曝光台 注意防骗
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fire detection capability for left or right engine) 9
ENG FLAMEOUT L (R) Left or right engine flameout 17
ENG FUEL LO TEMP L (R) Left/right engine inlet fuel temperature is below 5°C with engine running 17
ENG FUEL SOV L (R) Left and/or right engine fuel shutoff valve failure 17
ENG OVERSPED L (R) Left and/or right engine shutdown caused by Independent Overspeed Protection 17
ENG OVHT L (R) Left and/or right turbine cooling air overheat 17
ENG SAV FAIL L (R) Corresponding engine start air valve failure 17
FADEC FAIL L (R) Major FADEC failure in both lanes. Engine operation may be affected 17
FADEC N1 CTL L (R) Left and/or right engine is in N1 control; left and/or right FADEC has detected a
fault and reverted to N1 control 17
FADEC OVHT L (R) Internal EEC temperature monitor tripped 17
FIRE BTL1 LO PRESS Extinguishing bottle #1 low pressure 9
FIRE BTL2 LO PRESS Extinguishing bottle #2 low pressure 9
FLAP FAIL Flap actuation inop 10
FLAP FAULT Flaps have been shut down 10
FLT SPLR DEPLOYED Displayed to alert crew that flight spoilers are deployed at low altitude (RA
between 10 and 300 ft.) or when throttle is at high power 10
FLT SPOILERS FAIL Displayed if control of at least 2 pairs of flight spoilers fail. In case of loss of
hydraulic power, failure is declared only if panel is upfloating 10
FUEL COMPUTR FAIL Fuel computer failure 11
FUEL FILTER L (R) Left and right fuel filter bypass 11
FUEL IMBALANCE Fuel imbalance 11
FUEL LO PRESS L (R) Left and/or right low engine fuel feed pressure with the HPSOV open 17
FUEL LO QTY Low fuel quantity 11
FUEL RECIRC FAIL L (R) Recirculation valve not in commanded position 11
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
For Training Purposes Only
Sept 04
7-49
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
FUEL TEMP SENSOR Bulk fault temperature no longer reliable 11
FUEL UNIT MISMATCH Fuel unit discrepancy between the fuel quantities displayed on the EICAS and
the Refuel/Defuel Panel 11
GEAR DISAGREE Gear not at selected position within 30 seconds of command or any gear unsafe 14
GEAR SYS FAIL Normal gear operation not available 14
GEN 1 (2) (3) (4) OVLD There is an overload on generator 1, 2, 3 or 4 6
GND LIFT DUMP
Displayed when:
· System power-on self tests detects a valve jammed in the deploy position.
· During T.O. or landing:
GLD not armed (loss or absence of automatic sum or OFF switch which affects
at least two pairs of spoilers (i.e. GS or MFS)
· GLD is lost or degraded (deployment delayed) for at least two pairs of spoiler
(GS or MFS), due to loss of one ground condition
· Two pairs of ground spoilers failed in retracted position (unless associated
hydraulics is low)
· One pair of ground spoilers failed in retracted position and one pair of flight
spoilers failed.
10
HYD 1 (2) (3) HI TEMP Indicates that hydraulic system No. 1-2-3 oil temperature is hot (≥ 96°C) 12
HYD 1 (2) (3) LO PRESS Indicates that hydraulic system No. 1-2-3 oil pressure is low (<1800 psi) 12
HYD 1 (2) (3) LO QTY Hydraulic system fluid level is too low for normal aircraft operation during flight 12
HYD 1-2 LO PRESS Indicates that both hydraulic systems have less than 1800 psi 12
HYD 1-3 LO PRESS Indicates that both hydraulic systems have less than 1800 psi 12
HYD 2-3 LO PRESS Indicates that both hydraulic systems have less than 1800 psi 12
HYD 3 OVERFILLED On ground, hydraulic system 3 fluid quantity exceeds 70% of its capacity.
Current level does not allow for fluid replacement when landing gear is retracted 12
HYD RAT PUMP FAIL Indicates that the hydraulic ram air turbine (RAT) hydraulic pump is not
producing pressure (<1800 psi) when it should be 12
HYD SOV FAIL L (R)
Indicates that the left and/or right engine hydraulic fire wall shutoff valve (SOV)
did not go to its commanded position (open or closed) when the pilot has
manually armed or disarmed the left and/or right engine fire extinguishing
system
12
IAC 1 (2) (3) OVHT IAC has overheated, resulting in possible loss of function 7
ICE Cowl or wing icing detected with one of the three anti-ice systems off (L/R cowl
or wing) 3
ICE DETECTOR FAIL Loss of both ice detectors 3
INBD BRAKE FAIL L (R) Failure on affected inboard brake 14
INBD BRK LO PRESS Inboard brakes supply depleted (hydraulic system 3) 14
INT CABIN DOOR Internal door not open and latched for takeoff or landing
IRS 1 (2) (3) MSCMP IRS 1, 2 or 3 has miscompared with the other two IRSs 16
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
7-50 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
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庞巴迪挑战者手册5(73)
