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X
W/S A/I FAIL L-R*
W/S A/I FAIL L-R*
Loss of power to windshield heater
X
W/S O’HEAT L-R*
W/S O’HEAT L-R*
Windshield anti-ice power ON; temperature too high
X
WING DE-ICE FAIL
De-ice system operating abnormally
X
WOW MISCOMPARE
Gear on-ground inputs do not agree
X
X
X
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here display L-R for example.
190-00494-02 Rev. B
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
490
Appendix A
Name
Inhibit
EMER
Emergency Bus Mode Inhibit
ESI
Engine Start Inhibit
TOPI
Takeoff Operation Phase Inhibit
AIR
In-Air Inhibit
LOPI
Landing Operation Phase Inhibit
ESDI
Engine Shutdown Inhibit
GND
On-Ground Inhibit
Red annunciation window text signifies warnings; yellow, cautions; and white, annunciation advisories. See the Airplane Flight Manual (AFM) for recommended pilot actions.
Comparatoromparatoromparatoromparator Annunciationsnnunciations
The Comparator monitors critical values generated by redundant sensors. If differences in the sensors exceed a specified amount, this discrepency will be annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare) as seen in Figure A-1. If one or both of the sensed values are unavailable, it will be annunciated as a ‘NO COMP’ (no compare). The following is a list of the possible annunciations:
Figure A-1 Sensor Comparator WindowComparatorWindow
Comparator Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
IAS MISCOMP
If both airspeed sensors detect < 35 kts, this is inhibited.
If either airspeed sensor detects > 35 kts, and the difference in sensors is > 10 kts.
If either airspeed sensor detects > 80 kts, and the difference in sensors is > 7 kts.
HDG MISCOMP
Difference in heading sensors is > 6º.
PIT MISCOMP
Difference in pitch sensors is > 5º.
ROL MISCOMP
Difference in roll sensors is > 6º.
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..
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
491
Appendix A
Reversionaryeversionary Sensor Annunciationsnnunciations
Reversionary sensor selection is annunciated in the Reversionary Sensor Window, as shown in Figure A-2. These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey gives access to ADC1, ADC2, AHRS1, and AHRS2 Softkeys. These softkeys allow manual switching of sensors. In the case of certain types of sensor failures, the G1000 may make some sensor selections automatically. The GPS sensor cannot be switched manually.
Figure A-2 Reversionary Sensor WindowsReversionarySensorWindow
Reversionary Sensor Window Text
Condition
BOTH ON ADC1
Both PFDs are displaying data from the #1 Air Data Computer.
BOTH ON ADC2
Both PFDs are displaying data from the #2 Air Data Computer.
BOTH ON AHRS1
Both PFDs are displaying data from the #1 AHRS.
BOTH ON AHRS2
Both PFDs are displaying data from the #2 AHRS.
BOTH ON GPS1
Both PFDs are displaying data from the #1 GPS receiver.
BOTH ON GPS2
Both PFDs are displaying data from the #2 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.
USING AHRS2
PFD1 is displaying data from the #2 AHRS.
USING GPS1
PFD2 is displaying data from the #1 GPS.
USING GPS2
PFD1 is displaying data from the #2 GPS.
G1000 Systemystem Annunciationsnnunciations
When a new message is issued, the MSG Softkey will flash to alert the flight crew of a new message. It will continue to flash until acknowledged by pressing the softkey. Active messages are displayed in white text. Messages that have become inactive will change to gray text. The MSG Softkey will flash if the state of a displayed message changes or a new message is displayed. The inactive messages can be removed from the Message Window by pressing the flashing MSG Softkey.
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Cessna Citation Mustang Pilot’Guide 2(66)
