Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Quest KODIAK
™
100
190-00645-07 Rev. A
88
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
AFCS ALERTS
The following alert annunciations appear in the AFCS System Status field on the PFD.
Condition Annunciation Description
Pitch Failure
PTCH
Pitch axis control failure. AP is inoperative.
Roll Failure
ROLL
Roll axis control failure. AP is inoperative.
Yaw Damper Failure
YAW
YD control failure; AP is inoperative
Pitch Trim Failure
(or stuck MEPT Switch)
PTRM
If AP engaged, take control of the aircraft and
disengage AP
If AP disengaged, move MEPT switches
separately to unstick
System Failure
AFCS
AP and MEPT are unavailable. FD may still be
available.
Elevator Mistrim Down
↓ELE
Pitch servo providing sustained force in the
indicated direction. May indicate a failure of the
pitch trim servo or trim system.
Elevator Mistrim Up
↑ELE
Aileron Mistrim Right
AIL →
Roll servo providing sustained force in the
indicated direction
Aileron Mistrim Left
← AIL
Rudder Mistrim Right
RUD →
Yaw servo providing sustained force in the
indicated direction. Aircraft rudder retrim after
substantial pitch and power changes required.
Rudder Mistrim Left
← RUD
Preflight Test
PFT
Performing preflight system test; aural alert
sounds at completion
PFT
Preflight system test failed; aural alert sounds at
failure
NOTE: Do not press the AP/YD DISC TRIM INTRPT switch during servo
power-up and preflight system tests as this may cause the preflight system
test to fail or never to start (if servos fail their power-up tests). Power must
be cycled to the servos to remedy the situation.