| Performance and Dimensions
|
S 6 |
S 6-RT |
| MTOW |
850 kg |
850 kg |
| empty weight |
603 kg |
619 kg |
| total payload |
247 kg |
231 kg |
| Bombardier-Rotax engine 4 cyl. 4 stroke |
912 S |
914 F |
| MTOP |
73.5 kW |
84.5 kW |
| MCP |
69.0 kW |
73.5 kW |
| fuel capacity standard |
70 L |
70 L |
| fuel capacity long range |
n.a |
140 L |
| wing span |
18,00 m |
18,00 m |
| wing span folded |
7,20 m |
7,20 m |
| aspect ratio |
18,60 - |
18,60 - |
| length |
8,52 m |
8,52 m |
| height |
2,45 m |
2,45 m |
| landing gear |
fixed |
retractable |
| main wheel |
380×150 |
380×150 |
| nose wheel |
300×100 |
300×100 |
| wheel track |
2,00 m |
2,00 m |
| wheel base |
2,00 m |
2,00 m |
| best glide ratio |
33:1 |
39:1 |
| airspeed at best glide ratio |
113 km/h |
119 km/h |
| min. sink rate (empty weight + 70kg) |
0,85 m/s |
0,73 m/s |
| min. wing loading (empty weight + 70kg) |
37,5 kg/m² |
38,4 kg/m² |
| max. wing loading |
45,9 kg/m² |
48,8 kg/m² |
| max. rate of climb at MSL (with MTOP) |
4,73 m/s |
5,8 m/s |
| rate of climb at MCP (with MTOW) |
4,44 m/s |
5,1 m/s |
| cruising speed at MCP at MSL |
267 km/h |
280 km/h |
| cruising speed at 55% MCP at MSL |
214 km/h |
240 km/h |
| fuel consumption at MCP |
25,0 l/h |
25,0 l/h |
| fuel consumption at 55% MCP |
14,5 l/h |
14,5 l/h |
| range at 55% MCP at MSL long range version |
n.a. |
2,400 km |
|
|
All numbers are subject to change. |
|
|
