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<!--BEGIN SPECIFICATIONS--> CH-47 Chinook Specifications Primary Function: Medium-lift helicopter Contractor: Boeing Crew: Cockpit-crew seats: 2 Cabin-troop seats/litters: 33/24 Unit Cost: N/A Powerplant Two Textron Lycoming T55-L-712 turboshafts each rated at 3,750 shp for takeoff and 3,000 shp for coninuous running Dimensions Length: 98ft 10.75 in Rotor Diameter: 60 feet (18.29 m) each -- CH-47D Height: 18 ft 11 in Weights Empty: 22,379 lb Maximum Takeoff: 50,000 lb Performance Speed: 159 mph (cruising) Ceiling: 22,100 ft Range: N/A Armament N/A <!--END SPECIFICATIONS--> <!--BEGIN ACHIEVEMENTS--> CH-47 Chinook Achievements During Desert Storm the CH-47D often provided the only means of transportation to shift large numbers of personnel, equipment, and supplies quickly. <!--END ACHIEVEMENTS--> <!--BEGIN FEATURES--> <!-- CH-47 Chinook Features --> <!--END FEATURES--> <!--BEGIN BACKGROUND--> <!-- CH-47 Chinook Background --> <!--END BACKGROUND-->
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