Cessna 210B - Fuel System Schematic; Fuel Selector Valve; Fuel Quantity Data; Auxiliary Fuel Pump Switch

Description
Description
-Fu el cannot be used from bol h tank s simu ltaneously.
FUEL QUANTI , TY DATA I (u.s. GALLONS) I
fUel QUANTITY INDICATORS
LEfT
LEfT •
- '''
•
V'
RIGHT RIGHT
'" ~'
~' __ ' ~. , fUEL TANK
CHECK
fiLLER
~ ""'-.... fillER CHECK
VAl VI: .
CAP
./"" ... FUel QUANTITY TRANSMITTERS ..... ~ CAP VALVE
fUEL TANK
~
STANDARD TANKS
LEFT TANK] 31.7 31.9 I
RIGHT TANK~ 31.7 . 31.9
40.0 41.0 41.9
I
4 2.0
RIGHT TANK
40.0
41.0 41.9
42 .0
I I
SELECTOR
VALVE
POSITION
USABLE FUEL
(ALL FLIGHT
CONDITIONS)
USABLE FUEL
(LEVEL FLIGHT
ONLY)
USABLE
FUEL
(CLIMBING.
DESCENDING)
TOTAL
VOLUME
32.4
32.4
LONG RANGE TANKS (OPTIONAL)
LEFT TANK I
DECREASE IN USABLE FUel IN All FLIGHT CONDITIONS IS DUE TO DETRIME N TA l
EFFECTS
OF UNCOORDINATED FLIGHT (SLIPS OR SKIDS) OR TURBULENT A IR T HA I
MAY BE ENCOUNTERED IN NORMAL FLYING CONDITIONS .
Figure 1-2.
reservoir tank.
Refer to figure 1- 2 for fuel quan-
tity data. See the Servicing Diagram
(figure 6-1) for a summary of fuel
system servicing information.
FUEL SELECTOR VALVE.
The rotary-type fuel selector valve
has three positions, labeled " BOTH
OFF," "LEFT ON" and "RIGHT ON. "
The "BOTH OFF" pOSition seals
both wing tanks off from the rest of
the fuel system and allows no fuel
to pass beyond the selector valve.
The "LEFT ON" position provides
fuel flow from the left tank to the
engine. Similarly, the "RIGHT ON"
pOSition
provides flow from the right
tank to the engine. Both the fuel feed
and vapor return lines for each tank
go throogh the selector valve, so that
fuel returns to the tank from which it
is drawn. Fuel cannot be us ed fro"1
both tanks simultaneoosly.
NOTE
The fuel selector valve hall ill ,
indicates the setting of t he V; i t \'
by its pOSition above the ~I I, I
Take off and land with the h:III"1
turned to the fullest tank .
AUXILIARY FUEL PU MP SWllrll
The auxiliary fuel pu mp
controls both of the ele ctric , lljili
iary pumps which supp ly 1111 I Ii
for starting and for en gi nl ' III" I "
if the engine-driven pump 11 111 .1 1 '1 I
The switch is a split to !" I II I I 1
The right half of the switrh , l.thi
1
\
" LO, " operates only one PUtllp. I
viding sufficient fuel fo r (JIIIII III
starting. The left hal! uf 1111
~ ~
FUEl R ESER VOIR
WITH DRAIN PLUG
SOLENOID
VALVE (OPT)
O IL
DILUTION
SWITCH
(OPT)
...
TO OIL SYSTEM
CODE
~ FUEL SUPPLY
IIIIIIIIIIIIIIl EXCESS FUel
AND VAPOR
_ RETURN FUEl
MECHANICAL
LINKAGE
~ ELECTRICAL
CONNECTION
8
FILTER
THROTTlE 0 SCREEN
~- - ' - ---
l1fE:2J
AIR THROTTLE
FUEl SYSTEM
SCHEMATIC
,.,.
fUEL flOW
GAGE
,-'.'1":\ :' /"'>" ,:7' , >, :',: " ,,, :?': '. ,'. ,'
fUEL NOZZLES
Figure 1-3.
1-5
1-4