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Rotax 912 i series Operator's Manual

Rotax 912 i series
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Effectivity: 912 i Series BRP-Powertrain page 3-6
OM Edition 1/Rev. 2 April 01/2014
d05696.fm
3.2) Before engine start
Carry out pre-flight checks.
3.3) Pre-flight checks
Safety
Operating media
Oil level
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
MASTER SWITCH, LANE A and LANE B
switch “OFF”. Before moving the propeller
anchor the aircraft.
WARNU
WARNING
Risk of burnings and scalds!
Hot engine parts!
Carry out pre-flight checks on the cold or luke
warm engine only!
Step Procedure
1 Check for any oil-, coolant- and fuel leaks.
If leaks are evident, rectify and repair them before next
flight.
WARNUNG
NOTICE
The oil specifications of the section Chapter
2.4) Operating media are to be observed!
Step Procedure
1 Check oil level and add oil if necessary.
2
NOTE: Propeller shouldn't be turned reverse
the normal direction of engine rotation.
Remove oil tank cover, turn the propeller slowly by hand in
direction of engine rotation several times to pump oil from
the engine into the oil tank.
3 It is essential to build up compression in the combustion
chamber. Maintain the pressure for a few seconds to let the
gas flow via the piston rings into the crankcase. The speed
of rotation is not important as the pressure and the amount
of gas which is transfered into the crankcase.
4 This process is finished when air is returning back to the oil
tank and can be noticed by a gurgle from the open oil tank.
5 Install oil tank cap.

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Rotax 912 i series Specifications

General IconGeneral
Number of Cylinders4
Max Power100 hp (73.5 kW)
Max Power Output RPM5800 rpm
Ignition SystemDual electronic ignition
Oil SystemDry sump, forced lubrication with separate oil tank
Reduction Gear Ratio2.43:1
TBO2000 hours
Engine Type4-stroke, horizontally opposed
Displacement1352 cm³
Bore x Stroke84 mm x 61 mm
Max Torque128 Nm
Fuel TypeAvgas 100LL or unleaded automotive gasoline
Fuel SystemElectronic fuel injection
Cooling SystemLiquid/air-cooled

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