912 UL is a piston engine model used in aircraft.
Engine Family: piston
Bore: 79.5 millimetre
Compression ratio: 9
Control system: Dual channel FADEC
Cooling system: Liquid & air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1211 cubic-centimetre
Dry weight: 57 kilogram
Fuel grade: RON 90
Fuel type: Mogas
Height: 0.38 metre
Length: 0.59 metre
Max. continuous RPM: 5500
Max. continuous hp: 78 horsepower
Max. takeoff RPM: 5800
Max. takeoff hp: 80 horsepower
Stroke: 61 millimetre
Width: 0.58 metre
ICAO: PIAT
View Type →ICAO: CH60
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