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Piper Cherokee 140 Owner's Handbook Manual page 19

Piper cherokee 140 aircraft owner's handbook

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THE
PIPER CHEROKEE
SECTION
II
the
tank
selector
valve
must
be switched
to
each tank
in
turn,
with
the
electric
pump on,
and
the
gascolatordrainvalve
open-
ed.
Each
tank
has an
individual
qulck
drain
located
at
the
bot-
tom, inboard, rear corner.
Fuel quantity
and
pressure
are
indicated
ongauges located
in
the engine gauge
cluster
on
the
right
side
of
the instrument
panel,
ELECTRICAT
SYSTEM
The
Cherokeeisequippedwith
thepiper
F.T.p. (Full
Time
Power)
Electrical
System,
ICs
12
volt alternatorprovides
elec-
trical
power
at all
engine
speeds
and
results
in
improved
per-
formance
for
radlo
and
electrical
equipment and
longerbattery
life.
In additionto
thealternator,
the
electrical
system includes
a 25 ampere-hour
baEery,
a
voltage
regulator
and a master
switch
relay.
The
battery
and
relay are
mounted beneath
the
baggage
compartment
floor.
Access
for
service
or
inspection
is
obtained
by raising the
hinged baggage
compartment
floor
panel. The
battery
box is
designed
to
accommodate
a
Larger
capacity
battery for
extreme
cold
weather
operation.
Electrical
switches,
fuses
and fuse
spares
are
located
on
the
lower
left
side
of
the
in-
strument
panel.
Standard
electrical
acce
s
-
sories,
in additiontothose
al-
ready
Iisted,
include
a
starter,
stall
warning
indicator, cigar
lighter
and
ammeter.
Mvi-
gation
lights,
anti-collision
light,
landing
Iight, instrumenr
lighting
and
a
cabin
dome
light
are
offered
as
optional
acces-
6s0630

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