Logo

2625 02

2625 02 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: 24 kilogram

Fuel grade: RON 95

Fuel type: Mogas

Height: 0.39 metre

Length: 0.35 metre

Max. continuous RPM: 6600

Max. continuous hp: 63 horsepower

Max. takeoff RPM: 6600

Max. takeoff hp: 63 horsepower

Stroke: 69 millimetre

Width: 0.25 metre

Manufacturer

Solo

Compatible Aircraft Types

Compatible Aircraft Models