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 |