Comparator Annunciations; Reversionary Sensor Annunciations - Garmin G1000 Reference Manual

CompArAtor AnnunCiAtions

Comparator
Window text
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
If both airspeed sensors detect < 35 knots, this is inhibited.
IAS MISCOMP
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.
IAS NO COMP
No data from one or both airspeed sensors.
HDG NO COMP
No data from one or both heading sensors.
PIT NO COMP
No data from one or both pitch sensors.
ROL NO COMP
No data from one or both roll sensors..

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
USING ADC1
USING ADC2
USING AHRS1
190-00600-02 Rev. A
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.
PFD2 is displaying data from the #1 Air Data Computer.
PFD1 is displaying data from the #2 Air Data Computer.
PFD2 is displaying data from the #1 AHRS.
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Annunciations & Alerts
Condition
Condition
55