Continental Diesel CD-155 (155 hp)
Continental Diesel offers with the CD-155 a jet fuel piston engine for general aviation with a take off power of 99 kW (155 hp). The CD155 is a turbo charged 4-cylinder in-line engine. The CD-155 is certified for the use of both jet fuel and diesel (DIN EN590) and is running with the two fuels in any mixture ratio.The engine has a time between replacement (TBR) of 2100 hr. Despite of improved performance, the CD-155 weighs as much as the CD-135.
General Engine Description
Engine work principle: Turbo diesel engine  
Cylinder, Configuration: 4, in-line  
Intake system: Common rail direct injection  
Cooling: Liquid cooled  
Approved propeller: 3-blade propeller of MT with hydraulic variable pitch (MTV-6 series)  
Weight (complete & dry): 134 kg 295.4 lbs
Usable Fuels (UAV): Diesel (EN 590), Jet A, Jet A-1, JP-5, DEF STAN 91-86, JP-8, DEF STAN 91-91, JP-8+100, Chinese Jet Fuel No 3  


Max. Power up to 6,000ft: 114 kW 155 hp
Max. Continuous Power: 114 kW 155 hp
Power Best Economy: 97 kW 132 hp
Recommended Load: 75 percent  
Power constant: available max. power at respective altitude  
Consumption in cruise flight: 18-22 l/h 4.7-5.8 gal/hr