Jabiru Aircraft
Pty Ptd
Aircraft Service Manual
Jabiru J230-C
REVISION
0
Dated : Feb 2006
Issued By: RAS
Page: 131 of 171
L:\files\Technical_manuals\J230_J430\J230.J430_Work_files\J230-C_Tech_Rev_1.doc
Print Date: 14/01/2009 4:41:00 PM
12.7.2
FUEL FILTER REMOVAL & INSTALLATION
1.
Drain fuel system, wing tanks and header tanks.
2.
Place a cloth beneath the filter to collect any fuel which may be split during removal
of the filter.
3.
Disconnect the fuel lines at both ends of the filter.
4.
Remove filter.
5.
Reverse the preceding steps for installation. Ensure waste cloth is removed.
WARNING
Ensure wing tank cap vent covers are removed.
The fuel filter must only be installed in one direction. An arrow on the side of the
filter marks the fuel flow direction. Ensure this arrow is pointed towards the
Firewall and Engine.
12.8 FUEL PUMPS
12.8.1
PRIMARY PUMP
The Primary Fuel Pump is located on the Starboard rear of the Engine. Refer to engine
Maintenance & Instruction Manual for details.
12.8.2
SECONDARY PUMP
A secondary, electronic pump is mounted inside the header tank enclosure behind the
rear cabin bulkhead. This pump is a back-up to the Primary Pump. It is recommended
that the Secondary Pump be engaged at least during take-off and landing.
