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SMOKE BAGGAGE FAIL Smoke detector installed in the baggage compartment has failed (one or both
smoke detectors installed in baggage compartment have failed) 9
SMOKE CABIN FAIL Smoke detector in cabin has failed (Global Express only) 9
SMOKE CLOSET FAIL One or more (i.e. up to four) closet smoke detectors have failed 9
SPLR LEVER FAIL The flight spoiler function for at least two pairs of flight spoilers is inoperative.
The ground lift dumping and roll assist functions are not affected 10
STAB TRIM
Displayed to alert the crew that the pitch trim function is not available due to both
pitch trim channels inoperative (failure, channel disconnect through PTRIM
DISCONNECT pushbutton, master disconnect switch pressed for more than 5
continuous seconds)
10
STALL PROTECT FAIL Pusher has failed, has been manually deactivated, a SPC channel has failed, an
AOA sensor has failed, or the pusher switch is enabled 10
START ABORTED L (R) FADEC has aborted an automatic start 17
STBY PITOT HT FAIL Standby pitot heat has failed 7
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
7-52 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
THROTTLE FAIL L (R) Corresponding throttle has failed. Engine operation will be affected as a function
of aircraft configuration 17
TRIM AIR FAIL Trim air failed (overheat) 10
TRIM AIR LEAK Leak detected in trim air duct 13
UNCOMMANDED BRAKE Brake on when pedals not applied 14
WINDOW HEAT FAIL L (R) Left/right side window temperature controller has failed and cannot heat 3
WING A/ICE FAIL L (R) Low temperature, left/right WAI valve closed or left/right bleed off with CBW
closed 3
WING A/ICE LEAK Bleed leak detected in wing anti-ice duct 11
WING A/ICE LO HEAT Low temperature detected on affected wing 3
WING FUEL HI TEMP Either the left or right or both wing fuel temperature is high 11
WING FUEL LO TEMP Either the left or right or both wing fuel temperature is low 11
WING FULL L (R) Left or right wing fuel overfill 11
WING TO CTR LEAK Wing tank to center tank leak 11
WOW FAIL Loss of WOW function 14
WSHLD HEAT FAIL L (R) Left/right windshield temperature controller has failed and cannot heat 3
XBLEED FAIL Bleed crossfeed failed (open or closed) 13
YD 1 (2) FAIL Affected yaw damper failed 2
YD 1-2 FAIL YD 1 and 2 fail 2
YD OFF FWC detects no YD engaged 2
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
For Training Purposes Only
Sept 04
7-53
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
ADVISORY MESSAGES (CYAN)
CAS MESSAGE DESCRIPTION CH.
→ FUEL XFER ON Left to right fuel transfer on 11
→ XFER VALVE OPEN Left to right transfer valve open 11
← FUEL XFER ON Right to left fuel transfer on 11
← XFER VALVE OPEN Right to left fuel transfer valve open 11
A/T 1-2 FAIL A/T 1 and/or 2 has stopped communicating or is invalid (as determined by
FWC), or the A/T reports a hardware or servo failure 17
A/T ADC MISCMP Selected A/T system is unavailable due to ADC data miscompare required for
dual coupled approach A/T operation 17
A/T IRS MISCMP Selected A/T system is unavailable due to IRS data miscompare required for
dual coupled approach A/T operation 17
AC BUS 1 (2) (3) (4) XFER
FAULT Transfer of alternative power supply to AC BUS1-2-3-4 may be lost 6
ADC 1 (2) (3) DEGRADED Set when the displayed ADC is unreliable. Degraded static error correction.
Note: To be reviewed when triple failure condition for RVSM criteria 16
ADC 1 (2) (3) FAIL Annunciated when either ADC1, ADC2 and/or ADC3 has failed 16
AFCS 1 (2) FAIL
Fault Warning determines that one or both AFCS function/s failed, either by
examining in-line validity or by invalidating data being transmitted. The AFCS
function includes the YD, Autopilot and Flight Director
2
AFT R/D VALVE OPEN AFT refuel/defuel valve failed open (not applicable to Global 5000) 11
AFT XFER FAULT AFT tank fuel transfer fault (not applicable to Global 5000) 11
AFT XFER OFF SCHED AFT tank fuel transfer off schedule (not applicable to Global 5000) 11
AP 1-2 FAIL Both autopilots are failed 2
APU BATT CHGR FAIL APU battery charger has detected a fault and shutdown 6
APU BLEED DISABLED
Annunciated when the LCV command is received and either the aircraft is
above 35,000 ft. Or the 60 second warm-up period after speed reaches 99% is
not complete (ground only)
4
APU FADEC FAIL Annunciated when no data is received by the DAU 4
APU FAULT
Annunciated when failure of a single speed sensor or EGT thermocouple rake is
detected or the fuel solenoid has failed to close or the fuel/oil filters have gone
　
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