T-2000-M1 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 90.5 millimetre
Compression ratio: 8.7
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2117 cubic-centimetre
Dry weight: 79 kilogram
Fuel grade: 100/130
Fuel type: Avgas
Max. continuous RPM: 3000
Max. continuous hp: 73 horsepower
Max. takeoff RPM: 3400
Max. takeoff hp: 77 horsepower
Stroke: 78.4 millimetre
Length: 0.67 metre
Width: 0.76 metre
Height: 0.45 metre
ICAO: RF10
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