The CD-230 to CDR-285 is a family of four-stroke 4-cylinder, air/oil-cooled, horizontally opposed, direct-drive piston aircraft engines with turbocharger and direct injection. The engine has a maximum continuous power of 265 HP @ 2500 RPM or 287 HP @ 2700 RPM in a rotorcraft application.
Certified fuels
Jet-A, Jet-A1, TS-1, No 3 Jet Fuel
Displacement
4976 cm³304 in³
Power
172 to 211kW234 HP to 287 HP
Maximum Rated RPM
2200 to 2700 RPM
Bore
126 mm4.96 in
Stroke
100 mm3.94 in
Compression ratio
15:1
Height
676.4 mm26.63 in
Width
926.3 mm36.47 in
Length
860.7 mm33.89 in
Dry Weight
198.8 kg438.3 lbs
Cruise Fuel Consumption
44.44 l/hr 11.7 gal/hr
Proposed Time Between Overhaul (TBO)
2000 to 2400 hrs or 12 years