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Rotax 912 Series Installation Manual

Rotax 912 Series
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d04921.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
61-00-00
page 3
August 01/2012
1) Propeller drive
General note The propeller in tractor or pusher arrangement must be fitted on the pro-
peller flange in accordance with applicable regulations. As required utilize
one of the three possible pitch circle diameters (P.C.D) on the flange.
The propeller design must be certified in accordance with applicable reg-
ulations, such as FAR or EASA, by the aircraft manufacturer.
1.1) Technical data
Direction of rota-
tion
See Fig. 1.
Direction of rotation of the propeller flange:
- left, counter clockwise, looking towards face of flange.
Graphic Direction of rotation
Fig. 1
08629
Transmission Gear transmission:
- i= 2.2727 (50 Teeth/22 T)
- i= 2.4286 (51 Teeth/21 T)
.
Vibration analy-
sis
NOTE: Vibration analysis of the whole system (engine, suspen-
sion, propeller etc.) should be carried out as part of the
certification process.
If no limits are available in the technical literature, a max.
of 1.0 IPS (inches per second) at 5000 rpm. can be as-
sumed.
.

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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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