Stamo 1400A is a piston engine model used in aircraft.
Engine Family: piston
Bore: 80 millimetre
Compression ratio: 6
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1490 cubic-centimetre
Dry weight: 53 kilogram
Fuel grade: 80/87
Fuel type: Avgas
Max. continuous RPM: 3100
Max. continuous hp: 42 horsepower
Max. takeoff RPM: 3200
Max. takeoff hp: 45 horsepower
Stroke: 74 millimetre
ICAO: NIPR
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