100 - 300hp piston engine UL350i

50 - 100kgfor light aircraftfor ULM

This engine has all ready-to-fly features and has a perfect budget/quality ratio. As it supports Avgas, Mogas 97/98 but also Mogas 95 it can be used all over the world. Dual (redundant) electronic spark ignition (variable timing) Electronic multipoint fuel injection (pressure and temperature compensated) Electronic RPM limiter Direct propeller drive 5 bearing crankshaft with surface hardening treatment and additional large thrust bearing (ball bearing type) Single central camshaft Push rods, tappets and OHV (hydraulic compensators have not been used) Wet sump forced lubrication with integrated pressure regulator Ram air cooled cylinders and cylinder heads Integrated permanent magnet AC generator, external rectifier-regulator Electric starter Electric fuel pump and pressure regulator to eliminate vapor lock and facilitate starting even under adverse conditions Displacement - 3503 cc [213.77 cu in] Bore - 105.6 mm [4.157 in] Stroke - 100 mm [3.937 in] Compression Ratio - 8 : 1 Firing Order - 1 - 3 - 2 - 4 Direction of Rotation - Clockwise - seen from cockpit Maximum Torque (ISA conditions) - 305 Nm [225 ft.lb] @ 2400 rpm DC output - 30 Amp (+/- 15 Amp available above engine/fuel pump needs) Oil capacity - 2.5 L [0.66 US gal] Fuel - Regular unleaded automotive gasoline with min. 95 Octane RON (87 MON = 91 AKI) AVGAS 100LL may also be used if regular fuel is not available.