Piper Malibu PA-46-310P Pilot Operating Handbook page 333

BENDIX/RING
SECTION 1
GENERAL
o.
E.
Roll rates in excess of 14° per second vill cause the
autopilot to disengage except vhen the CVS switch is held
depressed.
Pitch rates in excess of
90
per second vill cause the
autopilot to disengage except vhen the CVS switch is held
depressed.
The airplane BATT HASTR function is unchanged and can be
used in an emergency to shut off electrical power to all
flight control systems while the problem is isolated.
The RADIO HASTR switch supplies power to the avionics bus
bar of the radio circuit breakers and the autopilot circuit
breaker.
The following circuit breakers are used to protect the
following elements of the King 150 Series Autopilot:
LABEL
AUTOPILOT
PITCH TRIM
COMPASS
FUNCTION
Supplies power to the KC 192 or the KC 191
Computer, the autopilot pitch and roll
servos, the optional
KA
185 Annunciator and
the Pitch Trim Circuit Breaker. It also
applies power to the KC 296 Yaw Computer, the
Yaw Servo, and the KAS 2978 Altitude/Vertical
Speed Selector, when installed.
Supplies power to the autotrim and manual
electric pitch trim systems.
Supplies power to
Compass System and
Rate Gyro if the
with an inverter.
the optional KCS SSA
the optional KRG 331 Yaw
airplane is not equipped
ENCODING ALT Supplies power to the King KEA 130A
Altimeter, when installed.
Piper Models PA-46-310P and PA-46-350P
Airplane Flight Manual Supplement
006-0428-01
Page 2 of 39
FAA Approved
Revision 4
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