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49 Cards in this Set
- Front
- Back
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ELECTRICAL POWER
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ALTERNATING CURRENT
DIRECT CURRENT STANDBY AC AND DC POWER |
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THE MAIN BATTERY
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ENERGIZES THE HOT BATTERY AND SWITCHED HOT BATTERY BUSSES WHEN AC POWER IS NOT AVAILABLE
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THE MAIN BATTERY
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EMERGENCY POWER FOR:
BATTERY BUS AC AND DC STANDBY BUS |
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CABIN UTILITY SWITCH
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RECIRCULATION FANS
LOGO LIGHTS |
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IFE/PASS SEAT SWITCH
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FLIGHT DECK AUXILIARY POWER OUTLET
FLIGHT DECK DOOR SURVALIANCE SYSTEM |
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STANDBY POWER
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AC STANDBY BUS IS POWERED BY AC TRANS 1
DC STANDBY BUS TR1, TR2, TR3 |
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IN FLIGHT OR GROUND LOSS OF ALL AC POWER
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AC STANBY BUS BATTERY THROUGH STATIC INV
DC SANDBY BUS AND BATTERY BUS BATTERY |
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STANDBY POWER SWITCH OFF
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STANDBY POWER OFF LIGHT ILLUMINATES
AC STANDBY BUS, STATIC INVERTER AND DC STANDBY BUS ARE NOT POWERED |
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STANDBY POWER SWITCH BAT
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AC STANDBY THROUGH STATIC INV BATT
DC STANDBY BUS THROUGH BATT |
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IF ALL SOURCES OF AC POWER ARE REMOVED
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STANDBY POWER CONTROL UNIT AUTOMATICALLY CHANGES THE STANDBY SYSTEM TO BATTERY POWER
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BATTERY SWITCH OFF
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REMOVES POWER FROM BATTERY BUS AND SWITCHED HOT BATTERY BUS WHEN OPERATING WITH NORMAL POWER SOURCES AVAILABLE
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BATTERY SWITCH OFF
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REMOVES POWER FROM BATTERY BUS, SWITCHED HOT BATTERY BUS, DC STANDBY BUS, STATIC INVERTER AND AC STANDBY BUS WHEN BATTERY IS ONLY POWER SOURCE
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STANDBY POWER ONLY
AIR SYSTEMS |
AIR COND PACK VALVES
MAN PRESS ALT WARN HORN PACK TRIP OFF LIGHT BLEED TRIP OFF LIGHT |
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STANDBY POWER ONLY
COMMUNICATIONS |
FLIGHT INTERPHONE
PASSENGER ADDRESS VHF 1 AUDIO CONTROL PANEL SWITCHES FOR THIS |
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STANDBY POWER ONLY
EMERGENCY EQUIPMENT |
PASSENGER O2
FLIGHT CREW O2 |
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STANDBY POWER ONLY
ENGINES AND APU |
STARTER VALVES AND RIGHT IGNITERS
UPPER DISPL EXCEPT VIBRATION THRUST REVERSERS APU OPERATION ( NOTE BELOW 25000 REC ) |
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STANBY POWER ONLY
FIRE PROTECTION |
APU AND ENGINE FIRE DETECTION
APU AND ENGINE FIRE EXTINGUISHER CARGO FIRE EXTINGUISHER |
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STANDBY POWER ONLY
FLIGHT INSTRUMENTS |
CAPTAIN EFIS PANEL
CAPTAIN EFIS DISPLAY ON CAPT OUTBOARD ALL STANDBY INSTRUMENTS AND CLOCKS VHF NAV 1 AND MARKER BEACON REC LEFT ADIRU |
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STANDBY POWER ONLY
FUEL SYSTEM |
ENGINE AND SPAR FUEL SHUTOFF VALVES AND LIGHTS
CROSSFEED VALVE QUANTITY INDICATORS |
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STANDBY POWER ONLY
HYDRAULICS |
STANDBY RUDDER SHUTOFF VALVES
ENGINE HYDRAULIC SHUTOFF VALVES |
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STANDBY POWER ONLY
LANDING GEARS BRAKES |
ANTISKID SYSTEM INBOARD
ANTISKID INOP LIGHT AIR/GROUND SYSTEM PARKING BRAKE |
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STANBY POWER ONLY
WARNING SYSTEMS |
MASTER CAUTION RECALL
STALL WARNING AURIAL WARNING |
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STANDBY POWER ONLY
AURIAL WARNINGS |
TAKEOFF LANDING CONFIGURATION
MACH AIRSPEED LIMIT CABIN ALTITUDE AUTOPILOT DISCONNECT GROUND PROXIMITY CREW CALL CHIME |
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STANBY POWER ONLY
ELECTRICAL |
STANDBY POWER OFF LIGHT
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NORMAL DC INDICATION
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26 +_4
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NORMAL AC INDICATION
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115+_5
FREQUENCY 400+_10 |
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BATTERY DISCHARGE
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A BATTERY DISCHARGE EXCEEEDENCE OCCURS
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TR UNIT LIGHT
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ANY TR ON THE GROUND
TR1 OR TR2 AND TR3 IN FLIGHT |
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ELEC
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A STANDBY POWER OR DC SYSTEM FAULT ON THE GROUND ONLY
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DRIVE
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A GEN DRIVE MALFUNCTION
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TANSFER BUS OFF
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THE TRANSFER BUS IS NOT ENERGIZED
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SOURCE OFF
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THE TRANSFER BUS IS NOT POWERED BY THE LAST SELECTED SOURCE
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GEN OFF BUS
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THE TRANSFER BUS IS NOT SUPPLIED POWER BY IDG
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APU GEN OFF BUS
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APU GEN AVAILABLE BUT NOT CONNECTED
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GRD POWER AVAILABLE
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GROUND POWER OF GOOD QUALITY CONNECTED TO AIRPLANE
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AUTOMATIC GEN ONLINE
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ONLY IN FLIGHT
ONLY 1 TIME PER FLIGHT IDGs NOT CONNECTED TO BUSSES APU FAILS/SHUTDOWN AFTER T/0 |
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LOAD SHEDDING
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GALLEY BUSSES ARE DEENEGIZED FIRST
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T/R
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CHANGE 115 VOLT AC FROM TRANSFER BUSSES TO 28 VOLT DC FOR USE BY THE DC BUSSES
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TR3
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IS AN AUX SOURCE OF DC POWER IF TR1 OR TR2 FAILS ALSO THE NORMAL SOURCE OF POWER FOR THE BATTERY BUS
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CROSS BUS TIE RELAY OPENS
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GLIDESLOPE CAPTURE
BUS TRANSFER SWITCH OFF |
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THE HOT BATTERY BUS
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ALWAYS CONNECTED TO BATTERY POWER. ITS COMPONENTS OPERATE AS LONG AS BATTERY VOLTAGE IS ABOVE MIN VALUE
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POWER TO THE SWITCHED HOT BATTERY
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IS CONTROLLED BY THE BATTERY SWITCH
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THE STATIC INVERTER
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CHANGES 24 VOLT DC BATTERY POWER TO 115 VOLT AC POWER FOR THE AC STANDBY BUS
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AUTOMATIC BATTERY CHARGER
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RESTORES AND MAINTAINS FULL BATTERY VOLTAGE
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THE BATTERY CHARGER
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IS SUPPLIED POWER FROM AC GROUND SERVICE BUS 2 WHEN A SOURCE OF AC POWER AVAILABLE
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PED
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PERSONAL ELECTRONIC DEVICES
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IDG LOW OIL PRESSURE IS CAUSED BY
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IDG FAILURE
ENGINE SHUTDOWN IDG AUTO DISCON DUE TO HIGH OIL TEMP BY SWITCH |
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ANY TWO TRs
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CAPABLE OF SUPPLYING THE TOTAL CONNECTED LOAD
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BATTERY VOLTAGE RANGE
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22-30 VOLTS
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