Rotax 912 series Operator's Manual page 36

Aircraft engines
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9.
Power consumption of the hydraulic propeller governor:
max. ............................................ 600 W
10.
Power consumption of the vacuum pump:
max. ............................................ 300 W
11.
Power consumption of the external alternator:
max. ............................................ 1200 W
12.
Deviation from bank angle
max. ............................................ 40°
13.
Rotation reverse the direction of engine rotation
max. ............................................ 1rotation
Effectivity: 912 ULS / S
OM Rev. 1
NOTE:
Up to this value the dry sump lubrication system
warrants lubrication in every flight situation.
AIRCRAFT ENGINES
page 10 - 6
Nov. 01/2002

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