912 TI is a piston engine model used in aircraft.
Engine Family: piston
Cooling system: Liquid & air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1211 cubic-centimetre
Fuel grade: RON 95
Fuel type: Mogas
Max. continuous RPM: 5500
Max. continuous hp: 111 horsepower
Max. takeoff RPM: 5800
Max. takeoff hp: 128 horsepower
ICAO: GYRO
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