d04918.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 Series
Edition 2/Rev. 0
00-00-00
page 5
August 01/2012
2.1) Standard version
Serial production - 4 stroke, 4 cyl. horizontally opposed, spark ignition engine, single cen-
tral camshaft hydraulic tappets - push rods - OHV
- Liquid cooled cylinder heads
- Ram air cooled cylinders
- Dry sump forced lubrication
- Dual ignition of breakerless, capacitor discharge design
- 2 constant depression carburetors
- Mechanical fuel pumps
- Electric starter (12 V 0.7 kW), 912 S/ULS (12 V 0.9 kW)
- Integrated AC generator with external rectifier regulator
- Propeller drive via integrated gearbox with mechanical shock absorber
and overload clutch
NOTE: The overload clutch is installed on all serial production
aircraft engines which are certified and non-certified air-
craft engines of the configuration 3.
Optional - Electric starter (12 V 0.9 kW)
- External alternator (12 V 40 A DC)
- Vacuum pump (only for configuration 1, 2 and 4 possible)
- Hydraulic constant speed propeller governor (only for configuration 3)
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