CAM 100 SPECIFICATIONS

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

 

CAM 100

Rotax 912

EA81

Type

4-cylinder, 4 stroke, in-line, liquid cooled

4-cylinder, 4 stroke, opposed cylinders, liquid cooled

4-cylinder, 4 stroke, opposed cylinders, liquid cooled

Core

Honda

Rotax

Subaru

Power Output

100 hp (75 kw) at propeller flange

MAX: 80 hp @ 5500 rpm

100 hp

Displacement

1488 cc (90.7 in.)

1,211.2 cc (73.91 in.)

1781 cc (108 in.)

Bore

74 mm (3.07 in.)

79.5 mm (3.13 in.)

92 mm (3.84 in.)

Stroke

86.5 mm (3.41 in.)

61.0 mm (2.40 in.)

67 mm (2.68 in.)

Direction of      Rotation

Clockwise facing propeller flange

Counter-clockwise (facing propeller flange)

 

Cooling

Water-glycol mixture

Liquid cooled cylinder heads, air cooled cylinder

 

Block

One piece aluminum with iron liners

 

 

Crankshaft

Full girdled, hardened, 5 main precision bearings

Case-hardened with plain bearings

 

Lubrication

Full pressure, internal gear type pump, wet sump

Dry sump with trochoid pump, cam shaft driven, oil return by BLOW-BY gas

a) Dry sump, remote reservoir - engine  b) Self contained oil sump / Internal Mist - reduction

Ignition

Redundant dual digital electronic

Capacitor discharge double ignition, generator with electronic advance and integrated magneto, redundant

Crank Triggered, dual ignition, single spark plug

Carburation

2 barrel progressive opening downdraft

Carburated

 

Reduction System

100 mm (3.93 in.) HTD cog belt

Integrated reduction gear, torsional shock absorption

Helical Cut, Steel spur Gear type

Reduction Ratio

2.4:1

2.27:1

1.48 to 3.41:1 (2.34:1 std)

Oil Type

5W30 Synthetic

SAE 20W50 or SAE 30

 

Oil Quantity

3.5 liters (3.7 US quarts)

3.0 liters (.8 US gal)

 

Weight

226 lbs (102.2 kg)

140.8 lbs (63.9 kg)

214 lbs (97.1 kg)

Fuel Required

90 Octane unleaded, minimum (R + M)/2.  Can also use 100 LL Aviation Gasoline

Premium grade leaded gas or SUPER ROZ 95 unleaded

Auto Lead & No Lead, Reg. or Premium     Aviation 80/87 (red) and 100 LL

Cylinder Head

One piece aluminum cross flow design

4 separate cylinder heads

 

Compression Ratio

9.6:1

9.0:1

8.9:1

Camshaft

Cast alloy, heat treated parkerized

 

 

Alternator

15 Amp belt drive (65 amp optional)

12V/250 W AC, 18 Amp

Dual (2) "V" type Belt Drive

Specific Fuel Consumption

.43 lb/bhp/hr at 80% power

.45 lb/bhp/hr @ 75% cruise

 

Starting System

Electric gear reduction starter

Integrated electric starter

2 kw, 3 stage, Geared Electric Starter

TBO

2500 hours

1,200 hours

 

Warranty

5 Years / 500 Hours

6 Months (1 Year Extended - Optional)

1 Year