| 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),
|
| Production |
| Model | Type | Army | USAF | USN |
| 200 | C-12L / RU-21J | 3 |
| A200 | C-12A | 60 | 30 |
| A200 | C-12C | 14 |
| A200 | C-12E | | 29 |
| A200C | UC-12B | | | 66 |
| A200CT | C-12D | 24 | 6 |
| A200CT | RC-12D | 13 |
| A200CT | RC-12G | 3 |
| A200CT | RC-12H | 6 |
| A200CT | RC-12K | 9 |
| A200CT | RC-12N | 15 | | 15 |
| A200CT | RC-12P | 9 | | 9 |
| A200CT | RC-12Q | 3 | | 3 |
| B200 | C-12F | 20 | 46 |
| B200C | C-12R | 29 | | 29 |
| B200C | RC-12F | | | 2 |
| B200C | RC-12M | | | 2 |
| B200C | UC-12F | | | 10 |
| B200C | UC-12M | | | 10 |
| Totals | | 208 | 82 | 90 |
| C-12E are conversions |
|
