Fuel Quantity Transmitters; Integral Fuel Bay Components - Cessna T182 Series Service Manual

MODEL 182 & T182 SERIES SERVICE MANUAL
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~1.
Upper Wing Skin
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2. Filler Cap
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Access Cover
4. Stiffeners
5. Wing Main Spar
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6. Lower Wing Skin
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\s 3 7. Outlet Baffles
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10. Vent Valve
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11. Interior Ribs (Bafles)
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12. Front Wing Spar
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^15. Quantity Transmitter
C \ 9s16_/ . Finger Filter
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17. Hat Section Stiffener
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When applying sealant in the fuel bay, DO
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\^ NOT plug fuel drain path below hat section
Beginning with Serial 18288475, \ /
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inspection plate (18) fasteners lat
12
17
7
7chag fom 3 each
NOTE
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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