Piper Turbo Saratoga PA-32-301T Pilot's Manual page 249

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PIPER
AIRCRAFT
CORPORATION
SECTION
9
PA-32-301T,
TURBO
SARATOGA
SUPPLEMEliTS
(5)
CYC
Pushbutton
switch
used
to
select cyclical
contour
mode.
Data is presented alternately
as
normal
for 0.5 seconds, then contoured
for 0.5
seconds.
Prcssing switch
a second
time
restores
normal
or
WX
mode.
(6)
Range Field
Maximum
selected
range
is
displayed.
Maximum
range
is
always
displayed
when
indicator is
in on-condition.
(7)
Test Field
Test
block
displays
three
illumination
levels.
(8)
Range Mark
Individual
label displayed
for
each
range
Identifier
mark.
(9)
Mode Field
Operating
mode
is
displayed
as
WX
or
CYC.
When system
is first
turned
on,
WAIT is
displayed
until
system
times
out
(30-40
seconds).
(b)
PRELIMINARY
CONTROL
SETTINGS
Place the Indicator
controls
in the
following
positions
before
applying
power from the
aircraft
electrical
system:
INTensity
control.............
Fully counterclockwise,
in OFF
TILT control.................................Fully
upward
RANGE
switch............................
12
nautical
miles
(c)
OPERATIONAL
CONTROL
SETTINGS
(1)
Rotate
INTensity
control
clockwise
to
bring
system
into
ON condition.
(2)
Note
that
WAIT
is displayed
during
warm-up
period
of
30-40
seconds.
(3)
When WX is displayed,
rotate
INTensity
control
clockwise
until display brightness
is at desired level.
(4)
Set RANGE
switch to desired range.
(5)
Adjust TILT control
for
desired
forward
scan area.
ISSUED:
JANUARY
10, 1980
REPORT:
VB-1070
9-25

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