CD-100 SERIESCONTINENTAL MOTORS CD-100 DIESEL ENGINE 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 advantage as aircraft engines. A diesel cycle engine 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 CD-135 and CD-155 are an automotive based, liquid cooled and turbo-charged engine. This is another example of Continental's commitment to the advancement of general aviation technology. THE CD-135 AND CD-155 IS A FAMILY OF FOUR-STROKE, 4-CYLINDER, IN-LINE, DOHC, 4 VALVES PER CYLINDER, COMMON RAIL DIRECT INJECTION SYSTEM, TURBO CHARGED, LIQUID COOLED, FADEC, WET SUMP OIL SYSTEM AND REDUCTION GEAR ENGINES. THE ENGINE HAS A MAXIMUM CONTINUOUS POWER OF 132.8 HP 0 2300 RPM OR 152.9 HP 0 2300 RPM. Certified fuels: Displacement: Power: Maximum Rated RPM: Bore: Stroke: Compression Ratio: Height: Width: Length: Dry Weight: Cruise Fuel Consumption: Time Between Replacement: Jet-A, Jet-A1, Chinese Jet Fuel No. 3, TS-1, JB-8, JP-8+100, Diesel (EN 590) 1991 cm3 121.5 cu.in

POWERING 100 YEARS OF EXPERIENCE FORWARD MODEL CYLIN- METO POWER BORE X STROKE DISPLACEMENT DRY WEIGHT FUEL GRADE COMPRESSION RECOMMEND. TBR DERS 13 RPM BASIC ENGINE RATIO