Piper Malibu PA-46-310P Pilot Operating Handbook page 357

BENDIX/KING
SECTION 6
SYSTEM DESCRIPTION
AND
OPERATION
20. REMOTE HARKER BEACON LIGHTS - Remote Airway, Outer and
Middle Marker Beacon lights driven by the Harker Beacon
receiver.
21. YAV DAMPER SVITCH (OPTIONAL) - Hay be used to engage and
disengage the Yaw Damper independent of the autopilot.
Illuminates continuously. (This switch is not required for
Yaw Damper installation and is a convenience option).
22. AUTOPILOT CONTROL VHEEL SVITCH ASSEMBLY - Switch assembly
mounted on the pilot's control wheel associated with the
autopilot and manual electric trim systems.
23. AUTOPILOT DISCONNECT/TRIM INTERRUPT (A/P DISC/TRIM INTER)
Switch - Vhen depressed will disengage the autopilot and
yaw damper and cancel all operating Flight Director modes.
Vhen depressed and held will interrupt all electric trim
power (stop trim motion), disengage the autopilot and yaw
damper and cancel all operating Flight Director modes.
24.
CONTROL VHEEL STEERING (CVS)
BUTTON -
Vhen depressed,
allows pilot to manually control the aircraft (disengages
the pitch and roll servos) without cancellation of any of
the selected modes. Vill engage the Flight Director mode
if not previously engaged. Automatically synchronizes the
Flight Director/Autopilot to the pitch attitude present
when the CVS switch is released, or to the present pressure
altitude vhen operating in the
ALT
hold mode. Vill cancel
GS couple. The aircraft must pass through the glideslope
again to allow GS recouple. The CVS button will not
disengage the Yaw Damper Servo.
FIGURE 1 ICING
I.CAP
150 AUTOPILOT
SYSTEM
CONTROLS
AND INDICATORS
Piper Models
PA-46-310P and PA-46-350P
Airplane Flight Manual Supplement
006-0428-01
Page 28 of 39
PAA
Approved
Revision 4
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