TECHNICAL DATA
Displacement
cc
230.8
Bore
mm
70
Stroke
mm
60
Compression Ratio
10/1
Power
Hp
33
kW
24
RPM
8.000
Weight of the engine ready to fly Kg
19.3
Static thrust
over 90 Kg
Lamellar intake with WALBRO WB39 carburetor
Aluminium cylinder with Nikasil ceramic coating
Exhaust resonance system
Poly-V belt reduction
Electronic ignition
Electric starter
Alternator for recharge battery in fly
Flying consumption at 5000 RPM, 3 liters/hour
Premix two stroke oil gasoline, 2,5% oil by volume to leaded fuel, 3% oil by volume to unleaded fuel
REDUCTION RATIO AVAIABLE
1:230 Crown gear 129 mm / Pinion 56 mm
1:234 Crown gear 129 mm / Pinion 55 mm
1:242 Crown gear 129 mm / Pinion 53,5 mm
1:3 Crown Gear 138 mm /Pinion 44 mm
