

| Type | 4-cylinder, 4 stroke, in-line, liquid cooled, overhead camshaft, normally aspirated |
| Power Output | 100hp (74.6 kw) at propeller flange |
| Displacement | 1488cc (90.7 cubic inches) |
| 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 | 226.2lbs (103.2 kg) - Weight Comparison Chart |
| Dimensions | H-25", L-32", W-19 |
| 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, heat 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 - Add $3995.00 Single fuel pump with bracket - Add $242.00 Dual fuel pump assembly with plumbing and bracket - Add $484.00 60 Amp Alternator - Add $180.00 Ceramic power-flow exhaust header - Add $700.00 |