S2400UL is a piston engine model used in aircraft.
Engine Family: piston
Bore: 94 millimetre
Compression ratio: 7.9
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2332 cubic-centimetre
Dry weight: 75 kilogram
Fuel grade: RON 95
Fuel type: Mogas
Max. continuous RPM: 3000
Max. continuous hp: 89 horsepower
Max. takeoff RPM: 3500
Max. takeoff hp: 99 horsepower
Stroke: 84 millimetre
