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