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| Aeroplane performances | 80 HP | 100 HP |
| Cruising speed (IAS) | 165 km/h (102mph) | km/h |
| Max. airspeed Vmax (IAS) | 180 km/h (112mph) | km/h |
| Stall speed | 65 km/h (40mph) | 65 km/h |
| Rate of climb (472,5 kg) | 5,0 m/s (985fpm) | 6,0 m/s (1181fpm) |
| Dimensions | ||
| Wing span | 9,45 m (31 ft) | |
| Length | 6,25 m (20.5 ft) | |
| Height | 2,20 m (7.22 ft) | |
| Wing area | 12,50 m² (134.5 sq ft) | |
| Empty weight inc. Recovery System | ||
| C42 A Competition | 256,0 kg | 260,0 kg |
| C42 A Champion | 251,0 kg | 255,0 kg |
| Payload* | ||
| C42 A Competition | 216,5 kg | 212,5 kg |
| C42 A Champion | 221,5 kg | 217,5 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. 700 km (435 miles) | |
| Length of takeoff run (grass) | 90 – 100 m | 75 – 85 m |
| Glide ratio | 11 | |
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