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General Characteristics Primary function: Light-lift utility Contractor: Bell Helicopter Co. Power Plant: Two Pratt and Whitney T400-CP-400 turboshaft engines Maximum Gross Weight: 10,500 pounds (4,763 kilograms) Range: 300-plus miles Ceiling: 15,000 feet (4,572 meters); 10,000 feet (3,048 meters) for gross weights above 10,000 pounds (4,536 kilograms) Maximum Speed: 149 mph (130 knots) Cruise Speed: 103-115 mph (90-100 knots) Length: 57 feet, 3 inches (17.44 meters) Width: 9 feet, 5 inches (2.87 meters) Height: 12 feet, 10 inches (3.9 meters) Diameter of Main Rotor: 48 feet (14.63 meters) Diameter of Tail Rotor: 8 feet, 6 inches (2.6 meters) Crew: Pilot with co-pilot and flight engineer, depending upon mission Date Deployed: 1970 Inventory: Active force, 62; Reserve, 0; ANG, 0 |
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