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Cessna 402C - Page 226

Cessna 402C
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SECTION
7
AIRPLANE
&
SYSTEMS
DESCRIPTIONS
FUEL
SYSTEM
SCHEMATIC
FUEL QUANTITy GAGE
,........---------{~EI--------__,
FUEL
VENT
VALVE
" /
""
//
FUEL
~
~
FUEL
FILTER
ltY
~
fiLTER
FUEL
SELECTOR
VALVES
RIGHT
MAIN TANK
i~~~-]~1t+_~f:;?'"";F~~~~
IvN:tvKEEs:",-=::::~~~:~~~llf~;--;~~n
-~~--'/:F
~ ~
~I
L~~
~Yp~S
__
r--....:<--
FUEL
VENT
VALVE
FUEL
FLOW
GAGE
THROTTLE
MIXTURE
TO CYLINDERS
LEFT ENGINE
DRIVEN FUEL
INJECTION
PUMP
RIGHT ENGINE
DRIVEN
FUEL
INJECTION
PUMP
RIGHT ENGINE
FUEL
CONTROL
UNIT
THROTILE
MIXTURE
VAPOR RETURN
FUEL
VENT
CROSSFEED FUEL
FUEL FILLER
FUEL
INJECTION
NOZZLE
(TYPICAL)
FUEL
SUPPLY
CODE
~
CHECK VALVE
MECHANICAL
ACTUATION
ELECTRICAL ACTUATION
DRAIN VALVE
FUEL
QUANTITY
TRANSMITTER
FUEL
INJECTION
NOZZLE
(TYPICAL)
Figure
7-16
52987008
1
November
1979
D
....
"..;~..;n
..
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lI"n
lORl