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