MZ 34, MZ 34 single cylinder engine, MZ 34 ultralight aircraft engine.


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The MZ 34 ultralight engine also incorporates a Nikasil bore, giving longevity without adding unnecessary weight.

The ignition system is fully electronic for maximum reliability and minimum maintenance.

This engine weighs a mere 17kg (38lbs) ready to fly (except propellor) and is supplied complete with reduction drive, electric starter, automatic decompression valve, battery and exhaust.

 

 

 

 
Technical specifications:
Engine type: MZ34 Single cylinder two stroke lamellar engine.
Cooling system: Free air cooled by propeller, or force air cooled by integral fan (optional).
Rotation: Clockwise when facing gear box. i.e. from the front in tractor format
Displacement: 313 c.c.
Bore / Stroke: 76 mm / 69 mm
Alternator output: 90 Watts
Ignition system: Fully electronic capacitive discharge
Fuel metering: carburetor with diaphram.
Lubrication: Fully synthetic oil, pre-mixed 50:1 in fuel. (unleaded mogas)
Output power: 27 Hp@ 6250 RPM, or 38 Hp@ 6450 RPM with a tuned exhaust.
Weight: 17 Kgs. Complete with all ancillaries, including exhaust, starter and battery.
Options: Fan cooling.
Guarantee: One year or 200 hours running time.
Time before overhaul: 500 hours running time. (to be increased)
Time between de-cokes: Due to high efficiency, this engine should not normally require de-coking.
 

Compact Radial Engines Inc. #3 8473 - 124th Street Surrey, British Columbia Canada, V3W 9G4 604-590-2950
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