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Rotax 912 Series Service Manual

Rotax 912 Series
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73-00-00
page 34
May 01/2007
Effectivity 912/914 Series
Edition 1 / Rev. 0
d02623
BRP-Rotax
Maintenance Manual
3.4) General information on the fuel system
The most common reason for engine failure is a fault in the fuel system. Many
problems can be prevented by regular checks. Contamination and formation of
condensate can lead to erratic engine running or misfiring.
- Check float chamber for dirt and water.
- In the event of serious contamination or water, drain, clean and flush the
whole fuel system thoroughly, including the tank, filter, fuel pumps, float
housing and fuel lines.
â–  CAUTION :
- Unsuitable routing of fuel lines may cause engine failure.
- After repair work, the fuel system must be checked for leaks.
- Always use clean and non-translucent, safety approved fuel containers. Do
not smoke, do not allow open flames or sparks in the vicinity.
- Never refuel with engine running.
- Do not fill the tank to the brim, allow for expansion of the fuel.
- Remove spilt fuel immediately, dispose of it respecting environmental
regulations.
- Gasoline is highly inflammable and under certain conditions explosive.
Handling of fuel in well ventilated places only.
- Close fuel cock, as the float needle valve may not retain the fuel pressure
over a longer period or during transport of the aircraft.

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Rotax 912 Series Specifications

General IconGeneral
Redline5800 rpm
TBO2000 hours
Displacement1211 cc
Bore79.5 mm
Stroke61 mm
Power Output80 hp (59.6 kW)
Compression Ratio9.0:1
Fuel TypeAvgas 100LL
Ignition SystemDual electronic ignition
Fuel SystemFuel Injected
Oil SystemDry sump
Engine Type4-cylinder, horizontally opposed, 4-stroke

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