| Zenith STOL CH 701 ✕ | Albatros L 69 ✕ | |
|---|---|---|
| Manufacturer | Zenith Aircraft Company | Albatros Flugzeugwerke |
| 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. | The Albatros L 69 was a two-seat German parasol monoplane racing and training aircraft of 1925. |
| ICAO Code | CH70 | |
| First Flight | 1986-01-01 | 1925-01-01 |
| Entry Into service | 1986-01-01 | |
| Designer | Chris Heintz | R. Schubert |
| Type | Kit aircraft | Racer |
| Length (m) | 6.096 | 6.1 |
| Height (m) | 2.4384 | 2.57 |
| Max Speed (km/h) | 136.7942 | 170 |
| Cruise Speed (km/h) | 128.7475 | |
| Min Speed (km/h) | 48.2803 | |
| Max Ceiling (m) | 3657.6 | 4000 |
| Rate of Climb (m/s) | 5.08 | 4.2 |
| Endurance (h) | 4.6 | 2 |
| National Origin | United States of America | |
| Number Built | 870 | 4 |
| Powerplant Description | 1 × Rotax 912 four-cylinder liquid-cooled piston engine, 60 kW (80 hp) each | 1 × Siemens-Halske Sh 12, 80 kW (107 hp) each |
| Status | In production | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Zenith_STOL_CH_701 | en.wikipedia.org/wiki/Albatros_L_69 |
| Flat Wing Span (m) | 8.2296 | 8.06 |
| Flat Wing Area (m²) | 11.3342 | 14 |
| Flat Wing Aspect Ratio | 5.98 | |
| Wake Category | L | |
| Aircraft Engine | Rotax 912 | Siemens-Halske Sh 12 |
| Number of Engines | 1 | 1 |