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PROBE MON FAIL L (R) Monitoring LRU has failed. Heater status on probes and associated systems is
not verified 7
R/D VALVE OPEN L (R) Left and/or right defuel valve failed open 11
RAM AIR FAIL Ram air failure 13
RAT GEN ON The RAT is deployed and the RAT LC is on 6
RECIRC FAN FAIL Both recirculation fans failed 6
REV LOCK FAULT L (R) One of two primary stow switches on corresponding thrust reverser indicating
unstowed with thrust lever in forward thrust range 17
REVERSER FAULT L (R) Minor fault in the thrust reverser system. Thrust reverser operation should be
normal 17
REVRSION CTLR FAIL Loss of rev control functions due to improper connection 16
RUD AUTHORITY SAFE
Displayed in combination with “RUD LIMITER FAIL” to alert the crew that the
rudder limiting capability failed and that authority available is safe in current
configuration and speed. Not displayed if the system is not able to determine its
authority status
10
RUD LIMITER FAULT Displayed to alert the crew that one and only one channel is failed 7
SAFETY VALVE OPEN Safety valve 1 or safety valve 2 not fully closed 13
SELCAL HF1 (2) Annunciated when the HF1-2 indicates an incoming message. Voice: “SELCALL”
twice. Reset with Push-To-Talk (PTT) 5
SELCAL VHF1 (2) (3) Annunciated when the VHF1-2-3 indicates an incoming message. Voice: “SELCALL”
twice. Reset with Push-To-Talk (PTT) 5
SET LDG ELEV No landing information is received by CPC from FMS or LDG ELEV is selected
MAN and no value was selected on the CPCS control panel 16
SHAKER 1 (2) FAIL
1. Pilot’s shaker has failed (the actual motor) or the commanding SPC channel
has failed
2. Copilot’s shaker has failed (the actual motor) or the commanding SPC
channel has failed
10
SLAT DRIVE OVHT
System shutdown due to overheat on at least one channel. Message self-clears
once the channel has cooled down. Always displayed in conjunction with “SLAT
FAULT”
10
SLAT FAULT Slats inoperative 10
ADVISORY MESSAGES (CYAN)
CAS MESSAGE DESCRIPTION CH.
7-58 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
SLAT HALFSPD System operating at half speed 10
SLAT-FLAP HALFSPD Slat actuation system (and/or flap actuation system) operating at half speed,
due to a fail or fault condition in one channel only of the slats and/or flaps 10
SLAT/FLAP BIT Posts on the ground only when maintenance action is required on the slat/flap
system prior to the 500 hour scheduled interval 10
SLAT-FLAP FAULT Slat and flap inoperative 10
SPLRS/STAB BIT Posts on ground only when maintenance required 10
SPLRS/STAB IN TEST
Displayed when the spoilers and stab trim systems perform their on-ground selftest,
once all hydraulics are ON, since spoilers and stab trim are inoperative
during the test (approximately 20 sec.)
10
STAB CH 1 (2) FAIL Displayed only when Stab Trim Channel 1 (or 2 but not both) is failed or inhibited
by abnormal master switch operation 10
STALL WARN ADVANCE Stall reversion mode has been activated - can be done automatically based on
a/c condition or manually 10
STALL WARN BASIC 1. Stall erroneously set in basic mode, or
2. Split between L and R AOR vanes 10
TAT 1 (2) (3) FAIL TAT probe 1, 2 and/or 3 failed 7
TAT HT 1 (2) (3) FAIL
1: Left engine TAT heater failed, or
2: Right engine TAT heater failed, or
3: Fuselage TAT heater failed
7
TERR FAIL
TERRAIN AWARENESS INOP and NOT SUPPRESSED when EGPWS
SYSTEMS FAIL message is displayed (i.e. COMPUTER FAIL or EGPWS not
communicating)
16
TRIM AIR FAULT Trim air fault 13
TRU 1 (2) FAIL TRU 1/2 has failed 6
WINDMILL ENVELOPE FADEC has determined that the aircraft is within the windmill start envelope 17
WINDSHEAR FAIL
(WINDSHEAR INOP) and NOT [(COMPUTER FAIL) or (EGPWS not
communicating)] SUPPRESSED when EGPWS SYSTEMS FAIL message is
displayed
16
WING A/ICE FAULT Loss of redundancy on wing a/ice system (CBW failed, one temperature sensor
fail, opening of CBW and closing of one WAIV) 3
WING A/ICE SENSOR Failure of both outboard wing a/ice temperature sensors 3
WOW FAULT Loss of redundancy on WOW 14
XFEED VALVE FAIL Crossfeed valve failure 11
YD HEAT 1 (2) FAIL Yaw damper actuator 1-2 heater failed. System is heating unused YD 10
YD NOT CENTERED YD linear actuator not centered while on ground 10
ADVISORY MESSAGES (CYAN)
CAS MESSAGE DESCRIPTION CH.
For Training Purposes Only
Sept 04
7-59
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
STATUS MESSAGES (WHITE)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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