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Rotax 912 Series Installation Manual

Rotax 912 Series
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d04918.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
00-00-00
page 11
August 01/2012
4.1) Safety information
Use for intended
purpose
- 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 discretion and
responsibility of the aircraft manufacturer, assembler 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, component or system which may be selected by the
aircraft manufacturer, assembler or user for aircraft application.
- In addition to observing the instructions in our Manual, general safety
and accident preventative measures, legal regulations and regulations
of any aeronautical authority must be observed.
- Where differences exist between this Manual and regulations provided
by any authority, the more stringent regulation should be applied.
WARNUNG
WARNING
Non-compliance can result in serious injuries or
death!
Only certified technicians (iRMT, see also Mainte-
nance Manual Line) and trained on this product are
qualified to work on these engines.
WARNUNG
WARNING
Non-compliance can result in serious injuries or
death!
Never fly the aircraft equipped with this engine at lo-
cations, airspeeds, altitudes, of other circumstances
from which a successful no-power landing cannot be
made, after sudden engine stoppage.
WARNUNG
WARNING
Non-compliance can result in serious injuries or
death!
Unless correctly equipped to provide enough electri-
cal power for night IFR (according latest requirement
as ASTM), the ROTAX 912 UL/ULS is restricted to
DAY VFR only.

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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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