L2400 DT is a piston engine model used in aircraft.
Engine Family: piston
Bore: 97 millimetre
Compression ratio: 8
Cooling system: Liquid & air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2424 cubic-centimetre
Dry weight: 86 kilogram
Fuel grade: RON 98
Fuel type: Mogas
Height: 0.43 metre
Length: 0.69 metre
Max. continuous RPM: 3000
Max. continuous hp: 114 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 129 horsepower
Stroke: 82 millimetre
Width: 0.79 metre
