S2100ULT is a piston engine model used in aircraft.
Engine Family: piston
Bore: 90.5 millimetre
Compression ratio: 6.5
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2161 cubic-centimetre
Dry weight: 76 kilogram
Fuel grade: RON 98
Fuel type: Mogas
Max. continuous RPM: 2800
Max. continuous hp: 99 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 109 horsepower
Stroke: 84 millimetre
