Piper Malibu PA-46-310P Pilot Operating Handbook page 334

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BENDIX/KING
SECfION 2 - LIMITATIONS
A. During autopilot operation, a pilot with seat belt fastened
must be seated at the left pilot position.
B. The autopilot and yaw damper must be OFF during takeoff and
landing.
c.
The system is approved for Category
I
operation only
(Approach mode selected).
D.
Autopilot maximum airspeed limitation:
185 KIAS
E. Maximum fuel imbalance with the autopilot engaged: 10
Gallons.
F. Continued autopilot or manual electric trim system use is
prohibited following abnormal or malfunctioning operation,
and prior to corrective maintenance.
G. The entire preflight test procedure outlined under Section
4, paragraph A of this supplement, including steps l
through 10, must be successfully completed prior to each
flight. Use of the autopilot or manual electric trim system
is prohibited prior to completion of these tests.
8.
The PITCH TRIM circuit breaker must be pulled following any
inflight illumination of the red TRIM warning light, but
only after first completing the Emergency Procedures
(Section 3) paragraph A. The manual electric trim and
autopilot autotrim systems will be disabled with the PITCH
TRIM circuit breaker pulled.
I. Altitude Select captures below 800 feet AGL are prohibited
(when the optional KAS 297B Altitude/Vertical Speed
selector is installed).
J.
Do not override the autopilot to change pitch or roll
attitude.
K. The autopilot must be disengaged below 200 feet AGL during
approach operations and below 800 feet AGL for all other
phases of flight.
L. Required Placards:
1. Adjacent to autopilot mode controller (KC 191/KC 192):
FAA Approved
Revision 4
Alll' O Pn.OT AND
El.£CTRIC TRlM
PR£fl JGHT TESTS
MUST
B(
COHOUCT£D
PRIOR TO EACH
ruGHT
Piper Models PA-46-310P and PA-46-350P
Airplane Flight Manual Supplement
006-0428-01
Page
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