| Specifications | C22 B | C22 C |
|---|---|---|
| Engine | Rotax 582 UL DCDI | Rotax 912 UL |
| Wingspan | 10.46 m | |
| Length | 5.60 m | |
| Height | 2.20 m | |
| Wing area | 15.70 m² | |
| Aspect ratio | 7.0 | |
| Empty mass (incl. rescue system) | 206 kg | 211 kg |
| Maximum take-off mass | 400 kg | 450 kg |
| Limit load factors | 4 g / −2 g | |
| Fuel capacity | 40 l / 50 l (optional) | |
| Take-off run | 120 m | 115 m |
| Take-off distance over 15 m obstacle | 200 m | 195 m |
| Rate of climb | 3.3 m/s | 3.7 m/s |
| Cruise speed | 100 km/h | 120 km/h |
| Never-exceed speed | 150 km/h | |
| Stall speed | 65 km/h | |
| Fuel consumption (cruise) | 10–13 l/h | 9 l/h |
| Range | 330 km | 440 km |