| Manufacturer |
Zenair |
| Description |
The Zenair Zenith CH 200 and CH 250 are a family of Canadian single-engined homebuilt light aircraft. |
| First Flight |
1970-03-22 |
| Designer |
Chris Heintz |
| Length (m) |
6.25 |
| Height (m) |
2.11 |
| Cockpit Crew |
2 |
| Max Speed (km/h) |
236.5736 |
| Cruise Speed (km/h) |
209.2147 |
| Min Speed (km/h) |
85.2952 |
| Max Ceiling (m) |
4602.48 |
| Rate of Climb (m/s) |
4.064 |
| National Origin |
France |
| Powerplant Description |
1 × Continental O-200 air-cooled flat-four, 75 kW (100 hp) each |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Zenair_CH_200 |
| Flat Wing Span (m) |
7 |
| Flat Wing Area (m²) |
9.8 |
| Flat Wing Aspect Ratio |
5 |
| Aircraft Engine |
Continental O-200 |
| Number of Engines |
1 |