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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
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-02 Rev. A 54
Annunciations & Alerts
Flight
Instruments
EICAS
Nav/Com/
XPDR/Audio
AFCS
GPS Nav
Flight
Planning
Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/Alerts
Appendix
Index
Messages
Description
Inhibits
Warning
Caution
Advisory
ESI
TOPI
AIR
LOPI
ESDI
EMER
GND
MFD COLD
MFD temperature is below -20° C
NOSE DOOR L-R*
One or both nose baggage doors not fully secured
X
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.
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
190-00600-02 Rev. A Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 55
Annunciations & Alerts
Flight
Instruments EICAS
Nav/Com/
XPDR/Audio AFCS GPS Nav
Flight
Planning Procedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
Alerts Appendix Index
Comparator Annunciations
Comparator Window Text
Condition
ALT MISCOMP
Difference in altitude sensors is > 200 ft.
　
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