Aeroplane performances |
80 HP |
100 HP |
Cruising speed (IAS) |
170 km/h(105mph) |
180 km/h (112mph) |
Max. airspeed Vmax (IAS) |
185 km/h (114mph) |
193 km/h (120mph) |
Stall speed |
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 |
9,45 m (31ft) |
Length |
6,38 m (21ft) |
Height |
2,20 m (7.22ft) |
Wing area |
12,50 m² (134.5 sq ft) |
Empty weight inc. Recovery System |
C42 A Competition |
271,5 kg |
275,5 kg |
C42 A Champion |
266,5 kg |
270,5 kg |
Payload* |
C42 A Competition |
201,0 kg |
197,0 kg |
C42 A Champion |
206,0 kg |
202,0 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. 750 km (466 miles) |
Length of takeoff run (grass) |
90 – 100 m |
75 – 85 m |
Glide ratio |
11 |