| Technical
data |
80 HP
|
100 HP
|
| Cruising speed (IAS) |
175 km/hr
|
185 km/hr
|
| Max. airspeed Vmax (IAS) |
185 km/hr
|
195 km/hr
|
| Stallspeed |
65 km/hr
|
65 km/hr
|
| Rate of climb (472,5 kg) |
5,0 m/s
|
6,5 m/s
|
| Wing span |
9,45 m
|
| Length |
6,38 m
|
| Height |
2,24 m
|
| Wing area |
12,5 qm
|
| Empty weight excl. recovery
system |
C42 B Champion
C42 B Competition
C42 B Club |
255 kg
260 kg
266 kg
|
| MTOW (Germany) * |
472,5 kg
|
| Payload * |
|
C42 B Champion
C42 B Competition
C42 B Club |
217,5 kg
212,5 kg
206,5 kg
|
Fuel tank volume
|
65 Liters
|
| Special typ Taiwan |
28 Liters
|
| Average consumption of fuel L/ hr |
10-13
|
10-14
|
| Range 50 Liters tank |
approx. 650 km
|
| Range 50+50 Liters tank |
approx. 1.300 km
|
| Length of takeoff run (grass) |
90-100 m
|
75-85 m
|
| Glide ratio |
11
|
* MTOW and
payload may be different according to
national law
State: 12.2003 - Technical changes reserved.
Technical informations are partially approximate values |
|
|
