaller utility vehicles. This became the Douglas Model 415 and a cost-plus contract worth more than $50 million was signed 25 June 1942 for 50 aircraft and one static test article. There were no XC- or YC-74 models produced.
This first flight of a C-74 occurred on 5 September 1945. The first C-74, 42-65402, was airborne just two months after it rolled off the assembly line. At the time of its first flight, the C-74 was the largest landplane to enter production, with a maximum weight of 172,000 lb (78,000 kg). It was able to carry 125 soldiers or 48,150 lb (21,840 kg) of cargo over a range of 3,400 mi (5,500 km). Perhaps the most notable feature of the C-74 was its cockpit arrangement with separate canopies over the pilot and copilot; the same arrangement was used for the XB-42 Mixmaster. This arrangement was unpopular with flight crews, however, and the aircraft were retrofitted with a more conventional arrangement. During the life of the aircraft, the radial engines were also upgraded to 3,250 hp (2,424 kW) Pratt & Whitney R-4360-49 engines. The aircraft was 31 feet longer than the C-54 Skymaster, and would be 24 feet longer than the proposed C-118 Liftmaster.
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