Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Quest KODIAK
™
100
190-00645-07 Rev. A
86
Annunciations & Alerts
Flight
InstrumentsEIS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
Aural Alert Description
“TIS not available” The aircraft is outside the Traffic Information Service (TIS) coverage
area.
“Traffic Advisory System Test
Passed”
“TAS System Test Passed”
Played when the optional traffic system passes a pilot-initiated
self test.
- SKY 497 TAS
- GTS 800 TAS
“Traffic Advisory System Test
Failed”
“TAS System Failed”
Played when the optional traffic system fails a pilot-initiated self
test.
- SKY 497 TAS
- GTS 800 TAS
“One o’clock” through
“Twelve o’clock”
or “No Bearing”
Intruder bearing (GTS 800 only).
“High”, “Low”, “Same
Altitude” (if within 200 feet of
own altitude), or “Altitude not
available”
Intruder relative altitude (GTS 800 only).
“Less than one mile”,
“One Mile” through “Ten Miles”,
or “More than ten miles”
Intruder distance (GTS 800 only).
COMPARATOR ANNUNCIATIONS
Comparator
Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
IAS MISCOMP
If both airspeed sensors detect < 35 knots, this is inhibited.
If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10
kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7
kts.
HDG MISCOMP
Difference in heading sensors is > 6 degrees.
PIT MISCOMP
Difference in pitch sensors is > 5 degrees.
ROL MISCOMP
Difference in roll sensors is > 6 degrees.
ALT NO COMP
No data from one or both altitude sensors.