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
ELECTRONIC DISPLAY SYSTEM
IRS 1 (2) (3) OVHT Annunciated when the IRS has overtemp condition (> about 70-73°C) 16
IRS 1 (2) (3) SET HDG IRS has defaulted to heading of 360° upon entering attitude mode 16
LARGE SERV DOORS One or more of AFT equipment bay, refuel/defuel, hydraulic access or belly
fairing stowage access doors/panels not closed 1
MACH TRIM FAIL
Displayed to alert the crew that due to loss of mach data acquisition, the mach
trim function has failed and will not compensate for pitching moments caused by
mach changes. Failure of pitch trim is covered by STAB TRIM message
10
MAIN GEAR DOOR L (R) Left and/or right main gear door not closed 14
MLG BAY OVHT FAIL Left and/or right main landing gear bay overheat detection element failure.
(Complete loss of overheat detection for main landing gear) 14
NOSE DOOR Nose gear door not closed 1
NOSE STEER FAIL Loss of nosewheel steering, nosewheel casters 14
OIL LO QTY L (R) Engine oil quantity is low 5
OUTBD BRAKE FAIL L (R) Failure on affected outboard brake 14
OUTBD BRK LO PRESS Outboard brakes supply depleted (hydraulic system 2) 14
OXYGEN LO QTY Either the oxygen quantity is low or one or more of the oxygen bottles are not
available 1
PACK AUTO FAIL L-R Left and right pack automatic control inoperative 13
PACK AUTO FAIL L (R) Pack control inoperative
PACK FAIL L (R) Left or right pack fail (overheat)
PACK FAIL L-R Left and right pack failed due to Ram air inlet duct rupture 13
PACK TEMP L (R) Manual temperature selection out of range 13
PARK/ EMER BRAKE ON Park brake is on with weight off wheels 7/14
PASSENGER DOOR Passenger door not closed 1
PITOT 1 (2) (3) HT FAIL Pitot 1-2-3 heat has failed 7
PLT BRAKE FAULT One or both pilot brake pedals not available 14
PRI FUEL PUMPS L (R) Left and/or right primary (AC) fuel pumps failure 11
RAT GEN FAIL A fault has been detected in the RAT generator system during power up BIT
check 6
REV LOCK FAIL L (R) Left and/or right thrust reverser locks (2 of 3) not locked with thrust lever in
forward thrust range. Thrust reverser will not deploy 17
REVERSER FAIL L (R) Left and/or right thrust reverser has failed and doors will stay in current position 17
ROLL SELECT Displayed to alert the crew that the pilot and copilot roll control are disconnected
and that no roll priority has been selected within 30 seconds from roll disconnect 10
ROLL SPOILERS FAIL Displayed if roll spoiler function is inoperative for at least 2 pairs of flight spoilers 10
CAUTION MESSAGES (AMBER)
CAS MESSAGE DESCRIPTION CH.
For Training Purposes Only
Sept 04
7-51
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
RUD AUTHORITY HIGH
Displayed to alert the crew that the rudder authority available is too high for the
indicated airspeed. This message will not be displayed if the rudder limiter
position or airspeed is indeterminate
10
RUD AUTHORITY LOW
Displayed in combination with “RUD LIMITER FAIL” to alert the crew that the
rudder limiting capability failed and that authority available is low (rudder limiting
failed in low authority position) for engine failure compensation or crosswind. Not
displayed if the system is not able to determine its authority status
10
RUD LIMITER FAIL
Displayed to alert the crew that rudder limiting capability is lost. If the system is
able to determine its rudder authority level versus the current A/C configuration,
one and only one of the following messages will be displayed also: “Rud
authority high” (system failed with too much authority available). “Rud authority
low” (system failed without enough authority available), “Rud authority safe”
(system failed with enough authority available and no risk of structure damage)
10
SG 1 (2) (3) FAIL Loss of communication with the SG, or the SG is indicating a power-up failure 7
SLAT FAIL Slat actuation system inop 10
SLAT FAULT Slats have been shut down 10
SLAT-FLAP FAIL Slat and/or flap actuation system inoperative, the slats and/or flaps can no
longer be selected 10
SLAT-FLAP FAULT
Slat and/or flap systems have shutdown and may be out of the selected position
due to jam, loss of power, overheat, etc. Once the condition clears, if the control
lever is selected to a new position, the system will again attempt to drive and the
message will disappear
10
SMALL SERV DOORS One or more of the small/access service doors not closed 1
SMOKE AFT (FWD) LAV
FAIL Smoke detector installed in the aft lavatory has failed 9
SMOKE AV BAY FAIL Smoke detector installed in the avionics bay has failed 9
SMOKE AV RACK FAIL Smoke detector in avionics rack has failed (Global 5000 only) 9
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
庞巴迪挑战者手册5(74)