Garmin Software Version 0720.10 Betriebsanweisung Seite 86

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Seitenansicht 85
G1000 Cockpit Reference Guide for the Piper PA-46 Mirage/Matrix
190-01107-00 Rev. A
70
Annunciations & Alerts
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
COMPARATOR ANNUNCIATIONS
Note that operating the system in the vicinity of metal buildings or other metal
structures can cause sensor differences that may result in nuisance miscompare
annunciations during start up, shut down, or while taxiing.
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 >
15 kts.
If either airspeed sensor detects > 80 knots, and the difference in sensors is
> 10 kts.
HDG MISCOMP
Difference in heading sensors is > 10 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.
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