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SECTION
7
AIRPLANE & SYSTEMS DESCRIPTIONS
CESSNA
MODEL
172N
FUEL
OUANTITY
T
RANSM ITTE
R
FUEL
OUANTI
TY
TRANSMITTE
R
FILLER
CAP
TO
ENSURE MAXIl!1UM FUEL
CAPACITY WHEN REFUELING
AND
MINII\4IZE
CROSS FEED
NG
WHEN
PARKED
ON
A
SLOPING
SURFACE, PLACE
THE
FUEL
SELECTORVALVE
N ElTHER
LEFT ON RIGHT
POSITION
Figure 7-6. Fuel System (Standard
and
Long
Range)
7-22
1
JuIy
1979
FUEL
OUANTITY
INDICATORS
VE
NT
lWITH
CHECK
LEFT FI]EL TANK
VALVE)
SELECTOH
VALVE
DRAIN
PLUG
FUEL
STRAINER
DRAI
N
CONT
ROL
CONDI
TION:
SYSTEM
SHOWN
WITH
FUEL SELECTOR
VALVE
IN
BOTH POSITION
SE
LECTOR
VALVE
CARBUR ETOR
CODE
rTIIl
FUEL
SUPPLY
MECHANICAL
LINKAGE
L
ELECTRICAL
CONNECTION
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