be
turn&
off
by
the
master switel~ whicla actuates a relay locat&
at
the
battery. The master switch for the electrical system
is
located at the %e%-hand side of
the
flight panel. The electrical
system operates
all
the e%eetrlcal accessories listed below:
1,
Radios
2.
Engine starter
3,
Starter vibrator
4.
Navigation lights and interior lights
5.
Landing light
6.
Rotsting beaeon
(if
installed)
7,
Heated pirot
(if
installed)
8,
Turn and bank
(if
installed)
9,
Cigarette
lighter
10.
Electric lalading gear (if installed)
I
I.
F
ue% gages
12.
Electric fuel
pump
13.
Stall warning horn
14,
Landing gear warning horn and warning
ligh9.s
NOTE:
The engine has
its
own separate
electrical
system
and
will
ccistfnue to run, even though
ehe
master
switch has been turned off, or even t*!;~ugh the ac-
cessory electrical
systeln Should malfuriceion,
bion is provided
by
two adjustable spot lights
mourned on the headliner. These lights are controlled
by
a rheostat
located on the headliner near the
lights. The
fuel
selector valve
is illuminated by
a
small light 1-~~ounted under the panel
on
the
left
side.
The
intensity of this light is controlled
by
rotating
the
lens housing. The
cabin
light, located on the headliner near
the center of the cahi.n, can be used to illuminate the pailel if
the
instrurnenr lighrs malfunction,
Electrical Load Meter
lneter in
the
engine instrument cluster
sholrrs
the amperage being produced by the generator.
This
in-
strument
is
not directly associared
with
the
battery circuit and,
therefore, will not directly indicate if the battery
is
charging
or discharging. In
riorl11a.l flight, the alnperage reading
will
be
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