Piper CHEROKEE D - Page 17

CHEROKEE
"D"
SECTION
II
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
the
lower
right
instrument
pane
1.
A
rheostat
switch
on
the
left
side
of
the
switch
panel
controls
the
navigation
lights
and
the
dome
instru-
ment
light.
It
also
dims
the
dome
light.
The
similar
switch
on
the
right
side
controls
and
dims
the
panel
lights.
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ALTERNATOR
ENGINE
FUEL
STALL
GYRO
AUTO
Pi
TOT TURN
6:
PITCH
START
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OUTPUT FIELD GROUP
PUMP
WARNING
WARNING
PILOT
HEAT BANK
TRIM
6.
ACC
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~
INSTRUMENT
LIGHTSI
NAV
I
ROTATING
I
LANDING NAY-COM NAY-COM
ADF
AUDIO
MARKER
·
PANEL OVERHEAD
LIGHTS BEACON LIGHTS I 2 AMPLIFIER BEACON
.
Circuit
Breaker
Panel
730130
9