Technical Data

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