P92 Classic Jabiru
M a i n t e n a n c e M a n u a l
SYSTEMS
Page E-2
Date
:
Issue 3: 4
th
July 2011
Section E
1 - FUEL SYSTEM
The fuel system (see Fig. E-1) consists of two metallic fuel tanks (1) located in the wing’s
leading edge after wing-fuselage union. Each fuel tank has 45 liters capacity. On the up-
per external is refueling’s cap (2), bay (3) for float (4) chamber and fuel tank bleed (5).
Metal cover plate (6) may be removed for inspection of tank interior that assembly riveted
and puttied with dope gasoline resistant. Return line discharged flange (7) of fuel system
on the left fuel tank rear wall placed. At each fuel tank outlets are present (and servicea-
ble by specific port holes) fuel mesh filters (8).
F
IGURE
E-1
F
UEL
S
YSTEM
Diaphragm mechanical pump (13), engine connected, stoking provide by means flexible
pipelines come to the fuel tank and across cabin vertical rods, easily accessible, after dis-
assembled plastic structural. On the same cabin vertical rods are circuit on-off valve (9),
one for each fuel tank, easily accessible to the pilot. Circuit link with union tee in corres-
pondence of the firewall, and then to drainage bowl (10), located left upper side in the en-
gine bay, visible through an upper cowling port.
