Aero engine · 80 HP
CA300
12 490,00 €
A lightweight naturally aspirated flat-four for ultralight aircraft and other light applications.
The CA300 is a compact aircraft engine with a very strong power-to-weight ratio. It suits ultralight aircraft, light sport designs, and projects where low weight and simple operation matter most.
Key features
- 4-cylinder horizontally opposed engine
- Liquid-cooled cylinder heads and air-cooled cylinders
- Redundant dual ignition
- Gearbox i=2.43
- Max. operating altitude 3500 m
- Dry sump and forced lubrication with separate oil tank
Technical data
- Displacement
- 1211 cm³
- Dimensions
- 670 x 580 x 420 mm
- Bore
- 79.5 mm
- Stroke
- 61 mm
- Dry weight
- 55.4 kg / 122 lbs
- Max. power
- 59.6 kW @ 5800 r/min
- Alternator
- 0.25 kW @ 14V
- Start mode
- Electric starter
- Ignition
- Dual capacitor ignition
- Fuel supply system
- Carburetor
- Fuel
- min. RON 95
- Cooling
- Liquid-cooled cylinder heads and air-cooled cylinders
- Gearbox
- i=2.43
- Max. operating altitude
- 3500 m
- TBO
- 2000 h
Brochure data
Performance curves
PDF brochure
Complete technical sheet
Download the original brochure with parameters, performance charts, and recommended applications.
Download PDF brochureReferences
Reference installations by SKYLEADER and DIRECT FLY
Photos are ordered by the priority supplied by the client. They serve as examples of installations and operation.
CA300
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