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Technical data K10 Swift
Technical data
| Modification | K10 LSA | K10 ULM | Wingspan
| 9,1 m
| 8,5 m | Wing Area
| 11,8 sq.m. | 11,02 sq.m | Overall Length
| 6,235 m | 6,235 m | Cockpit Width
| 1,20 m | 1,20 m | Height
| 2,67 m | 2,67 m | Empty Weight
| 285 kg
| 265 kg | Maximum Take Off Weight
| 575 kg
| 472.5 kg | Loading
| + 4.7/-2.3 G
| + 4.7/-2.3 G
| Aerodynamic Efficiency
| 12 | 12 | Baggage area
| 360 lt | 300 lt | | Total Fuel Capacity | 80 lt
| 65 lt |
Flight Characteristics
Modification | K10 LSA | K10 ULM | | Powerplant | ROTAX 912 ULS | ROTAX 912 UL | Maximum speed in level flight (with engine 4800 rpm)
| 225 km/h | 225 km/h | Cruising speed
| 180 km/h | 165 km/h | Speed at lift off
| 70 km/h | 80 km/h | | Stalling speed | 58 km/h | 65 km/h | | Rate of climb | 6 m/sec | 4 m/sec | | Maximum altitude | 4000 m | 4000 m | Take off Roll Distance
| 100 m | 130 m | | Landing Distance | 75 m | 90 m | | Fuel Consumption | 14 lt/h | 12 lt/h | | Max range ability | 900 km | 750 km |
Three-view drawing of aircraft |
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