The Continental® CD-155 jet fuel piston engine for General Aviation generates a take-off power of 114 kW (155 HP) at 2300 RPM. The CD-155 is a turbocharged, 4-cylinder in-line engine which is EASA and FAA certified. The CD-155 runs on both jet fuel and diesel (DIN EN590), and accepts any combination of the two.
The engine has a time between replacement (TBR) of up to 2,100 hours or 12 years. Despite the improved performance, the CD-155 weighs as much as the CD-135.
4-cylinder, in-line diesel cycle engine, DOHC, 4 valves per cylinder, common rail direct injection, system turbo charged, liquid cooled, FADEC, wet sump oil system and reduction gear engine.
Engine Work Principle
Turbo Diesel Engine
Cylinder, Configuration
4, In-Line
Valve Gear
DOHC
Intake System
Common Rail Direct Injection
Cooling
Liquid Cooled
Oil System
Wet Sump
Electrical System
Full Authority Digital Engine Control (FADEC)
Prop Drive
Reduction Gearbox With Integrated Clutch (ratio i = 1:1,69)
Approved Propeller
3-blade Propeller of MT with Hydraulic Variable Pitch (MTV-6 series)
Displacement
1991 cm³121.5 in³
Bore
83 mm3.27 in
Stroke
92 mm3.62 in