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Rotax 914 series Installation Manual

Rotax 914 series
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page 22
July 01/2008
Effectivity: 914 Series
Edition 2 / Rev. 0
d04275
INSTALLATION MANUAL
BRP-Rotax
- engine suspension frame
- expansion tank (coolant)
- electric starter (standard or starter with extended power output)
- integrated AC generator with external rectifier regulator
- oil tank
- external start relay
- drive of hydraulic governor (on configuration 3 only)
Auxiliary equipment (optional)
CAUTION: Any equipment not included as part of the standard engine version and
thus not a fix component of the engine is not in the volume of supply.
Components especially developed and tested for this engine are
readily available at BRP-Rotax.
Following auxiliary equipment has been tested on ROTAX engine type 914 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.
- external alternator
- vacuum pump (feasible on configuration 2 and configuration 4 only)
- drive for tachometer/hour-meter
- oil cooler with connections
- coolant radiator
- coolant overflow bottle

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Rotax 914 series Specifications

General IconGeneral
Bore79.5 mm
Stroke61 mm
Compression Ratio9.0:1
Cooling SystemLiquid-cooled cylinder heads, air-cooled cylinders
Redline5800 rpm
Engine Type4-cylinder, 4-stroke
Fuel TypeAvgas 100LL
Oil SystemDry sump
Fuel Systemfuel injection
TBO (Time Between Overhauls)2000 hours
Displacement1.211 liters (1211 cc)
Power Output84.6 kW (115 hp) at 5, 800 rpm

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