V-3420-19 (B8) is a piston engine model used in aircraft.
Engine Family: piston
Fuel grade: 130
Bore: 139.7 millimetre
Compression ratio: 6.65
Cooling system: Liquid
Cylinder configuration: Double V @ 60°
Cylinder count: 24
Displacement: 56044 cubic-centimetre
Dry weight: 1440 kilogram
Fuel type: Avgas
Height: 1.03 metre
Length: 6.65 metre
Max. continuous RPM: 2600
Max. continuous hp: 2100 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 2600 horsepower
Stroke: 152.4 millimetre
Width: 1.52 metre
