Reversionary Sensor Annunciations; Afcs Alerts - Garmin Cessna Caravan G1000 Cockpit Reference Manual

Annunciations & Alerts

REVERSIONARY SENSOR ANNUNCIATIONS

Reversionary
Sensor Window
Text
BOTH ON ADC1
BOTH ON ADC2
BOTH ON AHRS1
BOTH ON AHRS2
BOTH ON GPS1
BOTH ON GPS2
XSIDE ADC
XSIDE AHRS

AFCS ALERTS

Alert Condition Annunciation
Rudder Mistrim
Right
Rudder Mistrim
Left
Aileron Mistrim
Right
Aileron Mistrim
Left
Elevator Mistrim
Down
Elevator Mistrim
Up
Pitch Trim Failure
(or stuck MEPT
Switch)
Yaw Damper
Failure
60
Garmin G1000 Cockpit Reference Guide for the Cessna Caravan
Both PFDs are displaying data from the number one Air Data Computer.
Both PFDs are displaying data from the number two Air Data Computer.
Both PFDs are displaying data from the number one Attitude & Heading Reference
System.
Both PFDs are displaying data from the number two Attitude & Heading Reference
System.
Both PFDs are displaying data from the number one GPS receiver.
Both PFDs are displaying data from the number two GPS receiver.
The PFD displaying this annunciation is displaying data from the cross-side Air Data
Computer.
The PFD displaying this annunciation is displaying data from the cross-side Attitude &
Heading Reference System.
Yaw servo providing sustained force in the indicated
direction. Aircraft rudder retrim after substantial pitch and
power changes required.
Roll servo providing sustained force in the indicated direction
Pitch servo providing sustained force in the indicated
direction. May indicate a failure of the pitch trim servo or
trim system.
If AP engaged, take control of the aircraft and disengage AP
If AP disengaged, move MEPT switches separately to unstick
YD control failure; AP also inoperative
Condition
Description
190-00748-00 Rev. C