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once the channel has cooled down. Always displayed in conjunction with “FLAP
FAULT”
10
FLAPS HALFSPD System operating at half speed 10
FLT SPOILERS FAULT
Displayed if one of a single pair of flight spoilers is inoperative (may be retracted
or deployed); objective is to allow dispatch with this message, provided that
affected panels are verified to be retracted. (In the event of hydraulics failure,
message inhibited if panels are retracted)
10
FMS 1 (2) (3) FAIL Either FMS is reporting a failure or the FMS data transmitted is invalid 16
FUEL COMPUTR FAULT Fuel computer fault (one of the two channels only) 11
FUEL FILTER L (R) Left or right impending fuel filter bypass 11
FUEL QTY DEGRAD Fuel quantity degraded accuracy 11
FUEL RECIRC ON Fuel recirculation on in an unauthorized configuration (not applicable to Global
5000 and -9 FMQ GC or later) 11
GEAR SYS FAULT Loss of redundancy for downlock indications or EICAS communication 14
GEN 1 (2) (3) (4) FAIL Gen 1, 2, 3 and/or 4 has failed 6
GND LIFT DUMP For one pair of ground spoilers, the ground lift-dump function is inoperative; or, a
ground spoiler upfloat is occurring in flight 10
GND PROX FAIL EGPWS INOP and NOT SUPPRESSED when EGPWS SYSTEMS FAIL
message is displayed (i.e. COMPUTER FAIL or EGPWS not communicating) 16
ADVISORY MESSAGES (CYAN)
CAS MESSAGE DESCRIPTION CH.
7-56 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
GPWS SYSTEMS FAIL COMPUTER FAIL or EGPWS not communicating 16
HUMIDIFIER FAIL Humidifier failed 13
HYD EDP 1A (2A) FAIL Indicates that the hydraulic engine driven pump 1A-2A is not producing
pressure (< 1800 psi) when it should be 12
HYD PUMP 1B (2B) (3B)
FAIL
Indicates that the hydraulic electrical pump 1B-2B-3B is not producing pressure
(< 1800 psi) when it should be 12
HYD PUMP 3A FAIL Hydraulic pump 3A not producing 1800 psi 12
IAC 1 (2) (3) INVALID Invalid software configuration in IAC, or incorrect aircraft ID 7
IAC 1 (2) (3) MEM FULL Trend and/or Exceedance memory is more than 80% full. Continued use will
overwrite previous recordings 7
IAC 1 (2) (3) WOW INOP WOW discrete into IAC is failed, resulting in no power-up testing and possible
function loss 7
IAC 1 (2) AURAL FAIL No 28V power to aural warning, or BIT failure being indicated 7
IAC CONFIG MISMTCH IACs not configured with the same options or aircraft configuration 7
ICE Cowl or wing icing detected with anti-ice systems on (left/right cowl and wing) 3
ICE DETECTOR FAULT Loss of one ice detector 3
IRS 1 (2) (3) AUX FAIL Annunciated when the indicated IRU backup power source has failed 16
IRS 1 (2) (3) AUX PWR Annunciated when the indicated IRS has lost its normal power source and has
reverted to Auxiliary DC power 16
IRS 1 (2) (3) FAIL Annunciated when the indicated IRS has failed. (IRU detects an internal failure) 16
IRS 1 (2) (3) NO ALIGN Set when IRS fails to properly align: e.g., annunciated due to improper position
entry or excessive airplane motion while in align mode 16
LTRK FAIL Annunciated when the LaserTrak (third navigation source for a dual FMS
installation) has failed or has been selected off 16
MACH XDUCER FAIL Mach transducer has failed 7
MAN PRESS FAULT One of the two altitude limitation systems in inoperative in the associated
manual channel 13
MFD CTLR 1 (2) FAIL Loss of one side’s MFD controller 16
MLG BAY OVHT FAULT Main landing gear bay detection element system fault (one channel of the
system is unreliable, other channel is still operational) 14
NAV LIGHTS FAIL Both the primary/secondary navigation lights for either the left wing or right wing
have failed or one minimum of the tail navigation lights have failed 1
NO TAKEOFF Indicates that the airplane is not configured for takeoff during taxi 7
OIL FILTER L (R) Left and/or right impending oil filter bypass 17
OIL RES LO QTY Oil system requires replenishment 17
OUTFLOW VLV 1 (2) FAIL Fwd/Aft outflow valve inoperative 13
ADVISORY MESSAGES (CYAN)
CAS MESSAGE DESCRIPTION CH.
For Training Purposes Only
Sept 04
7-57
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
PACK FAULT L (R) Left and/or right pack fault 13
PASSENGER OXY ON Oxygen, either manually selected or automatically turned on, is flowing to the
main cabin oxygen masks 1
PITCH DISC FAULT Pitch disconnect solenoid has failed in the locked or unlocked position 10
PITCH FEEL FAULT Displayed to alert the crew that either pitch feel is inoperative, or degraded
(force gradient not nominal) on one or both channels 10
PRI FUEL PUMP L (R) Left and/or right primary (AC) fuel pump failure 11
　
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