Flat Wing Area
28.1496 m²
Entry Into service
1974-01-01
Maximum Take-Off Weight
5.6699 t (paragliders: kg)
Total Fuel Capacity
2555.91
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Beechcraft C-12 Huron |
5.6699 |
2555.91 |
2685.4 |
Similar airplanes
All data (21 fields)
- Name
- Beechcraft C-12 Huron
- Manufacturer
- Beechcraft
- Description
- The Beechcraft C-12 Huron is the military designation for a series of twin-engine turboprop aircraft based on the Beechcraft Super King Air and Beechcraft 1900.
- Entry Into service
- 1974-01-01
- Designer
- Beechcraft
- Type
- Military utility aircraft
- Length (m)
- 13.1064
- Height (m)
- 4.572
- Cockpit Crew
- 1
- Max Seating
- 13
- Max Speed (km/h)
- 535.2275
- Max Ceiling (m)
- 10668
- Rate of Climb (m/s)
- 12.446
- Capacity Description
- 13 passengers
- Powerplant Description
- 2 × Pratt & Whitney Canada PT6A-42 turboprop engines, 634 kW (850 hp) each
- Primary Users
- United States Air Force, United States Army , United States Marine Corps , United States Navy
- Status
- Active service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Beechcraft_C-12_Huron
- Flat Wing Span (m)
- 16.4592
- Flat Wing Area (m²)
- 28.1496
- Number of Engines
- 2