Aeroplane performances |
80 HP |
100 HP |
Cruising speed (IAS) |
187 km/h (116mph) |
197 km/h (122mph) |
Max. airspeed Vmax (IAS) |
202 km/h (125mph) |
210 km/h (13omph) |
Stallspeed |
65 km/h (40mph) |
65 km/h (40mph) |
Rate of climb (472,5 kg) |
5,0 m/s (985fpm) |
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 CS Competition |
280,5 kg |
284,5 kg |
C42 CS Champion |
275,5 kg |
279,5 kg |
Payload* |
C42 CS Competition |
192,0 kg |
190,5 kg |
C42 CS Champion |
197,0 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. 800 km (497 miles) |
Length of take off run (grass) |
90 – 100 m |
75 – 85 m |
Glide ratio |
11 |