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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 1-6
OM Edition 1/Rev. 2 April 01/2014
d05694.fm
1.4) Safety notice
Normal use z
- This engine is not suitable for acrobatics (inverted flight, etc.).
- This engine shall not be used on rotorcrafts with an in-flight
driven rotor (e.g. helicopters).
- It should be clearly understood that the choice, selection and
use of this particular engine on any aircraft is at the sole dis-
cretion and responsibility of the aircraft manufacturer, assem-
bler and owner/user.
- Due to the varying designs, equipment and types of aircraft,
BRP-Powertrain grants no warranty or representation on the
suitability of its engine’s use on any particular aircraft. Further,
BRP-Powertrain grants no warranty or representation of this
engine’s suitability with any other part, components or system
which may be selected by the aircraft manufacturer, assemb-
ler or user for aircraft application.
- Certain areas, altitudes and conditions present greater risk
than others. The engine may require humidity or dust/sand
preventative equipment, or additional maintenance may be re-
quired.
- You should be aware that any engine may seize or stall at any
time. This could lead to a crash landing and possible severe
injury or death. For this reason, we recommend strict compli-
ance with the maintenance and operation and any additional
information which may be given to you by your dealer.
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
Never fly the aircraft equipped with this en-
gine at locations, airspeeds, altitudes, or oth-
er circumstances from which a successful no-
power landing cannot be made, after sudden
engine stoppage.
WARNU
WARNING
Non-compliance can result in serious injuries
or death!
For each use of VFR or IFR in an aircraft the
applicable requirements and other existing
regulations must be adhered.

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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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