CAM 125
(Honda based 130 Hp engine for homebuilt and experimental aircraft).
Price: $9850.00 (Add $8795.00 for redrive)
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 cubic in) |
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, heat treated, parkerized |
Alternator | 35 Amp belt drive |
Specific Fuel Consumption | 0.43 lb/bhp/hr at 70% power |
Starting System | Electric gear reduction starter |
|