Scarab Junior 40 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 107.95 millimetre
Compression ratio: 5.2
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 5
Displacement: 4933 cubic-centimetre
Dry weight: 108 kilogram
Fuel grade: 54
Fuel type: Avgas
Max. continuous RPM: 2050
Max. continuous hp: 90 horsepower
Max. takeoff RPM: 2050
Max. takeoff hp: 90 horsepower
Stroke: 107.95 millimetre
ICAO: -
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