| Zenith STOL CH 701 ✕ | |
|---|---|
| Manufacturer | Zenith Aircraft Company |
| Description | The Zenith STOL CH 701 and CH 750 are a family of light, two-place kit-built STOL aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario, based company, Zenair. |
| ICAO Code | CH70 |
| First Flight | 1986-01-01 |
| Entry Into service | 1986-01-01 |
| Designer | Chris Heintz |
| Type | Kit aircraft |
| Length (m) | 6.096 |
| Height (m) | 2.4384 |
| Max Speed (km/h) | 136.7942 |
| Cruise Speed (km/h) | 128.7475 |
| Min Speed (km/h) | 48.2803 |
| Max Ceiling (m) | 3657.6 |
| Rate of Climb (m/s) | 5.08 |
| Endurance (h) | 4.6 |
| National Origin | United States of America |
| Number Built | 870 |
| Powerplant Description | 1 × Rotax 912 four-cylinder liquid-cooled piston engine, 60 kW (80 hp) each |
| Status | In production |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Zenith_STOL_CH_701 |
| Flat Wing Span (m) | 8.2296 |
| Flat Wing Area (m²) | 11.3342 |
| Flat Wing Aspect Ratio | 5.98 |
| Wake Category | L |
| Aircraft Engine | Rotax 912 |
| Number of Engines | 1 |