Piper Turbo Saratoga PA-32-301T Pilot's Manual page 279

PIPER AIRCRAFT CORPORATION SECTION 9
PA-32-301T, TURBO SARATOGA SUPPLEMENTS
CAUTIONS
Flight
Director Autopilot
versions only are
equipped
with a remote
go-around
switch.
When G|A mode is selected the
AUTOPILOT
WILL DISCONNECT and warning
horn
will
sound.
Pilot
may use
Flight Director steering
for
missed approach
guidance and after aircraft
is stabilized in a proper climb with gear and
flaps
up
autopilot
may
be re-engaged and will
retain
G|A
mode. Autopilot only versions
do
-
not
have
a G/A switch.
To avoid inadvertent or false glideslope
cap-
tures
while operating
on the localizer
use
NAV
mode
instead of APR
mode.
Refer
to
Edo-Aire Mitchell
Century 41
Operator's Manual, P/N 68S803, dated 1-79
for
additional
System Description and
Normal
Operating
Procedures.
(b)
PREFLIGHT PROCEDURES
NOTE
During
system
functional
check the system
must be provided adequate
D.C.
voltage
(12.0
VDC
min.)
and instrument
air
(4.2
in. Hg.
min.).
It is recommended that the engine be
operated to provide
the necessary power and
that the
aircraft
be positioned
in
a
level
atti-
tude, during the functional check.
(i)
AUTOPILOT (F/D
Switch ON
if F/D
Equipped)
a.
Engage
autopilot
by
pushing
programmer
OFF
-
ON
switch
ON.
b.
Rotate
D.G. .HDG
bug left then right
and
verify
that
control wheel movement corresponds
to HDG command
input.
c.
Press pitch modifier
button
first up then
down
and note
that pitch control follows pitch command input. Autotrim
shouId follow pitch command input after approximately
three second delay.
ISSUED: OCTOBER 2, 1980
REPORT: VB-1070
9-55