P92 Classic Jabiru
M a i n t e n a n c e M a n u a l
SYSTEMS
Page E-3
Date
:
Issue 3: 4
th
July 2011
Section E
Downstream respect to the gascolator is located a fuel filter (11) built in an electric fuel
pump (12) and then the mechanical (13). Mechanical pump feeds the fuel manifold (14);
its left branch feeds the left carburetor. In derivation a tee connector (16) with restrictor
feed the fuel pressure gauge (15). The rear branch of the ”X” manifold (14) is connected
to the fuel return line (17). In case of mechanical pump failure, electrical pump feed is
available.
Return tube (17) engage in pipe fitting (18) located
on the fire-wall and then by means a thin transparent
tube return at the LH fuel tank.
Disassembled wing is necessary disconnect return
tube by means pipe fitting (19). For release of pipe
fitting’s little tube push in direction to the base
knurled flange. For coupling to the tube insert in
your seat.
Periodically check the fuel tank vent (5) to ensure
that their openings are unobstructed; repeat inspec-
tion more frequently if operating in dusty conditions.
It is recommended, for inspection purposes, to use a
small rubber tube to blow through the vent clearing
possible obstructions.
F
IGURE
E-2
G
ASCOLATOR
Drain gascolator daily (see Fig. E-2) using the spring tap (2). Unscrew ring nut (1) for
disconnect bowl and accede at wire mesh filter (4), use particular care at don’t damage
seal (3) and spring (1).
2 - INSTRUMENTATION
The instrument panel, realized in light alloy (see Fig. E-3), is imaginatively divided in
three sections. The left section holds flight control instruments, the right section holds
engine controls and the central section holds eventual communication and navigation in-
struments.
On lower part of instrument panel are the following:
Magneto switches and switches for navigation lights, landing light and strobe light if
installed;