PRIMUS
r
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
The autopilot controller shown in figure 6--2, is used to manually control
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
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.
