d04918.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
00-00-00
page 6
August 01/2012
Auxiliary equip-
ment tested
NOTE: The following equipment is not included as part of the stan-
dard engine version!
The following auxiliary equipment has been tested on ROTAX engine
type 912 for safety and durability to the standards of aviation.
The furnishing of proof in accordance to the latest FAR or EASA has to be
conducted by the aircraft manufacturer.
- Airbox
- External alternator
- Engine suspension frame
- Vacuum pump (feasible on configuration 2 and configuration 4 only)
- Drive for rev counter/hour-meter
- Oil cooler with connections
- Coolant radiator
- Coolant overflow bottle
Auxiliary equip-
ment not tested
The following auxiliary equipment has not been tested on ROTAX
engine type 912 for safety and durability to the standards of aviation.
- Exhaust system
- Intake filter
- Flydat
- Mechanical rev counter
- Electric rev counter
- Shock mount
Any equipment not included as part of the standard en-
gine version and so does not be part of the engine is
not in the scope of supply.
Components especially developed and tested for this
engine are readily available at BRP-Powertrain.
Non-compliance can result in serious injuries or death!
The user assumes all risks possibly arising by utilizing
auxiliary equipment.
The furnishing of proof in accordance to the latest FAR
or EASA has to be conducted by the aircraft manufac-
turer.
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