The Rotax 618 is a 73.8 hp (55 kW) two-stroke, two-cylinder, liquid cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.

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  • The Rotax 618 is a 73.8 hp (55 kW) two-stroke, two-cylinder, liquid cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.
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dbpprop:coolingsystem
  • liquid cooled
dbpprop:displacement
  • 617 (xsd:integer)
dbpprop:fueltype
  • premium unleaded: RON 90 octane or higher leaded or unleaded or AVGAS 100 LL
dbpprop:oilsystem
  • oil-in-fuel (pre-mix) at 50:1
dbpprop:power
  • 55 kW 73.4 HP SAE @ 6750 RPM
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  • 0.56 hp/lb (1.07 kg/kW)
dbpprop:stroke
  • 68 mm (2.68 in)
dbpprop:type
  • 2-cylinder, 2-stroke, rotary valve, oil-in-fuel or oil-injected lubrication, dual carburetors, dual ignition
dbpprop:valvetrain
  • rotary inlet valve, exhaust valve
dbpprop:weight
  • 59.1 (xsd:double)
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  • The Rotax 618 is a 73.8 hp (55 kW) two-stroke, two-cylinder, liquid cooled, gear reduction-drive engine that was formerly manufactured by BRP-Rotax GmbH & Co. KG. It was designed for use on ultralight aircraft.
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  • Rotax 618
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