Continental CD-135 Jet-A Engine

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

Our CD-135* jet fuel piston engine for General Aviation generates a take-off power of 99 kW (132.8 hp). The CD-135* is a turbocharged, 4-cylinder in-line engine which has been EASA certified since August 2006 and FAA certified since October 2006. Its predecessor, the Centurion 1.7, has been certified by the European Aviation Authorities since May 2002 and by the FAA since October 2003. The weight of all CD-135* engines is identical to 1.7 engines, enabling a straight replacement.

The CD-135* is certified for the use of both kerosene and diesel (DIN EN590) and is running with the two fuels in any mixture ratio. The engine has a time between replacement (TBR) of 2,100 hrs.

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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 engines.

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 oil system

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 mm3.26 in

Stroke

92 mm3.62 in

Compression

18:1

Dimensions (WxLxH)

778 x 816 x 636 mm30.63 x 32.12 x 25.04 in

Dry Weight

134 kg295.4 lbs

*Not available for any new program. Please see CD-155 engine.

Performance

Max. Power up to 6,000ft	99 kW	135 HP
Max. Continuous Power	99 kW	135 HP
Power Best Economy	71 kW	97 HP
Recommended Load	75%
Power constant	available max. power at respective altitude
Torque at propeller	410 Nm	302 ft./lb
Torque at propeller (Best Economy)	340 Nm	250 ft./lb
Prop RPM max. and take off	2300 RPM
Prop RPM best economy	2000 RPM
Prop RPM over-speed tested	2660 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	15-20 l/hr	4-5.3 gal/hr
Specific fuel consumption	214 g/kW hr	0.35 lb/HP hr

Electrical System

Electrical system	Full Authority Digital Engine Control (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 60 countries
Supplemental Type Certification	DA40, DA42, C172, PA28, DR400