Airbus Lights And Switches Flashcards
Flight control panel ELAC -dark - fault (amber) - off (white)
Elevator Aileron Computer-
Black is normal
Amber fault is either a self test during power up or fault
White off is computer is off
SEC flight control panel
Dark
Amber fault
White OFF
Spoiler Elevator Computer
Dark is normal
Amber is fault
White is computer is off
FAC flight control panel buttons
Flight Augmentation Computer
Dark is normal flight protections are on
Fault Amber means there’s a computer fault
White off means the computer is off
What is the EVAC panel?
EVAC = Evacuate Panel
Has buttons related to the evacuate options. Alerts FAs and plays automatic briefing over PA
GPWS FAULT
TERR
SYS
TERR: Predictive EGPWS FAILED. No database to predict when you’ll hit a mountain…
SYS: MODES 1-5 Failed
CABIN PRESS Pushbuttons
MODE SEL
DITCHING
MODE SEL:
Both Auto systems failed
DITCHING:
Closes: Everything below water line…….
-Avionics Ventilation inlet valve
- Avionics Ventilation extract valve
- Both Pack flow control valves
- Ram Air Inlet valve
-Outflow valve (Auto control)
Wing and Engine Anti-Ice
FAULT
WING/ ENG
Wing: Low Pressure or Valve Disagreement (Transit)
ENG: Valve Disagreement (Transit)
AIR COND PANEL:
Pack FAULT
ENG BLEED FAULT
PACK FAULT:
Overheat (compressor or pack outlet) OR Valve Position Disagreement
ENG BLEED:
Leak
Overheat
Overpressure downstream
Start in process with Bleed valve not clsd
APU Bleed On with Bleed valve not closed
AIR CONDITIONING PANEL:
APU BLEED FAULT
HOT AIR FAULT
APU: Leak
Hot Air:
Overheat detected!
Automatically…….Hot air valve and Trim Air valves close.
Electrical Panel
BATT 1/2:
OFF and FAULT
OFF: Battery Line contactor open, no charging
FAULT: Battery charging is outside limits. Not charging
ELECTRICAL
AC ESS FEED PB:
ALTN AND FAULT
ALTN: switches AC ESS BUS to be powered by AC BUS 2
FAULT: AC ESS BUS is not powered
ELECTRICAL FAULTS:
IDG FAULT
ENG GEN FAULT
APU GEN FAULT
IDG: HI OIL TEMP AND LOW OIL PX.
ENG: GCU TRIP OR LINE CONTACTOR OPEN
APU: GCU TRIP OR LINE CONTACTOR OPEN
Electrical GALLEY PB FAULT
Any Generator load > 100%
FUEL PUMPS FAULT
ALL
LOW PUMP PRESSURE
FUEL. CNTR TANK MODE SELECTOR PUSH BUTTON
FAULT = 550lbs center tank with less than 11,000lbs in an outboard tank. (Bottom)
- PUMPS RUN AFTER ENG START 2 MINUTES
- IF SLATS ARE RETRACTED
- 550 lbs then + 5 Mintuesh
ENGINE CONTROL PANEL UNDER THRUST LEVERS:
Engine Start
FAULT LIGHT
HP Fuel Valve Disagreement
Automatic start abort
HYD PANEL Fault Lights
ENG 1(2) Pump
ELECTRIC PUMPS
PTU
ENG 1(2): (GREEN AND YELLOW)
- Reservoir Low level
-Reservoir Fluid Overheat - Reservoir Low Air Pressure
-Low pump pressure
ELECTRIC PUMPS (BLUE AND YELLOW)
- Reservoir Low level
-Reservoir Fluid Overheat - Reservoir Low Air Pressure
-Low pump pressure - Pump Over Heat
PTU (GREEN OR YELLOW…)
- Reservoir Low level
-Reservoir Fluid Overheat - Reservoir Low Air Pressure
PTU run when in Auto?
Greater than 500 PSI difference between yellow and green Hydraulic Systems
GEN 1 LINE Pushbutton:
Smoke (Amber)
OFF
SMOKE: smoke detected in avionics bay
OFF: Disconnects Generator 1 from AC BUS 1. A fuel pump in each wing Tank is powered by Generator one. AC BUS 1 powered by Gen 2…
Oxygen Panel
Passenger
SYS ON
A signal has been sent to deploy the masks. Doesn’t necessarily mean they deployed.
EMER ELEC PWR
RAT and EMER GEN
RED FAULT
RAT IS DEPLOYED AND NOT SUPPLYING POWER
IRU
Align Flashing and Steady Light
FLASHING—
IRU
FAULT Flashing and Steady
Steady = IRU is lost
Flashing = Attitude and Heading May be recovered in ATT
EVAC PANEL
EVAC
—
EVAC = Light flashes when button pushed
ON = Tone in Cabin and flashing lights at FA stations
