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 |