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 |