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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 8-2
OM Edition 1/Rev. 0 January 01/2012
d05872.fm
8.1) Engine preservation
General note
Due to the special material of the cylinder wall, there is no need
for extra protection against corrosion for the ROTAX aircraft engi-
nes. At extreme climatic conditions and for long out of service pe-
riods we recommend the following to protect the valve guides
against corrosion:
8.2) Engine back to operation
If preservation including oil change took place within a year of sto-
rage, oil renewal will not be necessary. For longer storage periods
repeat preservation annually.
WARNU
WARNING
Risk of burnings and scalds!
Hot engine parts!
Always allow engine to cool down to ambient
temperature before start of any work.
Step Procedure
1 Engine warm up.
2 Engine cool down.
3 Change oil.
4 Remove the top spark plugs and spray all openings withcor-
rosion inhibiting oil.
5 Turn the propeller several times by hand in direction of the en-
gine rotation, so that the corrosion inhibiting oil all necessary
points reaches.
6 Install the Spark plug in according the Maintenance Manual.
7Close all openings on the cold engine, such as exhaust end
pipe, venting tube, air filter etc. against entry of dirt and hu-
midity.
8 Spray all external engine parts of steel with corrosion inhibit-
ing oil.
Step Procedure
1 Remove all plugs and fasteners.
2 Clean spark plugs with plastic brush and solvent.

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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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