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 12 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 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

2300 rpm

Height

Width

Highlighted Applications

Diamond DA40 TDI

Diamond DA42 Twin Star

Cessna 172

Robin DR400

Piper PA-28

  1. Engine rated power at sea level standard day inlet conditions (29.92 in Hg, 59°F, 0 water vapor) with maximum allowable cylinder head and oil temperatures with full rich (maximum) fuel flow.
  2. See Maintenance Manual M-0 for details and applicability.

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