Rotax 912 ULS 3 - Additional Operating Limits - 912 A;F;UL

Effectivity: 912 A/F/UL BRP-Powertrain page 2-4
OM Edition 2 / Rev. 0 April 01/2010
d04674.fm
Engine start, ope-
rating temperature
Fuel pressure
The aircraft engine manufacturer strongly recommends the instal-
lation of an additional pump, unless this has not been covered by
legal obligations so far.
Propeller go-
vernor
Vacuum pump
External alternator
Bank angle
NOTE: Up to this value the dry sump lubrication system
warrants lubrication in every flight situation.
Max. 50 °C (120 °F)
Min. -25 °C (-13 °F)

WARN
U

WARNING
Non-compliance can result in serious injuries
or death!
Exceeding the max. admissible fuel pressure
will override the float valve of the carburetor
and to engine failure.
Max. 0.4 bar (5.8 psi)
Min. 0.15 bar (2.2 psi)
Power consumption of the hydraulic propeller governor:
Max. 600 W
Power consumption of the vacuum pump:
Max. 300 W
Power consumption of the external alternator:
Max. 1200 W
Deviation from bank angle:
Max. 40°