Military


C-12 Huron

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)
Range1,974 nautical miles (3,658 km)
Crew Two
ArmamentNone
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),
    • Production
    Model Type Army USAF USN
    200C-12L / RU-21J3
    A200 C-12A 6030
    A200 C-12C 14
    A200 C-12E 29
    A200C UC-12B 66
    A200CT C-12D 246
    A200CT RC-12D 13
    A200CT RC-12G 3
    A200CT RC-12H 6
    A200CT RC-12K 9
    A200CT RC-12N 1515
    A200CT RC-12P 99
    A200CT RC-12Q 33
    B200 C-12F 2046
    B200C C-12R 2929
    B200C RC-12F 2
    B200C RC-12M 2
    B200C UC-12F 10
    B200C UC-12M 10
    Totals 2088290
    C-12E are conversions







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