Continental^® CD-135 Jet-A Piston Engine

Introducing the CD-135 Jet-A piston engine that offers a fusion of robust power and excellent fuel efficiency. Its foundation in automotive-based engineering principles guarantees consistent, dependable performance across diverse flying conditions.

The CD-135 is a member of the CD-100 Series of engines which is a family of liquid cooled, turbocharged, 4-cylinder, fuel injected, compression ignition, four-stroke, geared, right (CW) rotating, aircraft engine with Full Authority Digital Engine Control (FADEC).

Continental^® CD-135 Jet-A Piston engine

Engine System

Full Authority Digital
Engine Control
(FADEC) controlled

Fuel Burn

Gallons (4.89 ) / liters (18.5) per hour at best economy

cooling system

Liquid Cooled

Fuel Savings With Jet-A

40% vs comparable
gasoline engine

Flight Hours

Over 10 Million

COST SAVINGS

With the ability to burn heavy fuels, the CD-135 engine ensures substantial fuel savings and lower operating costs. Engineered for efficiency, the CD-135 delivers reliable performance while minimizing expenses.

CONVENIENCE

The CD-135 engine by Continental Aerospace Technologies™ brings unparalleled convenience to aviators, thanks to its versatile fuel capabilities. Whether you are operating in remote locations or urban environments, the ability to burn heavy fuels, ensures you have access to readily available and cost-effective options. This flexibility not only simplifies logistics but also enhances operational efficiency, allowing for seamless transitions between different fuel types without compromising performance.

RELIABLITY

Nothing is more important than a safe, reliable engine. CD-135’s design and advanced technology focus on reliability, reducing downtime and maintenance needs. Pilots can trust the CD-135 for its dependability, backed up by the global engine leader in general aviation.

TECHNICAL DATA

Certified fuels

Jet-A, Jet A1, JET A-1 (ASTM D 1655) Jet Fuel No. 3, TS-1, JB-8, JP-8+100, Diesel (EN 590)

BORE

length

Displacement

power

Stroke

Comp. Ratio

CONFIGURATION type

Time between replacement (TBR)

2100 hrs or 12 yrs

Speed

Height

Width

PERFORMANCE

Max Power up to 6,000ft

99 kW

135 hp (DIN)

Max Continuous Power

99 kW

135 hp (DIN)

Power Best Economy

71 kW

97 hp (DIN)

Recommended Load

75 percent

Torque at Propeller

411 Nm

303 ft.lbf

Torque at Propeller (Best Economy)

337 Nm

249 ft.lbf

Prop RPM Max and Take Off

2300 RPM

Prop RPM Best Economy

2010 RPM

Engine RPM Max and Take Off

3890 RPM

Engine RPM Best Economy

3380 RPM

Consumption in Cruise Flight

15-20 l/hr

4-5.3 gal/hr

Specific Fuel Consumption

214 g/kWh

0.35 lb/HPhr

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-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

ENGINE Oil

AeroShell Oil Diesel Ultra 5W-30, Shell Helix Ultra 5W-30  & Helix Ultra 5W-40

Cooling Liquid

G48/Glysantine (50% Water, 50% BASF Glysantin), Protect Plus, Protect G05

GearBOX Oil

Centurion Gearbox Oil N1

JET-A PISTON ENGINES

Continental® CD-135 Jet-A Piston Engine

Continental® CD-135 Jet-A Piston engine