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Rotax OM-912 User Manual

Rotax OM-912
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Fuel pressure
m WARNING
Non-compliance can result in serious injuries or death!
Fuel pressure in excess of stated limit can lead to an override of the
float valve with subsequent engine stop.
The aircraft engine manufacturer strongly recommends the in-
stallation of an additional pump, unless this has not been cov-
ered by legal obligations so far.
Fuel pressure
Max. 0.4 bar (5.8 psi)
(0.5 bar (7.26 psi))
2
Min. 0.15 bar (2.2 psi)
Propeller
governor
Power consumption of the hydraulic propeller governor:
Max. 600 W
Vacuum pump
Power consumption of the vacuum pump:
Max. 300 W
External alternator
Power consumption of the external alternator:
Max. 1200 W
Bank angle
Deviation from bank angle:
Max. 40°
NOTE
Up to this value the dry sump lubrication system warrants lubri-
cation in every flight situation.
Page 2-4
November 01/2016
BRP-Rotax Effectivity: 912 Serie
Edition 4 / Rev. 0
2. applicable only for fuel pump from S/N 11.0036

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Rotax OM-912 Specifications

General IconGeneral
BrandRotax
ModelOM-912
CategoryEngine
LanguageEnglish

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