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2625 01

2625 01 is a piston engine model used in aircraft.

Specifications

Engine Family: piston

Bore: 76 millimetre

Compression ratio: 9.5

Cooling system: Liquid

Cylinder configuration: Inline

Cylinder count: 2

Displacement: 625 cubic-centimetre

Dry weight: 23 kilogram

Fuel grade: RON 95

Fuel type: Mogas

Height: 0.41 metre

Length: 0.35 metre

Max. continuous RPM: 6250

Max. continuous hp: 52 horsepower

Max. takeoff RPM: 6250

Max. takeoff hp: 52 horsepower

Stroke: 69 millimetre

Width: 0.24 metre

Manufacturer

Solo

Compatible Aircraft Types

Compatible Aircraft Models