Continental CD-155 Jet-A Engine

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Continental CD-100 Jet-A Engine Series: Aircraft Engine Facing Right

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.

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List of CD100 STCs

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 mm 3.27 in

Stroke

92 mm3.62 in

Compression Ratio

18:1

Dimensions (WxLxH)

778 x 816 x 636 mm30.63 x 32.12 x 25.03 in

Weight (complete & dry)

134 kg295.4 lbs

Performance

Max. Power up to 6,000ft	114 kW	152.9 HP
Max. Continuous Power	114 kW	152.9 HP
Power Best Economy	71 kW	97 HP
Recommended Load	75 percent
Power Constant	Available max. power at respective altitude
Torque at Propeller	473 Nm	349 ft.lb.
Torque at Propeller (Best Economy)	410 Nm	302 ft. lb.
Prop RPM Max. and Take Off	2300 RPM
Prop RPM Best Economy	2000 RPM
Prop RPM Over-Speed Tested	2000 RPM
Engine RPM Max. and Take Off	3890 RPM
Engine RPM Best Economy	3380 RPM
Engine RPM Over-Speed Tested	4500 RPM
Consumption in Cruise Flight	18-22 l/hr	4.75-5.8 gal/hr
Specific Fuel Consumption	220 g/kWh	0.36 lb/HPhr

Electrical System

Electrical System	FADEC
Voltage	28 V, optional 14 V
Alternator Performance	1680 W (28 V), Optional 1260 W (14 V)
Current / Voltage	60 A (28 V), Optional 90 A (14 V)
Compact Engine Display	0.3 kg	0.66 lbs

Operating Fluids

Certified Fuels	Diesel (EN 590), Jet A, Jet A-1
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
Oil	Shell Helix Ultra 5W30; Shell Helix Ultra 5W40; AeroShell Oil Diesel 10W-40; AeroShell Oil Diesel Ultra
Cooling Liquid	50% Water; 50% BASF Glysantin; G48/ Glysantin; Protect Plus
Gear Oil	Shell EP 75W90 API GL-4

Certificates

Lifetime	Up to 2100 hrs or 12 years
Type Certification	EASA, FAA, in 57 countries
Supplemental Type Certification	Cessna^® 172, Diamond^® DA40, Robin^® DR400, Piper^® PA-28