S2200UL is a piston engine model used in aircraft.
Engine Family: piston
Bore: 92 millimetre
Compression ratio: 8.8
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2234 cubic-centimetre
Dry weight: 66 kilogram
Fuel grade: RON 98
Fuel type: Mogas
Max. continuous RPM: 2700
Max. continuous hp: 79 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 84 horsepower
Stroke: 84 millimetre
