Rotax 912 i Series Installation Manual page 87

Introduction
The fuel flows from the tanks via the water trap/fine filter to the electrical
fuel pumps; from there it flows to the injection lines, the injection valves
and the fuel pressure regulator. The fuel pressure regulator feeds any
surplus fuel back to the tank.
This section of the Installation Manual contains information on the aircraft
Table of contents
engine fuel system.
Requirements of the fuel system
Connections for Bowden cable actuation and permissible load
Effectivity: 912 i Series
Edition 1/Rev. 0
BRP-Powertrain
INSTALLATION MANUAL
Chapter: 73-00-00
FUEL SYSTEM
The design of the fuel system is the responsibility of
NOTICE
WARNUNG
the aircraft manufacturer.
The fuel system must be designed to ensure that the
engine is supplied with sufficient fuel at the correct
pressure in every operational situation. Operating lim-
its must be adhered to!
Subject
Operating limits
Fuel temperature
Fuel pressure indicator
Technical data
Fuel lines
Coarse filter
Water trap
GENUINE- ROTAX fuel pump assy. (optional)
General requirements placed on the fuel pump
Technical data
Requirements on cable actuation
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73-00-00
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January 01/2012