Honeywell SPZ-8000 Pilot's Manual page 145

Digital integrated flight control system
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SPZ--8000 Digital Integrated Flight Control System
Table 6--6 lists the primary caution message annunciators.
Message
PITCH TRIM FAIL
MISTRIM [TRIM
NOSE UP/DN]
MISTRIM [TRIM
NOSE R/L]
MISTRIM [TRIM R/L
WING DN]
EXCESSIVE DEV
Primary Caution Messages (Steady)
Automatic Flight Control System (AFCS)
6-12
Timed--out
Reset
(5 Sec)
Light On
No
No
No
No
No
Table 6--6
Comments
No
Pilot must
manually
disconnect
autopilot (AP).
This action also
clears the
messages.
No
Message is
displayed only
while excessive
loads are sensed
at the elevator
servo.
No
Message is
displayed only if
the linear
actuator remains
off center.
No
Message is
displayed only
while excessive
loads are sensed
at the aileron
servo.
No
Message clears
when aircraft is
within CAT 2
lateral and
vertical limits.
A28--1146--055
REV 2

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