The CH-47D ended up being the result of June 1976 agreement for a modernized Chinook.The improvements included a redesigned cockpit to cut back pilot workload, an enhanced trip control system, and improved avionics. The Chinook has two tandem three-bladed counter-rotating fiberglass rotors. The CH-47D is powered by two Allied Signal Engines T55-L-712 3750 shp turboshaft engines and it has a maximun rate of 163 miles per hour. The CH-47D made its very first trip in-may 1979. The CH-47D carrys two times force of a CH-47A and has now improved performance. The CH-47D can run during the night as well as in most climate conditions. The CH-47D has an air-to-air refueling probe. The Chinook can accommodate a multitude of interior payloads, including automobiles, artillery pieces, 33 to 44 troops, or 24 litters plus two medical attendants. The "D" model can hold up to 26,000 pounds externally. The CH-47D has three cargo hooks: a center (main) connect and two extra hooks fore and aft for the main hook Engine: 2 Lycoming T-55-L-714turboshaft, 3,750 shp each Rotor Diameter: 60 ft Fuselage Length: 51 ft general Length: 99 ft Height: 18 ft 7 in Empty body weight: 22,452 lb Max Takeoff body weight: 50,000 lb Max Speed: 185 miles per hour Ceiling: 17,000 ft number: 1,250 kilometers Crew: 2
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