Piper Turbo Saratoga PA-32-301T Pilot's Manual page 282

SECTION
9
PIPER AIRCRAFT
CORPORATION
SUPPLEMENTS PA-32-301T,
TURBO
SARATOGA
(e)
COMPASS SYSTEM (NSD 360A)
(For other compass
systems,
refer to appropriate
manufacturer's
instructions)
(1)
Check
slaving switch
in
slave or slave 1 or
2 position, as appro-
priate.
(Slaying
systems with R.M.L output provide only slave
and free
gyro positions.)
(2)
Rotate
card to center slaving
meter
-
check HDG displayed
with
magnetic
compass
HDG.
(3)
Perform standard VOR
receiver
check.
(4)
NAV -
APPR
-
Engage
NAV or APPR mode switch and
observe steering bar indicates turn toward
the VOR needle.
NOTE
lf the Omni Bearing Selector is
more
than 45°
from the aircraft
heading,
the flight director
steering bar will only
indicate a turn toward the
omni bearing.
(f)
IN-FLIG.HT PROCEDURE
-
FLIGHT
DIRECTOR
(l)
Century 41 circuit
breaker -
IN. Flight director
switch
-
ON.
(2)
Adjust
HDG bug
to aircraft heading and select
desired
pitch
attitude
by
activation of the CWS (Pitch Synch) switch or the
modifier
switch.
(3)
Maneuver
aircraft manually
to satisfy the commands
pre-
sented.
Select
other modes as desired; refer
to
Century 4I
Operator's Manual for mode description.
(g)
IN-FLIGHT PROCEDURE
-
AUTOPILOT/FLIGHT
DIREC-
TOR AUTOPILOT
(1)
Flight director
switch
-
ON, if F/D equipped. Rotate heading
bug to desired heading.
(2)
Trim aircraft for
existing
flight condition
(all
axes). Engage
autopilot.
(3)
During
maneuvering
flight
-
control aircraft through
use
of the
HDG bug
and the pitch modifier. (HDG-ATTmodes)
(For use
of pitch synch switch see Operator's Manual.)
(4)
For navigation
operations
select modes
as required
by the
operation
being conducted
and in accordance with the mode
description provided in Operator's Manual. For specific
in-
structions relating to coupled instrument approach operations,
refer
to
Special Operations
and Information Section 4, item
(i).
REPORT:
VB-1070 ISSUED: OCTOBER 2, 1980
9-58