Rotax 912 i series Installation Manual

d05780.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 0
00-00-00
page 13
January 01/2012
- For continuing airworthiness see Maintenance Manual Line.
- Unauthorized modifications of engine or aircraft will automatically
exclude any liability of the manufacturer for sequential damage.
Engine run - In the interest of safety, the aircraft must not be left unattended while
the engine is running.
- To eliminate possible injury or damage, ensure any loose equipment
or tools are properly secured before starting the engine.
- When in storage protect the engine and fuel system from contamina-
tion and exposure.
- Never operate the engine and gearbox without sufficient quantities of
lubricating oil.
- Never exceed the maximum permitted operational limits.
- Allow the engine to cool at idle for several minutes before turning off
the engine.
- Propeller and its attachment with a moment of inertia in excess of the
specified value must not be used and releases the engine manufac-
turer from any liability.
- Improper engine installation and use of unsuitable piping for fuel, cool-
ing and lubrication system releases the engine manufacturer from any
liability.

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled