Flat Wing Area
19.7791 m²
Flat Wing Aspect Ratio
7.243
Cruise Speed
329.6557 km/h
Entry Into service
1968-07-01
Maximum Take-Off Weight
3.0731 t (paragliders: kg)
Total Fuel Capacity
537.5285
Maximum Range
2272.404 km
Pictures
No pictures yet for this family.
Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Beechcraft Duke |
3.0731 |
537.5285 |
2272.404 |
Similar airplanes
All data (25 fields)
- Name
- Beechcraft Duke
- Manufacturer
- Beechcraft
- Description
- The Beechcraft 60 Duke is an American-built twin-engine, piston-driven fixed-wing aircraft designed and produced by Beechcraft.
- First Flight
- 1966-12-29
- Entry Into service
- 1968-07-01
- Production End
- 1983-01-01
- Designer
- Beechcraft
- Type
- Light aircraft
- Length (m)
- 10.0584
- Height (m)
- 3.6576
- Cockpit Crew
- 1
- Max Seating
- 5
- Max Speed (km/h)
- 459.2956
- Cruise Speed (km/h)
- 329.6557
- Min Speed (km/h)
- 135.1959
- Max Ceiling (m)
- 9144
- Rate of Climb (m/s)
- 8.1331
- Capacity Description
- 5 passengers
- Number Built
- 596
- Powerplant Description
- 2 × Lycoming TIO-541-E1C4 turbocharged six-cylinder, horizontally opposed direct drive engines, 283 kW (380 hp) each
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Beechcraft_Duke
- Flat Wing Span (m)
- 11.8872
- Flat Wing Area (m²)
- 19.7791
- Flat Wing Aspect Ratio
- 7.243
- Number of Engines
- 2