Piper Turbo Saratoga PA-32-301T Pilot's Manual page 252

SECTION 9
PIPER AIRCRAFT CORPORATION
SUPPLEMENTS PA-32-301T, TURBO SARATOGA
SECTION 4
-
NORMAL
PROCEDURES
PREFLIGHT INSPECTION
(a)
AutoFlite Il master switch
-
ON.
(b)
Rotate
turn command knob to left and right. Aircraft
control
wheels should rotate in
corresponding
directions.
(c)
With AutoFlite
Il on, rotate aircraft control wheel to left and right.
Only
light forces should be
required
to
override roll servo clutch.
(d)
AutoFlite
Il master
switch
-
OFF
-
rotate
control wheel
left
and
right
to
assure
disengagement.
IN-FLIGHT PROCEDURE
(a)
Engagement
(1)
Check turn command knob
in center detent position.
(2)
AutoFlite
11 master switch
-
ON.
(b)
Disengagement
(I)
AutoFlite 11 master switch
-
OFF.
(c)
Heading
Changes
(1)
Move
trim
knob on
instrument for drift correction
from
a
constant
heading.
(2)
Move turn command
knob for left or right
banked turns.
Rotation of
knob
to stop will yield an appropriate
bank
angle
to obtain
an approximate
standard
rate turn. Intermediate
settings may
be
used
for lesser turn
rates.
(d)
OMNI Tracker
(1)
Turn command knob
-
move to center detent position and push
IN
to
engage tracker.
Aircraft will track desired radial estab-
lished on NAV f
(or
as selected, if equipped with a NAV
selector switch).
NOTE
Tracker
must be engaged
within
10° of being
"on
course,"
i.e. VOR course needle centered
and aircraft heading
within
a
10° of VOR
course.
REPORT: VB-1070 ISSUED: APRIL 4, 1980
9-28 REVISED: MAY 16, 1980