Douglas
C-74 Globemaster I

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

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 at 15:09 hrs. on 5 September 1945 at Long Beach with Ben O. Howard at the controls and lasted 79 minutes. 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 (2,420 kW) Pratt & Whitney R-4360-49 engines. The aircraft was 31 ft (9.4 m) longer than the C-54 Skymaster, and would be 24 ft (7.3 m) longer than the proposed C-118 Liftmaster.

The second built, 42-65403, c/n 13914, crashed during flight testing on 5 August 1946 at Torrance, California, when it lost a wing during an overload dive test. All four crew bailed out successfully. The fourth aircraft was diverted to a static test article at Wright Field, Ohio, up and virtually every component was tested to destruction between August 1946 and November 1948. This was done in order to determine the individual components' ability to withstand design loads. The fifth C-74 built was modified to be a prototype for the C-124 Globemaster II, which used the same wing as the C-74, but used a much larger fuselage. This newer aircraft quickly superseded the C-74 in service Wiki Link