Effectivity: 914 Series BRP-Powertrain page 1-10
OM Edition 2 / Rev. 0 April 01/2010
d04473.fm
1.6) Standard version
Serial production - 4-stroke, 4 cylinder horizontally opposed, spark ignition engi-
ne with turbocharger and electronic control of boost pressure
(TCU = turbocharge control unit), one central cam-shaft -
push-rods - OHV
- Liquid cooled cylinder heads
- Ram air cooled cylinders
- Dry sump forced lubrication
- Dual breakerless capacitor discharge ignition
- 2 constant depression carburetors
- 2 electric fuel pumps (12 V DC)
- Electric starter (12 V 0.7 kW)
- Integrated AC generator with external rectifier-regulator (12 V
20 A DC)
- Prop drive via reduction gear with integrated shock absorber
and overload clutch
NOTE: The overload clutch is installed on all serial
production aircraft engines which are certified
and on non-certified aircraft engines of the con-
figuration 3.
- Stainless steel exhaust system
- Engine suspension frame
Optional - Electric starter (12 V 0.9 kW)
- External alternator (12 V 40 A DC)
- Vacuum pump: (only for configuration 2 and 4 possible)
- Hydraulic constant speed propeller governor: (for configurati-
on 3 only)
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