S2100-1-AS1 (SA2100-H1S) is a piston engine model used in aircraft.
Engine Family: piston
Bore: 90 millimetre
Compression ratio: 8.6
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2136 cubic-centimetre
Dry weight: 69 kilogram
Fuel grade: RON 98
Fuel type: Mogas
Max. continuous RPM: 2700
Max. continuous hp: 72 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 79 horsepower
Stroke: 84 millimetre
ICAO: SF25
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