C-12 Huron
Encyclopedia : C : C1 : C12 : C-12 Huron
| C-12 Huron | ||
|---|---|---|
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| Description | ||
| Role | Liaison, VIP transport, special operations, support | |
| Crew | 2 (pilot, copilot) + 8 passengers | |
| Dimensions | ||
| Length | 43 ft 9 in | 13.3 m |
| Wingspan | 54 ft 6 in | 16.61 m |
| Height | 15 ft | 4.6 m |
| Wing area | 303 ft² | 28.15 m² |
| Weights | ||
| Empty | 7,538 lb | 3,419 kg |
| Loaded | ||
| Maximum take-off | 12,500 lb | 5,670 kg |
| Powerplant | ||
| Engines | 2 Pratt & Whitney PW-PT61-42 turboprops | |
| Power | 850 hp each | 630 kW |
| Performance | ||
| Maximum speed | 339 mph | 545 km/h |
| Ferry range | 2,334 mi | 3,756 km |
| Service ceiling | 35,000 ft | 10,670 m |
| Rate of climb | ||
The C-12 Huron is the military version of the Beechcraft King Air, used by the United States Air Force, United States Army, and the United States Navy. These aircraft are used for various duties, including embassy support, medical evacuation, passenger and light cargo. The A, B, C, D and E models are based on the King Air A200, while the later versions are based on the B200.
The U.S. Navy version (C-12F) provides logistics support between Navy air stations. Powered by two PT-6A-42 turboprop engines, the C-12F can deliver a total payload of up to 4,215 lb (1,900 kg). The cabin can readily accommodate cargo, passengers or both. It is also equipped to accept litter patients in medical evacuation missions.
General characteristics
- Primary Function: Passenger and cargo airlift
- Contractor: Raytheon Aircraft Company (Formally Beech Aircraft)
- Unit Cost: $2 million
- Propulsion: Two Pratt & Whitney PT-6A-42 turboprop engines; 850 shaft horsepower (630 kW) each
- Length: 43 ft 10 in (13.3 m)
- Height : 15 ft (4.6 m)
- Weight: Max. gross, take-off: 15,000 lb (6,750 kg)
- Cruising Speed: Max.: 294 knots (334 mph, 544 km/h)
- Ceiling: 35,000 ft (10,700 m)
- Range: 1,974 nautical miles (3,658 km)
- Crew: Two
- Armament: None
- Date deployed: 1994
- Predecessor: Beechcraft C-6 Ute
- Successor: Cessna C-35 Citation
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