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Boeing-Vertol H-47 Chinook
Design & Development

The original Model 107/YHC-1A was rejected by the Army as being too small for its needs. The YHC-1A was then evaluated by the US Marine Corps, and ordered as the HRB-1 (CH-46A after 1962).

The Army then ordered the larger Model 114/HC-1B. The pre-production Boeing Vertol YCH-1B made its initial hovering flight on September 21, 1961. In 1962 the HC-1B was redesignated the CH-47A under the 1962 United States Tri-Service aircraft designation system.

The Chinook is powered by two turboshaft engines, mounted on either side of the helicopter's rear end and connected to the rotors by driveshafts. The counter-rotating rotors eliminate the need for an anti-torque vertical rotor, allowing all power to be used for lift and thrust. If one engine fails, the remaining engine can drive both rotors.

A commercial model of the Chinook, the Boeing-Vertol Model 234, is used worldwide for logging, construction, fighting forest fires and supporting petroleum exploration operations. As of December 15, 2006 Columbia Helicopters, Inc of Aurora, Oregon has purchased the Type certificate of the Model 234 from Boeing. Currently the company is seeking FAA issuance of a Production Certificate to produce parts with eventual issuance of a PC to produce aircraft.

The Chinook was also built under license by Elicotteri Meridionali in Italy and Kawasaki in Japan.


Sources:
Wikipedia: H-47 Chinook

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