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