![Continental Motors Group - logo](https://img.aeroexpo.online/images_ar/logo-p/L171290.gif)
![video corpo](https://img.aeroexpo.online/media/ps/images/common/stand/video-icon.gif)
Catalog excerpts
![CD-300 - 1](https://img.aeroexpo.online/pdf/repository_ar/171290/cd-300-15165_1m.jpg)
POWERING 100 YEARS OF EXPERIENCE FORWARD Continental® continues its leadership in advanced technology by offering a line of engines to meet the needs of a growing global market. Diesel engines offer distinctive advantages as aircraft engines. A diesel cycle engine is designed for continuous high stress, making it suitable for aviation applications. Also by design, a diesel engine cannot operate too lean. Self ignition means no danger of detonation, since fuel is not introduced until the optimal moment of combustion. The CD-300 concept is a liquid-cooled and turbo-charged engine. This is another example of Continental’s commitment to the advancement of general aviation technology. THE CD-300 IS A 4-VALVE, 6-CYLINDER DIESEL ENGINE IN V CONFIGURATION WITH COMMON RAIL DIRECT INJECTION. THE ENGINE IS TWIN TURBO-CHARGED, LIQUID-COOLED AND INCORPORATES A WET OIL SUMP AS WELL AS A DUAL REDUNDANT FADEC SYSTEM, INTEGRATED GEARBOX AND PROPELLER GOVERNOR. TAKE OFF POWER IS 300 HP fa 2300 RPM. EASA CERTIFIED, FAA VALIDATION PENDING. Certified fuels: Jet-AI Dry Weight (incl gearbox): 248.5 kg 547.8 lbs Cruise Fuel Consumption: 34.9 liters/hr 9.2 gallons/hr Time Between Replacement: TBR 1200h, projected 2000h
Open the catalog to page 1All Continental Motors Group catalogs and technical brochures
-
PAINT CATALOG
44 Pages
-
Battery Catalog
102 Pages
-
TITAN™ ENGINE
1 Pages
-
CD - 100 SERIES
2 Pages
-
400 SERIES
2 Pages
-
300 SERIES
2 Pages
-
200 SERIES
2 Pages
-
X540_series_engines
1 Pages
-
X370_series_engines
1 Pages
-
X360_series_engines
1 Pages
-
X340_series_engines
1 Pages
-
X320_series_engines
1 Pages