| Manufacturer |
Zenair |
American Aviation Corp |
| Description |
The Zenair Zenith CH 200 and CH 250 are a family of Canadian single-engined homebuilt light aircraft. |
The Grumman American AA-1 series is a family of light, two-seat aircraft. |
| First Flight |
1970-03-22 |
1963-07-11 |
| Entry Into service |
|
1968-01-01 |
| Production End |
|
1978-01-01 |
| Designer |
Chris Heintz |
Jim Bede |
| Type |
|
Sport, personal and trainer aircraft |
| Length (m) |
6.25 |
5.87 |
| Height (m) |
2.11 |
2.07 |
| Cockpit Crew |
2 |
|
| Max Speed (km/h) |
236.5736 |
222 |
| Cruise Speed (km/h) |
209.2147 |
201 |
| Min Speed (km/h) |
85.2952 |
97 |
| Max Ceiling (m) |
4602.48 |
4191 |
| Rate of Climb (m/s) |
4.064 |
3.89 |
| Capacity Description |
|
one passenger |
| National Origin |
France |
|
| Number Built |
|
1820 |
| Powerplant Description |
1 × Continental O-200 air-cooled flat-four, 75 kW (100 hp) each |
1 × Lycoming O-235-C2C flat-four engine, 81 kW (108 hp) each |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Zenair_CH_200 |
en.wikipedia.org/wiki/Grumman_American_AA-1 |
| Flat Wing Span (m) |
7 |
7.46 |
| Flat Wing Area (m²) |
9.8 |
9.11 |
| Flat Wing Aspect Ratio |
5 |
|
| Aircraft Engine |
Continental O-200 |
Lycoming O-235 |
| Number of Engines |
1 |
1 |