Pitch Wheel; Autopilot Controller - Honeywell PRIMUS 1000 Pilot's Manual

PRIMUSr1000 Integrated Avionics System
Message
AP AIL MISTRIM
AP ELEV MISTRIM
AUTO TRIM FAIL
AUTOPILOT FAIL
YAW DAMPER FAIL
Amber (Caution) Flight Guidance System Messages

AUTOPILOT CONTROLLER

The autopilot controller shown in figure 6--2, is used to manually control
the autopilot through the PITCH wheel and TURN knob.
P
I
T
C
H

PITCH Wheel

Rotating the PITCH wheel with the autopilot engaged changes the pitch
attitude proportional to the rotation of the wheel and in the direction of
wheel movement. Movement of the PITCH wheel cancels only altitude
hold or altitude preselect capture.
Flight Guidance System (FGS)
6-6
Autopilot has detected the aileron out
of trim.
Autopilot has detected the elevator out
of trim.
Autopilot elevator trim has failed.
The autopilot has failed.
Autopilot has detected that the yaw
damper has failed.
Table 6--3
DESCEND
CLIMB
Autopilot Controller
Figure 6--2
Description
TURN
AD--50485@
A28--1146--112--00