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Aircraft - Engine Spec.

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Bore

Stroke

Displacement

Compression Ratio

3.31” / 84 mm

2.40” / 61 mm

82.6 cu/in / 1352 cm 3

10.5:1

Max power (5 min's)

Max power (cont.)

Max torque

Engine weight

Fuel consumption @ 83 mph

R.P.M. @ 60 mph

100 hp@ 5800 rpm

95 hp @ 5500 rpm

94 ft/lbs @ 5100 rpm

124.7 lb’s / 56.6 kg’s

11-14 ltr’s p/h

4000 rpm

2.43 : 1 reduction with slipper clutch

Integral Gearbox

Performance

Combustion Chambers

Engine Spec.

4 cylinder, 4 stroke liquid/air cooled engine with opposed cylinders, dry sump forced lubrication with separate 3 ltr (.8 gal US) oil tank, automatic adjustment by hydraulic valve tappet, 2 CD carburettors, mechanical fuel pump, electronic dual ignition, electric starter, integrated reduction gear i= 2.43

Rotax 914 - 115 bhp

Rotax 912s - 100 bhp

Rotax 912 - 80 bhp