SECTION II
CHEROKEE ''ARROW"
nut plates. This allows easy removal for service or inspection.
The fuel selector control is located on the left side panel, forward
of the pilot's seat. If a modified selector valve cover has been installed,
the button on the selector cover must be depressed and held while the
handle is moved to the OFF position. The button releases automatically
when the handle is moved back into the ON position.
An auxiliary electric fuel pump is provided-i~- case ~f failure
of the engine driven pump. The electric pump should be on for all
take-offs and landings, and when switching tanks. The pump
switch is located in the switch panel above the throttle quadrant.
Each tank has an individual quick drain located at the
bottom, inboard, rear corner, and should be drained to check for
water before each flight. The fuel strainer, which is also equipped
with a quick drain,
is
located on the front lower left corner of
the firewall. This strainer should be drained regularly to check
for water or sediment accumulation.
Fuel quantity and pressure are indicated on gauges located
in
a cluster on the left side of the instrument panel.
ELECTRICAL SYSTEM
The electrical system includes a 12 volt 60 amp alternator,
battery, voltage regulator, overvoltage relay and master switch
relay. The battery
is
mounted in a stainless steel box imme-
diately aft of the baggage compartment. The regulator and over-
voltage relay are located on the forward left side of the fuselage
behind the instrument panel.
Electrical switches are located on the right center instru-
ment pane 1, and the circuit breakers are located on ~he lower
right instrument pane
1.
A rheostat_-swi~ch on the left stde . of the
switch panel controls the navigahon hghts and the dome mstru-
ment light.
It
also dims the dome light. The similar switch on
the right side controls and dims the panel lights.
.
Standard electrical accessories include starter, electnc
fuel pump, stall warning indicator, cigar lighter, voltmeter, and
12
730320
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