CD200 ‒ Series

  • Continental® continues its leadership in advanced technology by offering a line of Jet-A Diesel engines to meet the needs of a growing global market. Diesel engines offer distinctive advantages as aircraft engines. A diesel cycle engine, like our AvGas engines, is designed for outstanding durability and reliability, making it suitable for aviation applications. Diesel engines, by design, operate continuously in an efficient manner and therefore do not require leaning. The emission of lead, nitrogen oxides, carbon hydride, or carbon monoxide is reduced significant. The CD-200 series concept is a horizontally opposed, air/oil cooled, four cylinder, turbocharged engine. The full line of Jet-A diesel engines is another example of Continental's commitment  to the advancement of general aviation technology.

    Continental Motors CD200 Diesel Engine

    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 265p @ 2500rpm or 287 hp @ 2700rpm 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 liters/hr 11.7 gallons/hr

    Time Between Replacement

    Currently 2000 to 2400 hrs

    CD-200 Details

    Model #CYL  Rated Power
    @RPM
    Bore x Stroke Displacement Dry Weight   Certified Fuel
    Grade
    Compression
    Ratio
    Recommend.
    TBO
    CD-230 4 172 kW @ 2200 126 x 100 mm 4968 cm³ 198.8 kg Jet-A, Jet A1
    TS-1
    No 3 Jet Fuel
    15:1 2000 hrs
    or 12 years
    234 hp @ 2200 4.96 x 3.94 in 302 in³ 438.3 lbs
    CD-265  4 195 kW @ 2500 126 x 100 mm 4976 cm³ 198.8 kg Jet-A, Jet A1
    TS-1
    No 3 Jet Fuel
    15:1 2400 hrs
    or 12 years
    265 hp @ 2500 4.96 x 3.94 in 304 in³ 438.8 lbs

    CDR-285 Rotorcraft Details

    Model #CYL  Rated Power
    @RPM
    Bore x Stroke Displacement Dry Weight   Certified Fuel
    Grade
    Compression
    Ratio
    Recommend.
    TBO
    CDR-265 4 194 kW @ 2700 126 x 100 mm 4988 cm³ 198.8 kg Jet-A, Jet A1
    TS-1
    No 3 Jet Fuel
    15:1 2000 hrs
    or 12 years
    264 hp @ 2700 4.96 x 3.94 in 304 in³ 438.3 lbs
    CDR-285  4 211 kW @ 2700 126 x 100 mm 4988 cm³ 198.8 kg Jet-A, Jet A1
    TS-1
    No 3 Jet Fuel
    15:1 2200 hrs
    or 12 years
    287 hp @ 2700 4.96 x 3.94 in 304 in³ 438.8 lbs



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