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Type: 4-cylinder, 4 stroke, in-line, liquid cooled,
overhead camshaft, normally aspirated |
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Power output: 125 hp (93.2 kw) at propeller flange Horsepower Comparison Chart |
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Displacement: 1590 cc (97.0 in3) |
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Bore: 75 mm (2.95
in) |
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Stroke: 84.6
mm (3.33 in) |
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Direction of Rotation: Clockwise (facing of propeller flange) |
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Cooling: Water-glycol mixture. Water pump driven by
camshaft belt |
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Block: One piece
aluminum with re-borable cast iron liners |
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Crankshaft: Fully girdled, hardened, 5 main precision bearings |
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Lubrication: Full pressure, internal gear type pump, wet sump |
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Ignition: High energy mulitspark electronic CD ignition |
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Carburation: Muliport
sequential electronic fuel injection |
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Reduction System: 100mm (3.93 in) HTD Cog Belt |
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Reduction Ratio: 2.4:1(6000 rpm engine/2500 rpm propeller) (6500 engine/2700
propeller) |
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Oil Type: 5W30 Synthetic |
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Oil Quantity: 3.5 litres (3.7 US quarts) |
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Weight: 247
lbs (112.8 kg) |
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Dimensions: H-23" L-331/4" W-211/2" |
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Fuel Required: 90 Octane unleaded, minimum (R + M)/2 Can also use 100LL aviation
gasoline |
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Cylinder Head: One piece, aluminum, cross flow design,
16 valve and VTEC variable valve
timing |
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Compression Ratio: 9.2:1 |
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Camshaft: Cast alloy, head treated, parkerized |
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Alternator: 60 Amp belt drive |
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Specific Fuel Consumption: 0.43 lb/bhp/hr at 70% power |
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Starting System: Electric gear reduction starter |
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