Specifications

CHEROKEE
SIX
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Fuel
Drain Lever
Fuel
quantity gauges
for
each
of
the
four
tanks
are
located
in
the engine
l3uge
cluster on
the
left
side
of the instrument
panel.
A fuel
pressure
indictor is also
incorporated
in the engine
gauge
cluster.
An electric
fuel
pump
is
provided
for
use
in
case
of failure
of the engine
driven
pump.
The
electric
pump
operates
from
a single switch
and
independent
circuit
protector.
It should be
ON
for
all takeoffs
and landings.
ELECTRICAL
SYSTEM
The
l4-volt electrical system
includes
a
l2-volt
brttery for
starting
and to back up alternator
output. Electrical
power
is supplied
by a 60
ampere
rlternaior.
The battery,
a
master
switch
relay, a
voltage
regulator
and an overvoltage
relay are located
beneath
the floor
of
the
forward
baggage
compartnient,
and
access
is obtained by
removing
the
floor.
Electricel switches
are located
on a
panel
to the
pilot's
left
and
all circuit breakers are
on the
lower
right instrument
panel
behind
a decorative
door.
Two thumb-wheel
rheostat switches
to the
left
of
the
circuit
breakers
control
the
navigation
lights
and the
intensity
of
the instrument
panel
lights.
AIRPLANE
AND
SYSTEMS
REVISED:
JUNE 20,1974
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