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Rotax 912 Series Installation Manual

Rotax 912 Series
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d04920.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
24-00-00
page 17
August 01/2012
2.7.2) Connection
General note
Feeding wiring Feeding wiring to electric rev counter on left side of ignition housing.
- Length approx. 600 mm (24 in.) starting from ignition housing.
Connections 2 flexible cables 0.5 mm
2
, white/yellow and blue/yellow (in insulation
wrap).
2.8) Battery
General note See Fig. 11.
2.9) Capacitor (Option electrical fuel pump)
General note See Fig. 11.
2.10) Easy start function on the electronic module (optional)
General note See Fig. 10.
In order to use the easy start function the relevant connections to the
starter relays and ignition switch need to be made.
The start function can be used for aircraft, which have an engine start
problem in cold conditions.
NOTE: In addition also a modified fly wheel hub is offered, which
aids improved starting.
WARNUNG
NOTICE
BRP-Powertrain developed especially for this applica-
tion a non-certified electric rev counter. Certification to
the latest requirements such as FAR or EASA has to
be conducted by the aircraft manufacturer. See also
SI-13-1996, latest issue.
WARNUNG
NOTICE
To warrant reliable engine start use a battery of at least
16 Ah capacity.
WARNUNG
NOTICE
To warrant reliable operation of the electrical fuel pump
the use of capacitor of at least 22 000 µF/25 V is
necessary.

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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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