Maximum Take-Off Weight
0.998 t (paragliders: kg)
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Zenith STOL CH 801 |
0.998 |
600 |
Similar airplanes
All data (20 fields)
- Name
- Zenith STOL CH 801
- Manufacturer
- Zenith Aircraft Company
- Description
- The Zenith STOL CH 801 is a four-seat sport STOL aircraft developed by Chris Heintz and available in kit form from the Zenith Aircraft Company.
- ICAO Code
- CH80
- Designer
- Chris Heintz
- Type
- STOL aircraft
- Length (m)
- 7.47
- Cruise Speed (km/h)
- 170
- Min Speed (km/h)
- 63
- Rate of Climb (m/s)
- 6.2
- Capacity Description
- three passengers and 1050 lb (475 kg) useful load
- National Origin
- United States of America
- Number Built
- 160
- Powerplant Description
- 1 × Lycoming O-360, 135 kW (181 hp) each
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Zenith_STOL_CH_801
- Flat Wing Span (m)
- 8.23
- Flat Wing Area (m²)
- 15.5
- Wake Category
- L
- Aircraft Engine
- Lycoming O-360
- Number of Engines
- 1