912 ULS is a piston engine model used in aircraft.
Engine Family: piston
Bore: 84 millimetre
Compression ratio: 10.8
Control system: Dual channel FADEC
Cooling system: Liquid & air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1352 cubic-centimetre
Dry weight: 58 kilogram
Fuel grade: RON 95
Fuel type: Mogas
Height: 0.38 metre
Length: 0.59 metre
Max. continuous RPM: 5500
Max. continuous hp: 93 horsepower
Max. takeoff RPM: 5800
Max. takeoff hp: 99 horsepower
Stroke: 61 millimetre
Width: 0.58 metre
ICAO: CH60
View Type →ICAO: CH65
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View Type →ICAO: FK9
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View Type →ICAO: WT9
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