|
|
Span |
17 m |
Wing Area |
17,95 m² |
Wing aspect ratio |
16,1 |
Fuselage length |
8,35 m |
Cockpit width |
0,68 m |
Cockpit height, front |
0,90 m |
Cockpit height, rear |
0,90 m |
Height at tailplane |
1,55 m |
Empty mass |
ca. 495 kg |
Max take-off mass |
700 kg |
Wing loading (90 kg payload) |
32,6 kg/m² |
Wing loading (max.) |
39,0 kg/m² |
Wing loading (without engine, 85 kg payload) |
28,5 kg/m² |
Max. payload in Cockpit |
205 kg |
Maximum speed |
280 km/h |
Minimum sink (single-seated) |
0,65 m/s |
Glide ratio (@ 90 km/h) |
34 |
|
|
Engine Power |
56 PS (41 kW) |
Engine displacement |
294 cm³ |
Volume of tank |
26 liter |
| |
|
Take off distance on grass (max. take-off mass) |
ca. 250 m |
Climb rate (single seated) |
ca. 2,9 m/s |
Climb rate (double seated) |
ca. 2,7 m/s |
Cruising speed |
140 km/h |
Fuel consumption in full climb |
ca. 19 l/h |
Fuel consumption in cruise |
ca. 14 l/h |
Range (using saw-tooth method) |
ca. 500 km |
|
|
top
|