Specifications |
Primary Function | Passenger and cargo airlift |
Contractor | Raytheon Aircraft (Beech) |
Unit Cost | $2 million |
Propulsion | Two Pratt & Whitney PT-6A-42 turboprop engines; 850 shaft horsepower each |
Length | 43 feet 10 (13.3 meters) |
Height | 15 feet (4.57 meters) |
Weight | Max. gross, take-off: 15,000 lbs (6,750 kg) |
Cruising Speed | Max.: 294 knots (334 miles, 544 km, per hour) |
Ceiling | 35,000 feet (10,668 meters) |
Range | 1,974 nautical miles (3,658 km) |
Crew | Two |
Armament | None |
Date deployed | 1994 |
Variants | 200 (A100-1 (U-21J)), 200C, 200CT, 200T, A200 (C-12A) or (C-12C), A200C (UC-12B), A200CT (C-12D) or (FWC-12D) or (RC-12D) or (C-12F) or (RC-12G) or (RC-12H) or (RC-12K), or(RC-12P) B200C (C-12F) or (UC-12F) or (UC-12M), or (C-12R), 1900C (C-12J), |