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50 Cards in this Set

  • Front
  • Back
L OIL PRESS
R OIL PRESS
Oil pressure switch senses pressure less than 15 PSI
L ENG HT
R ENG HT
Engine cooling air temperature above 860 F
GND SPOILER
Failure of Ground Spoiler component or deployed Ground Spoiler panel in-flight
REV UNLOCK
Thrust Reverser overcenter links have moved overcenter toward the deploy position
L FUEL PRESS
R FUEL PRESS
Fuel pressure at the inlet to the HP fuel pump is less than 15 PSI due to boost pump system failure, crossflow/boost pump mis-management, or a fuel leak
L PYLON HT
R PYLON HT
Pylon temperature is above 325 F
AFT EQUIP HT
Aft equipment area temperature is above 200 F. Possibility exists that high pressure duct has blown or that fire is in progress.
BATT ON BUS
Aircraft batteries are supplying power to the Essential DC Bus
CABIN DOORS
Main or Baggage door not locked
CAB PRESS LO
Cabin altitude has exceeded 10,000 feet
CAB PRESS MAN
Cabin pressurization controller switched to its manual mode
L FUEL FILT
R FUEL FILT
Fuel filter clogged
L BLEED HT
R BLEED HT
Bleed air temperature is above 550 F
BATT SW OFF
Battery No. 1 and/or No. 2 switch is off
CAB OXY ON
Passenger masks have deployed
BLEED PRESS
Bleed air pressure has exceeded 90 PSI, probably through failure of one of the regulator valves
FUEL LOW LEVEL
Fuel level in hopper is below approximately 700 pounds
L CONV HT
R CONV HT
Coverter temperature is above 220 F
AV INV 1 FAIL
No. 1 avionics inverter has failed, or power has been lost to the DC Essential Bus. Verify lost source on EPMP.
AV INV 2 FAIL
No. 2 avionics inverter has failed, or power has been lost to the Right Main DC Bus. Verify lost source on EPMP.
L DC PWR
R DC PWR
DC Output from converter has dropped off line
L ALTNTR HT
R ALTNTR HT
Alternator temperature is above 250 F
L PITOT HT
R PITOT HT
Pitot tube heater elements not energized
L AC PWR
R AC PWR
AC output from converter has dropped off line
T/R HT
Transformer Rectifier temperature above 374 F
APU ALTNTR HT
APU alternator temperature is above 300 F
TONE GEN
Aural warning tone generator has failed
TRANS/RECT
Transformer Rectifier has been selected ON (manually or automatically) and there is no TRU output
AUX AC PWR
The output power from the APU has dropped off line
COMB HYD HT
Combined hydraulic system fluid temperature above 220 F
FLT HYD HT
Flight hydraulic system fluid temperature is above 220 F
AUX MASTER WARN CB
Loss of power (CB open) to one or more of the 16 AUX MAST WARN circuit breakers or either MASTER WARNING NO. 1 or NO. 2 power circuit breakers
EPMP PS
Either one or all sources power supply (4) to the EPMP has failed.
The sources are:
(1) DC Essential Bus (2 CB)
(2) BATT No. 1
(3) BATT No. 2
COMB HYD
Failure of combined hydraulic system pressure
FLT HYD
Failure of flight hydraulic system pressure
AUX HYD HT
Auxiliary hydraulic pump case temperature is above 300 F
RADIO RACK HT
Temperature of 200 F in the radio rack area
STAB FLAP
Flaps are up and stabilizer is not up
TRIM OFF
Electric trim inoperative
ANTI-SKID
Failure in anti-skid system
UTIL HYD OFF
Utility hydraulic pump switch is in the off position
L WING HT
R WING HT
Wing anti-ice exhaust duct temperature is above 180 F
STALL BARR VALVE NO 1
STALL BARR VALVE NO 2
Indicates that the respective stall barrier system is giving a stall angle indication
L MAIN FUEL
R MAIN FUEL
Main boost pump has failed
COOL TURB HT
Cooling turbine discharge air above 400 F
SERVICE DOOR
Fuel, water, LAV, or aft equipment door not locked
L ALT FUEL
R ALT FUEL
Alternate boost pump has failed
L CONV FAILED FAN
R CONV FAILED FAN
A converter cooling fan has failed.
Note: If the light extinguishes after illumination...this indicates another fan has failed
ICE DET
Inoperative
FLT RECORD
Flight recorder inoperative