TDA CR 2.0 16V is a piston engine model used in aircraft.
Engine Family: piston
Bore: 83 millimetre
Compression ratio: 16
Control system: Dual FADEC
Cooling system: Liquid
Cylinder configuration: Inline
Cylinder count: 4
Displacement: 1955 cubic-centimetre
Dry weight: 219 kilogram
Fuel type: Diesel
Height: 0.66 metre
Length: 0.86 metre
Max. continuous RPM: 3800
Max. continuous hp: 190 horsepower
Max. takeoff RPM: 3800
Max. takeoff hp: 215 horsepower
Stroke: 90.4 millimetre
Width: 0.65 metre
