R320

R320

R320

Product catalog summary
Description:
The R320 engine is designed for equipping PPG tandem trikes or small microlight airplanes. It is a high-performance engine suitable for experimental and uncertified aircraft.
Engine Performance:
  • Displacement: 294.7cc
  • Intake Type: Reed valves into the crankcase
  • Bore and Stroke: 72mm each
  • Maximum Power RPM: 8000
  • Engine Weight (with exhaust and air filter): 32.8 Kg
Carburetor Specifications:
  • Main Jet: 115
  • Idle Jet: 35
  • Needle: CHN, positioned 5th from top
  • Throttle Valve: 7
  • Carburetor Model: Keihin PWKS 38
  • Mixture Screw: 1 turn from fully closed
Additional Features:
  • One liquid-cooled aluminum cylinder with Nikasil ceramic coating
  • Poly–V belt driven reduction with options of 1/2.7 or 1/3
  • Electric starter with CDI ignition (pre-ignition set up is 0mm from TDC)
  • In-flight consumption at 5400 RPM: 5 liters/hour
  • Lubrication: 2.5% two-stroke oil with 95 unleaded petrol, 3% during running-in phase
  • Top Thrust with a 130cm propeller: 140 kilos*

*Thrust may vary based on propeller size, material, shape, and meteorological conditions.

Warnings:
The Paramotores HE Microlight Aircraft engines do not comply with federal safety regulations for standard aircraft. They are intended for use in experimental and microlight uncertified aircraft only, where engine failure will not compromise safety. It is crucial to read the operator’s manual before use. Further information is available from authorized HE Paramotores dealers.
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Catalog excerpts

R320-1

The R320 is the perfect engine to equip PPG tandem trikes or small microlight airplanes ENGINE PERFORMANCE Intake type Reed valves into the crankcase Bore Stroke Engine weight with exhaust and air filter. Needle position Throttle valve Mixture screw 1 turn from fully closed One liquid cooled aluminium cylinder with Nikasil ceramic coating Poly–V belt driven reduction. Reduction 1/ 2.7 or 1/3 Electric starter with CDI ignition (pre ignition set up is 0mm from TDC) In flight consumption with at 5400 R.P.M. (level flight), 5 litres/hour Lubrication mixture of 2,5% two stroke oil with 95 unleaded petrol and 3% during running in phase Top thrust with a 130cm propeller: 140kilos* (*) depending on propeller size, material, shape and on meteorological conditions, altitude… Warning: The Paramotores HE Microlight Aircraft engines do not comply with federal safety regulations for standard aircraft. This engine is for use in experimental and microlight uncertified aircraft only and only in circumstances in which an engine failure will not compromise safety. Before operating the engine read operator’s manual. Information is available from your local authorized HE Paramotores deal

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.