71-00-00
page 14
October 01/2010
Effectivity 912/914 Series
Edition 1 / Rev. 3
d04775
BRP-Powertrain
Maintenance Manual
DIRECTION OF counterclockwise, seen from the front in the direc-
ROTATION: tion of the propeller flange
OVERLOAD CLUTCH: multi-disk clutch
VACUUM PUMP drive via the gearbox
(optional):
PROPELLER PITCH drive via the gearbox
GOVERNOR (optional):
TURBOCHARGER: Exhaust gas turbine with wastegate, radial-flow com-
pressor T25
3)
TURBOCHARGER electronic, proportional plus integral plus derivative
CONTROL UNIT (TCU):regulator with 2 external indicating lamps
3)
CERTIFICATION: 912 A: in acc. with JAR 22
912 F: in acc. with FAR 33
912 S: in acc. with FAR 33 and JAR-E
914 F: in acc. with FAR 33 and JAR-E
CERTIFICATION 912 A: EASA.E.121
912 F: EASA.E.121, E00051 EN
912 S: EASA.E.121, E00051 EN
914 F: EASA.E.122, E00058 NE
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