UL260iSA is a piston engine model used in aircraft.
Engine Family: piston
Bore: 105.6 millimetre
Compression ratio: 9.1
Control system: FADEC
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2592 cubic-centimetre
Dry weight: 63 kilogram
Fuel grade: RON 98
Fuel type: Mogas
Height: 0.47 metre
Length: 0.55 metre
Max. continuous RPM: 2800
Max. continuous hp: 95 horsepower
Max. takeoff RPM: 3300
Max. takeoff hp: 107 horsepower
Stroke: 74 millimetre
Width: 0.66 metre
