Piper Turbo Saratoga PA-32-301T Pilot's Manual page 281

PIPER
AIRCRAFT CORPORATION SECTION 9
PA-32-301T, TURBO
SARATOGA SUPPLEMENTS
Any failure of
the
preceding operations indicates that
a
failure
exists in
the
system
and
the
Command
Trim
shall
not
be
operated
until
the failure has been identified and corrected.
Autotrim
-
Before
the
First Flight of Each Day
(1)
Check trim
master
switch ON, autopilot
OFF.
(2)
Press and hold TEST pushbutton on Mode Annunciator.
Verify the following
sequence. (Each sequence will last approx-
imately
two seconds.):
a.
All annunciations light with FAIL and AP flashing.
b.
Autotrim flashes, goes steady,
then flashes.
c.
All lights go steady.
d.
After
three to five seconds, AUTOTRIM and FAIL flash
continually.
(3)
With TEST
button
on
the Mode Annunciator still depressed,
verify
Trim
will not operate
in
either
direction with the Control
Wheel Switch.
(4)
Release
TEST
pushbutton. All lights
except
HDG
and
ATT
shall extinguish.
Any deviation from the
above sequence
indicates that
a
failure
exists in either
the
primary system or in the monitor circuits.
The
autopilot
and trim
system
shall not be operated until the failure has
been identified
and corrected.
CAUTION
Recheck
trim position prior to
initiating
take-
off.
(d)
FLIGHT DIRECTOR
(1)
Check circuit
breaker
-
IN.
(2)
Flight director switch on steering
horizon
-
ON. (Adjacent to
instrument on single cue horizon, if installed)
(3)
Pitch modifier DN
-
UP
-
check pitch steering
indicator
moves
appropriately.
(4)
HDG bug RT
-
LT
-
check roll steering indicator
moves
appropriately.
ISSUED:
OCTOBER
2,
1980
REPORT: VB-1070
9-5T