曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
LOADING
XM Radio Page - active channel field
Acquiring channel audio or information
OFF AIR
XM Radio Page - active channel field
Channel not in service
---
XM Radio Page - active channel field
Missing channel information
WEATHER DATA LINK FAILURE
Weather Datalink Page - center of page
No communication from Data Link Receiver within last 5 minutes
ACTIVATION REQUIRED
Weather Datalink Page - center of page
XM subscription is not activated
Table 8-3 GDL 69/69A Data Link Receiver Error Messages
488 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Additional Features eatures
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Blank Page
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
489
Appendix A
Annunciationsnnunciations and Alerts
CAS Messagesessages
Messages
Description
Inhibits
Warning
Caution
Advisory
ESI
TOPI
AIR
LOPI
ESDI
EMER
GND
AFT DOOR
Tailcone baggage door not fully secured
X
AFT JBOX CB L-R*
Start control circuit breaker (located in aft j-box) tripped
X
AFT JBOX LMT L-R*
Current limiter blown (located in aft j-box)
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Cessna Citation Mustang Pilot’Guide 2(65)
