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Technical characteristics
AIRPLANE K-10 SWIFT DESCRIPTION Modification | 10 (02) | 10 (01) | | Wingspan | 8.5 m | 9.1 m | Weight without Balistic Recovery System
| 265 kg | 280 kg | | Engine | ROTAX 912 UL\ULS | | Engine power | 80 hp\100 hp | | Max speed | 225 km/h | 225 km/h | | Max speed with extended flaps | 120 km/h | 120 km/h | | Max range ability | 750 km | 900 km | | Speed at lift off | 80 km/h | 70 km/h | | Stalling speed(with extended flaps, engine with min gas) | 65 km/h | 58 km/h | | Running start/run | 130\90 m | 100/75 m | | Rate of climb | 5/7 m/sec | 6 m/sec | | Fuel tank capacity | 65 lt | 80 lt | | Baggage area | 300 lt | 360 lt | | Cruising speed (with engine 5500 rpm) | 180/200 km/h | 180 km/h | | Max Take-off mass | 450 kg | 575 kg | Load factors (at 450 kg)
| +7.5/-3.75 | +6.75/-3.37 |
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