Cessna 182 1978 - Fuel Quantity Transmitters; Integral Fuel Bay Components

MODEL
182 & T182 SERIES
SERVICE MANUAL
*-~1 1' t ~1. Upper Wing Skin
I/
2
2. Filler
Cap
2,J ^^~ / ~3.
Access
Cover
4.
Stiffeners
5.
Wing
Main
Spar
.~"*-
(j. '"4~
%
-
.
6
6. Lower
Wing
Skin
/*'*C - ''--
\s
3
7. Outlet
Baffles
wj\ ''--.t ^-q f - \ / 8. Wing Rib (Cell Wall)
\'^ '-'--_ '-;'
'.-: ."y., ,,
9. Fuel Vent
\ '..
'"::;. ""--
<
10.
Vent
Valve
4
11. Interior
Ribs
(Bafles)
<:A
:I^.
'".C -
1
12. Front
Wing
Spar
\'"^
.
"1
J,
_
\
13.
Interior
Vent
D
I:_~ /.s^ 14. Root
Rib.
|ft \y ^^s. ' k; ;-.,-<-- ^15. Quantity Transmitter
C \ 9s16_/ . Finger Filter
C15K
17. Hat
Section Stiffener
^^. ^^<^e-at
Ax^-.
\
s
^
When
applying
sealant in the
fuel bay,
DO
( Gus$?
t
^\^ ^ < ^ ~>^
\^ NOT plug fuel drain path
below hat section
Beginning
with Serial 18288475,
\
/
~~~~~~~~~i.
inspection
plate (18)
fasteners
lat
12
17
7
7chag
fom
3
each
NOTE
'.'
A i. "'.>
loss,
bay is acceptable.
Do
not attempt to apply
pressure to the bay
i. Reseal
and retest if a leaks
are found.
without
a good regulator
and a positive shut-
off in thesplie ontinlth ul1-0When
applyinsu sealant
iin
the
fuel
bay,TERS. One
bay to
more than 1/2 psi or damage may
float-actuated, variable-resistive transmitter
is
y tomooccur eha 2sodmae
a located in eachp fuel
drain path below hat s connected onc-
trically to separate
galvanometric
gages, one for
r
skin
(6).
Apply pressure slowly untl 1/2
PSI is obtained each
tereby ndicl
82level
n each
bay.
Apply
soap solution as requition
and procedur
fteor
oper
change
from 3 each
to 6 each.
Figure 12-12. Integrai
Fuel Bay Components
(1 of 4)
h. Allow
15 to 30 minutes form pressure to stabilize.
aton and mintenance are contained
in Secton 15.
losRevson,
bay
is accep
ble29
J. Reseal and retest
if any leaks are
found.
without a good regulator and a positive shut-
off in
the supply
line.
Do
not inflate
the
fuel
12-50.
FUEL
QUANITY
TRANSMITTERS.
One
bay to
more than 1/2 psi or damage
mary
float-actuated,
variable-resistive transmitter
is
occur.
located
in each fuel bay. They
are connected elec-
trically
to separate galvanometric
gages, one
for
f. Apply pressure slowly
until 1/2 PSI is obtained. each bay,
thereby indicating fuel level in each bay.
g. Apply
soap solution as required.
A complete description
and procedures
for oper-
h.
Allow
15 to 30
minutes
for pressure
to stabilize.
ation
and maintenance
are
contained
in Section
15.
Revision I 12-29