C85-12 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 103.18 millimetre
Compression ratio: 6.3
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 3081 cubic-centimetre
Dry weight: 82 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2275
Max. continuous hp: 85 horsepower
Max. takeoff RPM: 2275
Max. takeoff hp: 85 horsepower
Stroke: 92.08 millimetre
ICAO: C120
View Type →ICAO: C140
View Type →ICAO: ERCO
View Type →ICAO: L8
View Type →ICAO: PAUL
View Type →ICAO: GC1
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View Type →ICAO: J4
View Type →ICAO: J5
View Type →ICAO: PA11
View Type →ICAO: J3
View Type →ICAO: J5
View Type →ICAO: M308
View Type →ICAO: J3
View Type →ICAO: PA11
View Type →ICAO: SKYR
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