| Type: 4-cylinder, 4 stroke, in-line, liquid cooled, overhead camshaft, normally aspirated |
| Power output: 100hp (74.6 kw) at propeller flange |
| Displacement:1488cc (90.7in3) |
| Bore: 74mm (3.07 in) |
| Stroke: 86.5 mm (3.41 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: Redundant dual digital electronic ignition with programmed automatic advance feeding single plug/coil units |
| Carburation: 2 barrel progressive opening downdraft |
| 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:226.2 lbs (103.2 kg) Comparison Chart |
| Dimensions: H-25" L-32" W-19 1/2" |
| Fuel Required: 90 Octane unleaded, minimum (R + M)/2 Can also use 100LL aviation gasoline |
| Cylinder Head: One piece, aluminum, cross flow design |
| Compression Ratio:9.6:1 |
| Camshaft:Cast alloy, head treated, parkerized |
| Alternator: 15 Amp belt drive |
| Specific Fuel Consumption: 0.43 lb/bhp/hr at 80% power |
| Starting System: Electric gear reduction starter |
| Optional:
Ellison Throttle Body Fuel
System
60 Amp Alternator |
Engine Specification Comparison Chart
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