MZ 202 engine, MZ202 engine,MZ 202 ultralight aircraft engine.


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The powerful, lightweight MZ 202 ultralight engine is the result of a union of space age materials,MZ 202 engine, MZ202 engine,MZ 202 ultralight aircraft engine. innovative design and state of the art manufacturing methods. The engine has a Nikasil bore, giving longevity without adding unnecessary weight.

A fully electronic ignition system is used providing maximum reliability and requiring minimum maintenance. Ample electrical power for all normal requirements is provided by the powerful 180 Watt alternator.

For the ultimate in power and reliability, the MZ 202 can be supplied with electronic fuel injection that is controlled by a computerised engine management system. In this guise the alternator output is increased to 260 Watts.

Technical specifications:
Engine type: Twin cylinder in line two stroke.
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: 626 c.c.
Bore / Stroke: 76 mm / 69 mm
Alternator output: Normally aspirated, 180 Watts. Fuel injection, 260 Watts.
Ignition system: Carbureted / Fuel Inj Fully electronic dual capacitive discharge / inductive mappedsystem.
Fuel metering: Twin carburetors or computerised electronic fuel injection.
Lubrication: Fully synthetic oil, pre-mixed 50:1 in fuel. (unleaded mogas)
Output power: Normally aspirated 66 Hp@ 6200 RPM, Fuel injection 69 Hp@ 6400 RPM
Weight: 42 Kgs. Complete with all ancillaries, including battery and wiring.
Options: Normally aspirated (carburetors), or electronic fuel injection. 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.
Power / Torque Graph
Compact Radial Engines Inc. #3 8473 - 124th Street Surrey, British Columbia Canada, V3W 9G4 604-590-2950
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