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Frontier Study Guide > Lights And Switches > Flashcards

Lights And Switches Flashcards

1
Q

ON BATT LIGHT

A

-Self Test During full Alignment
-One or more IR are on BATT
-5 min to recover Power or two the Captain’s not using will drop off

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2
Q

IR 1/2/3 Fault Light/OFF

A

-Steady Fault Light: Fault in IR/IR Lost
-Flashing Fault Light: Attitude/Heading may be recovered

-OFF: Illuminates when inertial data output is disconnected

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3
Q

ADR 1/2/3 Fault Light/OFF

A

Fault:
-Fault in Air Data
-Pitot Static system on that side has been lost

OFF:
-Associated ADR is off

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4
Q

ELAC 1 (Elevator Aileron Computer)

A

ELAC: Normal Pitch/Roll, Alternate Pitch/LAF (if installed), Direct Pitch/Roll, Abnormal Attitude, Aileron Droop, Acquisition of Autopilot orders.
-ELAC Fault: Fault is detected/only 8 seconds during power up if it’s a good test.

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5
Q

SEC 1/ 2/ 3 (Spoiler Elevator Computer)

A

SEC: Normal Roll, Speed-brakes/GND Spoilers, Alternate/Direct Pitch (SEC 1/2 only), Direct Roll, Alternate LAF (if Installed), Abnormal Attitude.
-SEC Fault Light: Fault in the system

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6
Q

FAC 1/2 (Flight Augmentation Computer)

A

-FAC: Gives us Speed tape symbology; F, S, Green Dot, Low Energy Warning, Wind Shear Protection
Flying the Tail: Turn Coordination, Yaw Damping, Rudder Trim, Rudder Travel Limits.
-FAC Fault Light: Fault in the system

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7
Q

GEN 1 Line PB

A

-Smoke Light, Smoke detected in Avionics Compartment
-Blower/Extract Fans PB will also show Fault
-PB, Isolates GEN for the #1 fuel pumps in the left/right wing tanks

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8
Q

RAT & EMER GEN (Fault Light)

A

-EMER GEN is not supplying PWR but it should be, AC Bus 1/2 not PWRD
-Lift guard and push the button for electrical power only

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9
Q

TERN GPWS/SYS PB (Fault Lights)

A

-TERR PB Fault light; Terrain Data base is lost, You will still have basics modes of the GPWS system (To Low Flaps, To Low Gear, and Terrain Recognition).

  • SYS Fault; Lost all modes including GPWS
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10
Q

G/S MODE & FLAP MODE

A

-Used for Abnormal conditions to shut down the selected mode

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11
Q

LDG Flaps 3

A

-Turn on when performing a FLAP 3 Landing
-Landing memo displays Flaps 3

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12
Q

CVR
GND CTL PB

A

-Powered for 5 min on external power, Captain must turn on CVR on the ground to capture briefings/checklist test. If the CVR doesn’t test, the parking brake is off
- Comes on automatically after engine start.
-In flight

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13
Q

Oxygen

A

-Passenger PB; SYSTEM ON signal sent to the back to drop masks (Automatically at 14,000’ Cabin ALT) or Press MASK MAN ON guarded switch for manual deployment
-Crew Supply; Allows O2 bottle to connect to manifold for Cockpit Masks

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14
Q

CALLS

A

-Contact Mech, FWD/AFT FA stations (Single Chime)
-EMER; Lift Guard Pressed (Triple High/Low Chime)

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15
Q

Wipers

A

230KTS Limit

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16
Q

APU Master SW; ON/FAULT

A

-ON; ECB (Electronic Control Box) PWR-up TEST is initiated, APU Air Inlet Opens, Pressurizing Fuel pump, Fuel Isolation Valve Opens, If External PWR or Main GEN is on; APU SYS Page is displayed.
-OFF; Light extinguishes and shuts down after 2 min cooldown.
-Fault Light; Fire (on the ground only) or Shutdown was Abnormal:
- DC PWR lost, BATTs PB off on BATT PWR only
- Air inlet flap closed
- Inlet overheat
- No Acceleration
- No Speed
- Under-speed
- Slow Start
- Overspeed
- Loss of Overspeed protection
- Overcurrent
- No Flame
- Reverse flow
- Low oil Pressure
- High Oil Temperature
- Clogged oil Filter
- EGT Over-temp
- Sensor failure
- IGV failure
- ECB failure
- Loss of EGT thermocouples

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17
Q

ANTI ICE

A

-WING; Outboard 3 slats are heated; Default to closed when PWR is lost,
Fault light: Low Air Pressure/Valve Switch Disagreement/Valve intransit

-ENG; Nacelle Lip only, Defaulted to open when PWR is lost
Fault Light: Valve Switch Disagreement/Valve intransit

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18
Q

Probe/Window Heat

A

-Aircraft has PWR, Drain Mast are heated
-PB ON, All Probes/Windows heated except TAT
-PB AUTO, Probes/Windows are heated at ENG Start
-TAT, PWRD when airborne only

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19
Q

Cabin Pressurization/ MODE SEL Fault Light

A

-Switches after each landing, System failure, lost both Auto Controllers
-Selecting MAN for 10 sec, then return to AUTO will select other system

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20
Q

LDG ELEV AUTO Rotary Switch

A

-Gets Landing Elevation from FMGC
-Must take it out of Auto if Destination in not in Data Base/Data Base in incorrect or ECAM or Abnormal procedure tells you to do so
-Still get auto pressurization regardless of position, Only changes the schedule to when the Outflow valve opens

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21
Q

Guarded “DITCHING” Switch

A
  • SYS in Auto will close Outflow valve, Emergency Ram air inlet, Avionics Inlet/Extract valves, Pack-flow CNTRL valves.
  • MODE SEL must go to Manual CNTRL, Outflow Valve now CNTRL by “MAN V/S CTL switch (Up to open, Down to Close).
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22
Q

ENG Fire PB 1/2

A
  • Silence CRC/Arms Squibs
  • Deactivates IDG
  • Closes LP Fuel valve/De-energizes FADEC
  • Closes Hydraulic Shutoff Valve
  • Closes Bleed/Pack Flow Control Valves
23
Q

APU Fire PB

A
  • Silences CRC/Arms Squib
  • APU Shuts Down
  • Closes Low Pressure Fuel Valve/Shuts Down APU Fuel Pump
  • Closes APU Bleed/Cross Bleed Valves
  • Deactivates APU Generator
    -APU Fire Light illuminates when warning is activated regardless of pushbutton position
24
Q

ENG Test PB

A

Looking for:

CRC/MASTER WARN Light
ECAM
Squib Light
DISCHARGE Light
Fire Light on ENG panel

25
Q

APU Test PB

A

Looking for:

CRC/Master Warning Light
ECAM
* APU Fire PB Light
* SQUIB Light
* DISCHARGE Light

(* If DC power only)

26
Q

Hydraulic; ENG PB 1/2 Fault light

A

Reservoir Problem:
Low Level
Fluid Over Heat
Low Air Pressure

Pump Problem:
Low Pressure

27
Q

Hydraulic; Blue/Yellow ELEC Pump PB (Fault Light)

A

Reservoir Problem:
Low Level
Fluid Overheat
Low Air Pressure

Pump Problem:
Low Pump Pressure
Over Heat

28
Q

Hydraulic; PTU PB (Fault Light)

A

Reservoir Problem:
Low Level
Fluid Overheat
Low Airpressure

29
Q

Fuel; LTK, RTK, CTK Pumps 1/2 (Fault Light)

A

Low Output Pressure

30
Q

Fuel; MODE SEL (Fault Light)

A

CTK > 550LBS

LTK/RTK < 11000LBS

31
Q

Electrical; Galley PB (Fault Light)

A

Any Generator Load > 100%

32
Q

BAT 1/2 PB (Fault Light)

A

Battery Charger Current is out of limits

33
Q

IDG 1/2 PB (Fault Light)

A

High Oil Temperature
Low Oil Pressure

34
Q

GEN 1/2 PB (Fault Light)

A

GCU Trip
Line Contactor open

35
Q

APU GEN PB (Fault Light)

A

GCU Trip
Line Contactor open
Inhibited at low speed

36
Q

AC ESS FEED (Fault Light)

A

AC ESS BUS not powered

37
Q

PAC 1/2 PB (Fault Light)

A

Compressor or PACK overheated
Valve disagreement

38
Q

ENG Bleed PB (Fault Light)

A

-Leak
-Overheat
-Over Pressure down Stream
-Start in process & Valve opened
-APU Bleed on & Valve opened
-HP Valve failed to open on ground
-Single BTS Fail or -Disagree on the ground
-Dual BTS Fail inflight or on ground
-Fan Duct Burst detected (LEAP 1-A only)

39
Q

APU Bleed PB (Fault Light)

A

Leak Detected

40
Q

Hot Air PB (Fault Light)

A

Over Heat Detected, Closes:
Hot air valve
Trim Air Valve

41
Q

Wing Anti-Ice PB (Fault Light)

A

Low Pressure
Valve Disagreement
Valve in Transit

42
Q

ENG Anti-Ice PB (Fault Light)

A

Valve disagreement
Valve in transit

43
Q

APU Master Switch PB (Fault Light)

A

Fire (on ground only),
Abnormal Shutdown

44
Q

EMER EXIT Off Light

A

EMER Exit Light Selected Off

45
Q

CARGO SMOKE FWD/AFT (DISCHARGE Light)

A

Bottle fully discharged

46
Q

VENTILATION BLOWER PB (Fault Light)

A

Smoke
Overheat
Air Pressure Low*
Computer Power Supply Failure
*Horn sounds if on the ground
+no engines running

47
Q

VENTILATION EXTRACT PB (Fault Light)

A

Smoke
Pressure is low*
Computer Power Supply Failure
*Horn sounds on the ground
+no engines running

48
Q

Cockpit Door (Fault Light)

A

System Failure (Latch, Control Unit, Pressure Sensor)

49
Q

ENG Control 1/2 (Fault Light)

A

Automatic Start Abort
HP Valve disagreement

50
Q

EFIS Controls, GPWS (Fault Light)

A

RED Fault Light: GPWS 1-4 alert/EGPWS Alert

Amber Fault Light: GPWS 5 Alert, too far below glide slope

51
Q

Minimum Battery Voltage

A

25.5 Volts

52
Q

Batteries in Auto

A

Will connect Sole source of electrics, need to charge (Below 26.5V), or starting the APU

53
Q

AC Bus 1/2 Lost in flight >100KTS

A

RAT will deploy automatically, Batteries only for 8 sec

54
Q

EVAC (Guarded Switch)

A

ON: Activates EVAC tone/Flashes EVAC lights at FA panels
OFF: Lights out

Frontier Study Guide (7 decks)

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