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Garmin G1000 Cockpit Reference Guide for the Socata TBM 850
190-00708-02 Rev. A
68
Annunciations & Alerts
Flight
InstrumentsEAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
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.
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
Condition
BOTH ON ADC1
Both PFDs are displaying data from the number one Air Data Computer.
BOTH ON ADC2
Both PFDs are displaying data from the number two Air Data Computer.
BOTH ON AHRS1
Both PFDs are displaying data from the number one Attitude & Heading Reference
System.
BOTH ON AHRS2
Both PFDs are displaying data from the number two Attitude & Heading Reference
System.
BOTH ON GPS1
Both PFDs are displaying data from the number one GPS receiver.
BOTH ON GPS2
Both PFDs are displaying data from the number two GPS receiver.
USING ADC1
PFD2 is displaying data from the #1 Air Data Computer.
USING ADC2
PFD1 is displaying data from the #2 Air Data Computer.
USING AHRS1
PFD2 is displaying data from the #1 AHRS.