M-14V26V1 is a piston engine model used in aircraft.
Engine Family: piston
Max. continuous RPM: 2650
Max. continuous hp: 265 horsepower
Bore: 105 millimetre
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 9
Displacement: 10161 cubic-centimetre
Dry weight: 255 kilogram
Fuel type: Avgas
Max. takeoff RPM: 2900
Max. takeoff hp: 358 horsepower
Stroke: 130 millimetre
Length: 1.11 metre
Width: 0.99 metre
Height: 0.99 metre
