YT-120CC
Twin cylindersAir-cooledTwo-strokeCDI ignition with automatic advanceMixture lubricationPush and pull devices
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| Power | 11.22 hp / 8.25 kW |
|---|---|
| Static thrust (100 m altitude) | 26.5 kg |
| Static thrust (1800 m altitude) | 23.5 kg |
| Max take-off weight | 60 kg |
| Recommended propeller | 26*10; 26*12; 27*10; 28*10 |
| Bore × stroke | 45 mm × 35 mm |
| Displacement | 120 cc |
| Weight | 3.05 kg |
| Crankshaft | Three ball bearings |
| Speed range | 1300–6500 rpm |
| Fuel/oil mix ratio | 25:1–30:1 |
| Igniter supply voltage | 6.0–8.4 V DC |
| Generator | 600 W |
| Fuel consumption (carburetor) | 4.5 L/h |
| Fuel consumption (EFI) | 3.3 L/h |
| Dimensions (L×W×H) | 285 × 220 × 222 mm |