Piper Malibu PA-46-310P Pilot Operating Handbook page 356

•
BENDIX/KING
SECl'ION 6
SYSTEM DESCRIPTION
AND
OPERATION
14. FLIGHT DIRECTOR (FD) MODE SELECTOR BUTTON - Vhen pushed
vill select the Flight Director mode (vith KC 192 Autopilot
Computer only), bringing the Command Bar in view on the
KI
256 and will command wings level and pitch attitude hold.
The FD mode must be selected prior to Autopilot engagement.
15. VERTICAL TRIM CONTROL - A spring loaded to center rocker
svitch which vill provide up or dovn pitch command changes:
while in ALT will adjust altitude at rate of about 500 fpm;
vhen not in ALT will adjust pitch attitude at a rate of .7
deg/sec. Vill cancel GS couple. The aircraft must pass
through the glideslope again to allow GS recouple.
16. KAP 150 SYSTEM KC 191 AUTOPILOT COMPUTER - Complete
Autopilot computer, including system mode annunciators and
system controls.
17. KA 185 REMOTE MODE ANNUNCIATOR (OPTIONAL) - Provides mode
annunciation in the pilots' primary scan area as well as
three Harker Beacon lights.
18. ARMED (ARM) ANNUNCIATOR - Illuminates continuously along
with NAV or APR when either the NAV or APR mode selector
button is depressed. The
ARM
annunciator vill continue to
illuminate until the automatic capture sequence is
initiated at which time ARM will extinguish and CPLD will
annunciate.
19. COUPLED (CPLD) ANNUNCIATOR - Illuminates continuously along
with NAV or APR at the initiation of automatic beam capture
sequence in either the NAV or APR modes. Normally the CPLD
condition follows an ARM condition but may be entered into
directly if the beam capture criteria is met when NAV or
APR is selected •
FAA
Approved
Revision 4
FIGURE 1
ICING KAP
150 Atrl'OPILOT SYSTBH
CONTROLS AND INDICATORS
Piper Models PA-46-310P and PA-46-350P
Airplane Plight Manual Supplement
006-0428-01
Page 27 of 39