Rotax 618, Rotax 618 aircraft engine, Rotax 618 75 HP aircraft engine specifications and technical data

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Rotax 618 75 HP aircraft engine specifications and technical data

Rotax 618 aircraft engine.

Rotax 618 aircraft engines specs.
DESCRIPTION: Two cylinder, two stroke liquid cooled engine with rotary valve inlet, with RAVE (adjustable variable exhaust), dual electronic ignition, integrated water pump and thermostat, exhaust system, electric start, model "C" or :E: gear box only, intake silencer, and oil injection.
BORE: 76.0 mm (2.99in.)
STROKE: 68.0 mm (2.68in.)
DISPLACEMENT: 617 cc (37.65 cu. in.)
COMPRESSION: Theoretical: 11.5 - effective 5.95
POWER OUTPUT: 48 kw (73.8 hp SAE) at 6750- 1/min
TORQUE: 75 nm (55.3 ft. lbs.) at 6,000 1/min.
MAX RPM: 6800
DIRECTION OF ROTATION: Counter- clockwise, viewed towards PTO
(Clockwise with Reduction installed)
CYLINDER: 2 light alloy cylinder with cast iron sleeves
PISTON: aluminum cast piston with 2 piston rings
PISTON/CYLINDER CLEARANCE: 0.06mm (.0024")
CHT: Cylinder Head Temperatures
(Optional Values)
Normal: 110C- 130C or 230F-270 F
Maximum: 150C or 300F
Max. Difference: 10C or 45F
EGT: Exhaust Gas Temperatures Normal: 500C - 620C or 930F - 1150F
Maximum: 650C or 1200F
Max. Difference: 25C or 45F
Crankcase Temp. Max.: 80C or 175F
Cooling Liquid Temp Max.: 80C or 175F
IGNITION SYSTEM: Breakerless Ducati Capacitor Discharge Dual Ignition with magneto generator
GENERATOR OUTPUT: 200 Watts AC at 6000prm and 13.5 RMS
IGNITION TIMING: 1.96mm or .077" (18 BTDC)
SPARK PLUG: 14mm NGK B8ES
ELECTRODE GAP: 0.5mm (.02")
ROTARY VALVE TIMING: Opens: 130 BTDC
Closes: 50 ATDC
CARBURETOR: 2 x Bing 54 36mm Slide Valve
FUEL PUMP: Pneumatic fuel pump
FUEL: Regular or Premium Gasoline, octane number not below RON 90 (unleaded)
LUBRICATION OF ENGINE: Oil-in- fuel with Super two-cycle oil ASTM/CEC standard, mixing ratio
LUBRICATION OF REDUCTION GEAR: Gear oil API-GL5 or GL6, SAE 140 EP or 85W - 140EP
DIRECTION OF PROPELLER SHAFT: Clockwise, viewed towards prop flange
STARTER: Rewind Starter Standard
STANDARD VERSION INCLUDES: Engine with carburetors w/ clamps, fuel pump, exhaust system
WEIGHT: Engine Block: ............................................ 68.3 lbs.
2 Carburetors ...............................................4.0 lbs.
Intake Silencer..............................................2.4 lbs.
Electric Starter..............................................7.7 lbs.
"C" Gear Box .............................................17.0 lbs.
Exhaust system .........................................13.2 lbs.

The Rotax 618 is no longer in production. For parts click here.

Rotax 618, 76 horsepower aircraft engine.

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