SECTION 7
AIRPLANE & SYSTEMS DESCRIPTIONS
CESSNA
MODEL 172N
FUEL
QUANTITY
TRANSMITTER
[
FILLER CAP
VENT
(WITH ,_...,....,...,...__.....,_....-��..,
CHECK
VALVE)
•
CONDIT
I
ON
:
SYSTEM SHOWN WITH
FUEL SELECTOR VALVE
IN BOTH POSITION
j::
:=::
,::--
:::
::
:::j
c::::J
CODE
FUEL SUPPLY
VENT
MECHANICAL
LINKAGE
ELECTRICAL
CONNECTION
VALVE
FUEL QUANTITY INDICATORS
11
SELECTOR
VALVE
]
FUEL
QUANTITY
TRANSMITTER
SELECTOR VALVE
DRAIN PLUG
FUEL
STRAINER
-
--
CARBURETOR
FUEL
STRAINER
DRAIN
CONTROL
0
THROTTLE
---
CONTROL
----f_ ..
:
,
---------O �������
TO
ENGINE
•
TO ENSURE MAXIMUM FUEL
CAPACITY WHEN REFUELING
ANO MINIMIZE CROSS-FEEDING
WHEN PARKED ON A SLOPING
SURFACE, PLACE THE FUEL
SELECTOR VALVE IN EITHER
LEFT OR RIGHT POSITION
Figure 7-6. Fuel System (Standard and Long Range)
7-22
1 July 1979
Содержание 17273274
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Страница 123: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS 7 6 Figure 7 2 Instrument Panel Sheet 1 of 2 CESSNA MODEL 172N 1 July 1979 ...
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