Flat Wing Area
16.8154 m²
Flat Wing Aspect Ratio
7.973
Cruise Speed
292.6157 km/h
Entry Into service
1978-01-01
Maximum Take-Off Weight
1.769 t (paragliders: kg)
Total Fuel Capacity
378.5412
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 Duchess |
1.769 |
378.5412 |
1444.56 |
Similar airplanes
All data (26 fields)
- Name
- Beechcraft Duchess
- Manufacturer
- Beechcraft
- Description
- The Beechcraft Model 76 Duchess is an American twin-engined monoplane built by Beechcraft intended partly as a low cost introduction to twin-engine aircraft.
- First Flight
- 1974-09-01
- Entry Into service
- 1978-01-01
- Production End
- 1983-01-01
- Designer
- Beechcraft
- Type
- Four-seat cabin monoplane
- Length (m)
- 8.8392
- Height (m)
- 2.7432
- Cockpit Crew
- 1
- Max Seating
- 3
- Cruise Speed (km/h)
- 292.6157
- Min Speed (km/h)
- 111.1199
- Max Ceiling (m)
- 5989.32
- Rate of Climb (m/s)
- 6.3398
- Capacity Description
- 3 passengers
- Number Built
- 437
- Powerplant Description
- 2 × Lycoming O-360-A1G6D air-cooled flat-four engines, 134 kW (180 hp) each
- Primary Users
- Flight schools
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Beechcraft_Duchess
- Flat Wing Span (m)
- 11.5824
- Flat Wing Area (m²)
- 16.8154
- Flat Wing Aspect Ratio
- 7.973
- Aircraft Engine
- Lycoming O-360
- Number of Engines
- 2