Airbus Lights And Switches Flashcards

1
Q
Flight control panel
ELAC
-dark
- fault (amber)
- off (white)
A

Elevator Aileron Computer-

Black is normal

Amber fault is either a self test during power up or fault

White off is computer is off

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2
Q

SEC flight control panel

Dark
Amber fault
White OFF

A

Spoiler Elevator Computer

Dark is normal
Amber is fault
White is computer is off

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3
Q

FAC flight control panel buttons

A

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

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4
Q

What is the EVAC panel?

A

EVAC = Evacuate Panel

Has buttons related to the evacuate options. Alerts FAs and plays automatic briefing over PA

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5
Q

GPWS FAULT

TERR
SYS

A

TERR: Predictive EGPWS FAILED. No database to predict when you’ll hit a mountain…

SYS: MODES 1-5 Failed

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6
Q

CABIN PRESS Pushbuttons

MODE SEL

DITCHING

A

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)
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7
Q

Wing and Engine Anti-Ice

FAULT
WING/ ENG

A

Wing: Low Pressure or Valve Disagreement (Transit)

ENG: Valve Disagreement (Transit)

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8
Q

AIR COND PANEL:

Pack FAULT
ENG BLEED FAULT

A

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

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9
Q

AIR CONDITIONING PANEL:

APU BLEED FAULT

HOT AIR FAULT

A

APU: Leak

Hot Air:
Overheat detected!
Automatically…….Hot air valve and Trim Air valves close.

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10
Q

Electrical Panel

BATT 1/2:

OFF and FAULT

A

OFF: Battery Line contactor open, no charging

FAULT: Battery charging is outside limits. Not charging

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11
Q

ELECTRICAL

AC ESS FEED PB:

ALTN AND FAULT

A

ALTN: switches AC ESS BUS to be powered by AC BUS 2

FAULT: AC ESS BUS is not powered

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12
Q

ELECTRICAL FAULTS:
IDG FAULT
ENG GEN FAULT
APU GEN FAULT

A

IDG: HI OIL TEMP AND LOW OIL PX.

ENG: GCU TRIP OR LINE CONTACTOR OPEN

APU: GCU TRIP OR LINE CONTACTOR OPEN

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13
Q

Electrical GALLEY PB FAULT

A

Any Generator load > 100%

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14
Q

FUEL PUMPS FAULT

ALL

A

LOW PUMP PRESSURE

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15
Q

FUEL. CNTR TANK MODE SELECTOR PUSH BUTTON

A

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
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16
Q

ENGINE CONTROL PANEL UNDER THRUST LEVERS:

Engine Start

FAULT LIGHT

A

HP Fuel Valve Disagreement

Automatic start abort

17
Q

HYD PANEL Fault Lights

ENG 1(2) Pump

ELECTRIC PUMPS

PTU

A

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
18
Q

PTU run when in Auto?

A

Greater than 500 PSI difference between yellow and green Hydraulic Systems

19
Q

GEN 1 LINE Pushbutton:

Smoke (Amber)

OFF

A

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…

20
Q

Oxygen Panel

Passenger
SYS ON

A

A signal has been sent to deploy the masks. Doesn’t necessarily mean they deployed.

21
Q

EMER ELEC PWR

RAT and EMER GEN
RED FAULT

A

RAT IS DEPLOYED AND NOT SUPPLYING POWER

22
Q

IRU

Align Flashing and Steady Light

A

FLASHING—

23
Q

IRU

FAULT Flashing and Steady

A

Steady = IRU is lost

Flashing = Attitude and Heading May be recovered in ATT

24
Q

EVAC PANEL

EVAC

A

EVAC = Light flashes when button pushed

ON = Tone in Cabin and flashing lights at FA stations