Our CD-155 jet fuel piston engine for General Aviation generates a take-off power of 114 kW (155 hp). 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 2,100 hr. Despite of improved performance 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 (ratio i = 1:1.69)
Engine work principle
Turbo diesel engine
Common rail direct injection
Wet sump oil system
Full Authority Digital Engine Control (FADEC)
reduction gearbox with integrated clutch (ratio i = 1:1,69)
3-blade propeller of MT with hydraulic variable pitch (MTV-6 series)
1.991 cm³121.5 cu.in
83 mm3.26 in
92 mm3.62 in
778 x 816 x 636 mm30.63 x 32.12 x 25.04 in
Weight (complete & dry)
134 kg295.4 lbs