| Aeroplane performances | 80 HP | 100 HP |
| Cruising speed (IAS) | 175 km/h (109mph) | 185 km/h (115mph) |
| Max. airspeed Vmax (IAS) | 190 km/h (118mph) | 198 km/h (123mph) |
| Stallspeed | 65 km/h (40mph) | 65 km/h (40mph) |
| Rate of climb (472,5 kg) | 5,0 m/s (985 fpm) | 6,0 m/s (1181fpm) |
| Dimensions | ||
| Wing span | 8,71 m (28.6ft) | |
| Length | 6,38 m (21ft) | |
| Height | 2,20 m (7.22ft) | |
| Wing area | 11,90 m² (128 sq ft) | |
| Empty weight inc. Recovery System | ||
| C42 C Competition | 278,0 kg | 282,0 kg |
| C42 C Champion | 273,0 kg | 277,0 kg |
| Payload* | ||
| C42 C Competition | 194,5 kg | 190,5 kg |
| C42 C Champion | 199,5 kg | 195,5 kg |
| Max. take off weight | 472,5 kg | |
| Consumption/Cruising range | ||
| Fuel tank volume | 65 Litre (14.3 Imp gal) | |
| Average consumption of fuel L/hr | 10 – 13 | 10 – 14 |
| Range 65 Litres tank | ca. 780 km (485 miles) | |
| Length of takeoff run (grass) | 90 – 100 m | 75 – 85 m |
| Glide ratio | 11 | |
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