ROTO 35 Vi
Engine displacement: ...................34,5 ccm
Max static engine thrust: .............9,5 kg
Bore .................................................39,5 mm
Engine weight: ...............................1520 g
Engine & ignition weight: .............1700 g
Arrangement of the engine: ........single cylinder
Cooling: ...........................................air-cooled
Lubrication: ....................................petrol 95 oct. + 2% oil
MAX RPM:........................................6800 rpm
Fuel system: ...................................Carburetor
Standard packaging:
1. ROTO 35 Vi ................................. 1 x
2. Ignition ROTO 35 Vi ................... . 1 x
3. Muffler ROTO STANDARD ...........1 x
4. Spark plug key CM6 .................... 1 x
Recommended airplanes models
Up to 3 m (9.10’)
Up to 14 kg (30.13 lb)
Recommended propeller
2 BLADE: 20-21/10