Our CD-155 jet fuel piston engine for General Aviation generates a take-off power of 114 kW (152.9 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 engine.
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
82 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