Cessna CH-1 Skyhook / YH-41
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The first prototype flew in July 1953, receiving FAA type certification in 1955. In 1955 a CH-1 successfully landed on, and took off from Pike's Peak, Colorado, at a height of 4300 metres. By May 1957 the Skyhook held three world altitude records in several weight classes by climbing to close on 30,000 feet.
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The Army's evaluation of the YH-41 showed it to be an excellent high altitude performer, though the type's limited payload and rather complex maintenance requirements precluded its large scale procurement by the Army. The ten YH-41’s were eventually relegated to miscellaneous flight test duties, most having to do with high-altitude helicopter operations, and in 1962 the surviving aircraft were redesignated NH-41A’s. ![]()
In 1960 the Skyhook was introduced to the civil market, becoming the first helicopter to receive single pilot IFR approval from the FAA. Production began in 1961 with three CH-1A (four seat) versions being offered at the same price, US$79,000.00. The price, US$20,000.00 more than Cessna's most expensive fixed wing single at the time, proved the stumbling block. Competing Hiller E4 and Bell 47J models were available US$10,000.00 cheaper. After several million dollars and a decade of development, Cessna only sold 23 before ceasing production in 1962 and, in an unprecedented move, purchased them all back and scrapped them; a move followed by the United States Army shortly therafter. Only one survives, at the United States Army Museum at Fort Rucker, Alabama. ![]() CH-1
Engine: 1 x Continental FSO-470-A, 260hp Rotor diameter: 10.66m Fuselage length: 9.78m Fuselage width: 1.63m Height: 2.53m Gross weight: 1360kg Empty weight: 896kg Max. speed: 195km/h Cruising speed: 160km/h Rate of climb: 351m/min Range: 432km Number of seats: 2
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