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X
ANTISKID FAIL
Antiskid Control Unit cannot perform anti-skid functions
X
BATTERY O’TEMP
BATTERY O’TEMP
Overheated NiCad battery (optional)
BATT TEMP FAIL
Battery temperature sensor failure
X
X
CABIN ALT
CABIN ALT
CABIN ALT
Cabin altitude potentially unsafe
X
X
X
CABIN DOOR
Cabin door not fully secured
X
CHECK DOORS
A door monitor has not been properly tested or has failed
X
X
X
X
DUCT O’HEAT L-R*
Duct temperature too high or sensor disconnected
X
X
ENG A/I COLD L-R*
ENG A/I COLD L-R*
Engine anti-ice system ON and inlet temperature is cold
X
X
ENG CTRL SYS L-R*
FADEC has a fault that requires maintenance
ENGINE FAIL L-R*
An engine has failed
F/W SHUTOFF L-R*
Fuel firewall shutoff valve fully closed
X
FLAPS FAIL
A flap system failure has occurred.
X
FUEL BOOST L-R*
FUEL BOOST L-R*
Electric fuel boost pump ON. Caution condition is displayed when the boost pump is operating in abnormal conditions.
X
FUEL FLTR BP L-R*
Engine fuel filter impending bypass switch closed
X
FUEL LO INOP L-R*
Fuel low level function failure
X
X
FUEL LVL LO L-R*
Fuel level in tank is too low
X
FUEL PRES LO L-R*
Fuel pressure too low
X
X
FUEL TRANSFER
Fuel transfer valve open
X
GEN OFF L-R
GEN OFF L-R*
One or both electrical generators offline
HYD PRESS LO
Hydraulic system pressure too low
X
X
HYD PUMP ON
Hydraulic pump running too long
X
X
NOSE DOOR L-R*
One or both nose baggage doors not fully secured
X
MFD COLD
MFD temperature is below -20° C
NO TIRE SPINDOWN
Antiskid control spindown function not working
X
X
OIL PRESS LO L-R*
Oil pressure less than redline low limit
X
X
X
OXYGEN OFF
Oxygen supply off
X
X
X
P/S HTR L-R*
No current detected to pitot static heater
X
PRESS CTRL
PRESS CTRL
Pressure controller loss of integrity
X
X
X
PRESS OFF
Air Source Selector switch in OFF or fresh air position
X
X
SPD BRK EXTEND
Speed brakes extended
X
STALL WARN FAIL
Failure detected in stall warning system
X
X
X
X
STALL WARN HI
Stall warning system on ice-contaminated schedule
X
X
STALL WARN HTR
No power delivered to stall warning vane heater
X
X
SURFACE DE-ICE
De-ice boots inflating/deflating as designed
X
T2 HTR FAIL L-R*
T2 probe heater failure
X
X
X
TAIL CONE BLD LK
Tailcone temp high, possible bleed air leak.
X
X
X
TAIL DE-ICE FAIL
De-ice system not operating normally
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:
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Cessna Citation Mustang G1000 Integrated Flight Dec(166)
