Honeywell PRIMUS 1000 - Autopilot Controller; PITCH Wheel

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Flight Guidance System (FGS)
6-6
Message Description
AP AIL MISTRIM Autopilot has detected the aileron out
of trim.
AP ELEV MISTRIM Autopilot has detected the elevator out
of trim.
AUTO TRIM FAIL Autopilot elevator trim has failed.
AUTOPILOT FAIL The autopilot has failed.
YAW DAMPER FAIL Autopilot has detected that the yaw
damper has failed.
Amber (Caution) Flight Guidance System Messages
Table 6--3
AUTOPILOT CONTROLLER
Theautopilotcontrollershown infigure6--2,is usedto manuallycontrol
the autopilot through the PITCH wheel and TURN knob.
AD--50485@
TURN
P
I
T
C
H
DESCEND
CLIMB
Autopilot Controller
Figure 6--2
PITCH Wheel
RotatingthePITCH wheelwiththeautopilotengagedchangesthepitch
attitude proportional to the rotation of the wheel and in the direction of
wheel movement. Movement of the PITCH wheelcancels only altitude
hold or altitude preselect capture.