Cessna 152 - Page 122

SECTION7
AIRPLANE & SYSTEMS DESCRIPTIONS
CESSNA
MODEL 152
FUEL QUANTITY INDICATORS
. FUEL
£[ _ ____.__.__I I ----
QUANTITY
TRANSMITTER
FILLER CAP
VENT
(WITH
CHECK
VALVE)
CONDITION:
• TO ENGINE
SYSTEM
SHOWN WITH
FUEL SHUTOFF
VALVE
IN ON POSITION
CODE
Eifilll!J FUEL SUPPLY
c:::J VENT
..__
MECHANICAL
LINKAGE
ELECTRICAL
CONNECTION
FUEL SHUTOFF
VALVE
m-
~t"
m
FUE
ORAi
F
STR
------0
FUEL
STRAINER
DRAIN
CONTROL
m
f
!!
CARBURETOR
TO ENGINE
--
--
THROTTLE
CONTROL
--0
---- O'
--
MIXTURE
CONTROL
Due to crossfeeding between fuel
tanks, the tanks should be re-
topped after each refueling
to
assure maximum capacity.
Figure 7-6. Fuel System (Standard and Long Range)
7-20
1 July 1978