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Lights And switches Flashcards

1
Q

ADIRS Control Panel

                       IR 1/2/3 Fault Light
A

Steady (amber) - Fault in IR

Flashing (amber) - Attitude and Heading may be recovered using ATT mode

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2
Q

ADIRS Control Panel

                    IR 1/2/3 Align Light
A

Steady (white) Normal during alignment (approx 10 minutes)

Flashing (white) -

  • no position entered within 10 minutes
  • bad position (1º difference between shutdown and entered)
  • Fault
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3
Q

ADIRS Control Panel

                        ON BAT Light (amber)
A
  • Self test during full alignment

- one or more IR are on BAT (external horn also sounds)

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4
Q

ADIRS Control Panel

IR 1/2/3 Rotary Selector OFF

A
  • ADIRU unpowered
  • Wait 5 minutes after gate arrival
  • Wait 10 seconds after switching OFF to unpower aircraft electrical system
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5
Q

ADIRS Control Panel

IR 1/2/3 Rotary Selector NAV

A

Normal mode supplying full inertial data

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6
Q

ADIRS Control Panel

IR 1/2/3 Rotary Selector ATT

A

ATT Attitude and Heading only supplied
-enter magnetic heading using keyboard (i.e. “H9990”)
-fourth digit is tenths
-heading entered will be converted to true
heading
-should be entered every 10 minutes

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7
Q

ADIRS Control Panel

ADR 1/2/3 Fault Light (amber)

A

Fault in Air Data

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8
Q

FLT CTL Panel

ELAC 1/2 Fault light (amber)

A
  • Self test during power-up

- Fault

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9
Q

FLT CTL

SEC 1/2/3 Fault light (amber)

A

Fault

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10
Q

FLT CTL

FAC 1/2 Fault light (amber)

A

Fault

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11
Q

EVAC

COMMAND - EVAC light (red)
- ON light (white)

A

EVAC light (red) - flashes when pb pushed.

ON light (white) - 
Cockpit: 
     -EVAC Light flashes red 
     -Horn 
Cabin: 
     -EVAC Lights flash at FWD and AFT FAPs 
    -Evacuation tone sounds
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12
Q

GPWS

TERR pb Fault Light (amber)

A

EGPWS Failed

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13
Q

GPWS

SYS pb Fault light (amber)

A

Modes 1-5 failed

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14
Q

GPWS

LDG FLAP 3 pb - ON light (white)

A

LDG memo changed to display FLAPS 3

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15
Q

RCDR

GND CTL AUTO pb - pushed

A

Voice and Data recorders operate:

  • 5 minutes after initial power up
  • On the ground from 1st engine start to 5 minutes after 2nd engine shutdown
  • Inflight
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16
Q

RCDR Panel

RCDR CVR TEST pb - pushed

A

Activates test when:

  • CVR is powered
  • Parking brake is ON
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17
Q

OXYGEN Panel

MASK MAN ON pb- Pushed

A
  • Mask doors open

- Prerecorded instructions broadcast

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18
Q

OXYGEN Panel

MASK MAN ON pb- AUTO

A
  • Mask doors open when cabin altitude exceeds 14,000 ft.

- Prerecorded instructions broadcast

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19
Q

OXYGEN Panel

PASSENGER - SYS ON light (white)

A
  • Signal to open mask doors has been activated

- Remains on until TMR RESET pb pushed on MX Panel

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20
Q

OXYGEN Panel

CREW SUPPLY- OFF light (white)

A

Closes valve

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21
Q

CALLS Panel

MECH pb - pushed

A
  • Illuminates blue COCKPIT CALL light in nose gear well

- External horns sounds in nose gear well (while holding button)

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22
Q

CALLS Panel

EMER pb - pushed

A
  • Illuminates EMERGENCY CALL light on all F/A panels
  • 3 high/low chimes
  • Pink light at all F/A call panels flashes
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23
Q

CALLS Panel

EMER pb - CALL light (flashing amber)

A
  • Emergency call from cockpit to cabin or vice versa
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24
Q

CALLS Panel

EMER pb - ON light (flashing white)

A
  • Emergency call from cockpit to cabin or vice versa
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25
CALLS Panel EMER CALL @ FAP (call from cabin to cockpit) - pushed
- ATT light flash on ACP - EMER CALL and EMER ON pb lights flash - Buzzer sounds 3 times - Buzzer Inhibited during takeoff until 1500 feet and during landing starting at 800 feet
26
EXT LT STROBE - AUTO
- On when main gear strut not compressed
27
SIGNS Panel EMER EXIT LT - armed
- Loss of AC1 bus illuminates only: - Overhead lights - Loss of DC ESS SHED bus illuminates: - Overhead lights - Exit signs - Path lighting
28
Signs Panel NO SMOKING - AUTO
Low tone chime sounds when: - On when Gear extended - Off when Gear retracted
29
APU Panel MASTER SW pb FAULT Light (amber)
- Auto shutdown for many reasons | - Fire will only cause auto shutdown on the ground
30
APU Panel MASTER SW pb - ON light (blue)
- ECB self-test - Flap opens - Fuel isolation valve opens - Fuel pump on if main fuel pump not on - ECAM page appears
31
APU Panel MASTER SW - OFF
- MASTER SW on Light and START AVAIL Light extinguish - Shutdown delay 60-120 seconds if APU bleed used - Flap closes at 7% N (wait 2 minutes after the AVAIL light extinguishes, before turning off electrical power to ensure the flap closes.
32
APU Panel START pb AVAIL Light (green)
N > 99.5% | N > 95 % for 2 seconds
33
APU Panel START pb ON Light (blue)
APU Starts
34
AIR COND Panel PACK FLOW Selector - LO, NORM, HI
- LO 80% - Select if less than 115 passengers - NORM 100% - Select if 115 or more - HI 120% - Select if abnormally hot and/or humid
35
AIR COND Panel PACK 1 2 pb - Pushed
Opens pack valve unless: - Fire pb released - Start in process - Ditching switch selected - Overheat in compressor outlet - Air pressure low
36
AIR COND Panel PACK 1 2 pb - FAULT light (amber)
- compressor outlet overheat - pack outlet overheat - valve disagreement
37
AIR COND Panel ENG 1 2 BLEED pb - Pushed
Opens bleed valve unless: - Leak - Overheat - Overpressure - Start valve open - APU Bleed valve open (or pb On) - Fire pb released - Air 8 psi or less
38
AIR COND Panel ENG 1 2 BLEED pb - FAULT light (amber)
``` Leak Overheat Overpressure downstream Start in process and valve not closed APU Bleed On and valve not closed ```
39
AIR COND Panel ENG 1 2 BLEED pb - OFF light (white)
- Bleed valve closed | - HP valve closed
40
AIR COND Panel RAM AIR pb ON Light (white)
If Ditching switch is NOT selected: - RAM AIR Inlet opens (check valve located downstream will not open if diff. psi is greater than 1 psi). - Outflow Valve Opens 50% if: - Differential psi < 1, and - not being controlled manually
41
AIR COND Panel APU BLEED pb FAULT Light (amber)
Leak
42
AIR COND Panel APU BLEED pb - ON Light (white)
Opens valve when pushed and: - N > 95% - No Leak
43
AIR COND Panel X BLEED selector - AUTO
``` Opens if: - APU Bleed valve is open Closed if: -APU Bleed valve is closed -Wing, Pylon or APU Leak (except during start) ```
44
AIR COND Panel HOT AIR pb FAULT Light (amber)
Overheat detected, and closes: - Hot air valve - Trim Air valve
45
AIR COND Panel HOT AIR pb OFF Light (white)
Closes: - Hot air valve - Trim air valve
46
ELEC Panel COMM pb ON Powers:
- Cabin and cargo Lights - Water system and Toilets - Drain mast ice protection - Galleys - In Flight Entertainment- IFE (if installed)
47
ELEC Panel GALLEY and CAB pb AUTO Powers:
- Main Galley* - Secondary Galley - In Flight Entertainment (IFE)* *Main Galley and IFE are shed when only one generator is operating (Except only IFE is shed if on the ground with APU Gen or EXT PWR)
48
ELEC Panel GALLEY and CAB pb FAULT light (amber)
Any generator load > 100%
49
ELEC Panel GALLEY and CAB pb - OFF light (white)
Both Galleys and IFE are unpowered
50
ELEC Panel BAT 1 2 pb AUTO
-Battery contactors are closed when: -APU Start (max 3 min during EMER GEN operation) -Battery voltage < 26.5 until < 4 amps (after 30 min delay in flight) -AC1 and AC2 buses are unpowered, and < 100 kts, or EMER GEN not supplying power -Battery contactors are open if battery voltage is low (on the ground with no power supply)
51
ELEC Panel BAT 1 2 pb - FAUL light (amber)
Battery charger current out of limits
52
ELEC Panel BAT 1/2 pb - OFF light (white)
-Battery contactors are open [Light powered by DC BAT BUS] - OFF light will not illuminate unless one of the BAT pb is ON, or ground power is used.
53
ELEC Panel IDG 1 2 pb Fault Light (amber)
- High Oil Temperature | - Low Oil Pressure (inhibited below 14% N2)
54
ELEC Panel IDG 1/2 pb - pushed
-Disconnects IDG -Can only be reconnected on the ground Caution- the following may cause damage: -holding the pb for more than 3 seconds -disconnecting an engine that is not running or windmilling
55
ELEC Panel GEN 1 2 pb Fault Light (amber)
- GCU Trip | - Line contactor open (other than by pb)
56
ELEC Panel GEN 1 2 pb OFF Light (white)
- Generator will not power electrical system | - Reset
57
ELEC Panel APU GEN pb Fault Light (amber)
- GCU Trip - Line contactor open - (other than by pb or EXT PWR pb selected On) - inhibited at low speed
58
ELEC Panel BUS TIE pb AUTO
Automatically closes one or both contactors to maintain power supply to AC1 and AC2 based on aircraft priority system: -Engine Generator -External Power (if selected On) -APU Generator
59
ELEC Panel AC ESS FEED FAULT Light (amber)
AC ESS Bus not powered
60
ELEC Panel AC ESS FEED - ALTN Light (white)
AC 2 Bus supplies AC ESS Bus
61
ELEC Panel AC ESS FEED - normal
AC 1 Bus supplies AC ESS Bus
62
EMER ELEC PWR Panel GEN 1 Line pb SMOKE Light (amber)
Smoke detected in Avionics Compartment
63
EMER ELEC PWR Panel GEN 1 LINE pb - OFF Light (white)
- Gen 1 is disconnected from AC Bus 1 (Gen 2 then powers AC Bus 1) - Powers one fuel pump in each wing tank
64
EMER ELEC PWR Panel RAT and EMER GEN Fault Light (red)
Emergency Generator is not supplying power, but should be (AC1 and AC2 are not powered)
65
EMER ELEC PWR Panel RAT AUTO
Automatically extends the RAT which powers the Blue Hydraulic System which drives the Emergency Generator when: - AC1 and AC2 are unpowered - aircraft speed > 100 knots
66
EMER ELEC PWR Panel RAT MAN ON
- Manually extends the RAT and connects Emergency Generator to electrical system
67
FUEL Panel LTK PUMPS 1 2 & RTK PUMPS 1 2 - pushed (dark)
- Operating when Center Tank Pumps pressure low
68
FUEL Panel ``` LTK PUMPS 1 2 - FAULT light (amber) CTR TK PUMP 1 2 - FAULT light (amber) RTK PUMPS 1 2 - FAULT light (amber) ————————————— CTR TK L or R XFR - FAULT light (amber) ```
- Low output pressure ———————————— - The associated wing tank overflowed
69
FUEL Panel CTR TK PUMP 1 2 Pushed (dark)
- Pump is operating if MODE SEL is MAN - Pump is operating if MODE SEL is AUTO: - For 2 minutes after first engine start - Slats are retracted - 5 minutes after CTK TK low level is reached (550 lbs)
70
FUEL Panel MODE SEL Auto (dark) - a/c with center tank pumps
Center Tank Pumps operate: - For 2 minutes after first engine start - Slats are retracted - 5 minutes after CTK TK low level is reached (550 lbs)
71
FUEL Panel MODE SEL Fault Light (amber)
Center Tank > 550 lbs AND Left or Right Wing Tank < 11,000 lbs
72
FUEL Panel MODE SEL - MAN - a/c with center tank pumps
Center Tank Pumps are only controlled by pbs - must be manually turned off when: - CTR TK fuel depleted - Inner Tank is full due to IDG cooling fuel returning
73
HYD Panel ENG 1 2 PUMP Fault Light (amber)
- Reservoir problem: - Low level - Fluid Overheat - Low Air Pressure - Pump problem: - Low pump pressure (inhibited on the grd with engine off)
74
HYD Panel ENG 1 2 PUMP OFF light (white)
- Stops pump | - Turns off Fault Light except for overheat
75
HYD Panel RAT MAN ON pb Pushed
Extends RAT and powers Blue system (2500 psi) | [switch powered by Hot Battery Bus]
76
HYD Panel Blue ELEC PUMP On (dark)
Pump operates when electric power available, and: - In Flight - On the ground, after first engine start
77
HYD Panel Blue ELEC PUMP Fault light (amber)
- Reservoir problem: - Low level - Fluid Overheat - Low Air Pressure - Pump problem: - Low pump pressure (inhibited on the grd with engine off) - Overheat
78
HYD Panel Yellow ELEC PUMP Fault light (amber)
- Reservoir problem: - Low level - Fluid Overheat - Low Air Pressure - Pump problem: - Low pump pressure (inhibited on the grd with engine off) - Overheat
79
HYD Panel Yellow ELEC PUMP Off (dark)
-Pump if Off -Pump will be turned on, regardless of switch, if Cargo Door Lever moved to Open/Close -Turns off Fault Light except for overheat
80
HYD Panel PTU AUTO
Automatically runs when Green & Yellow differential psi >500 -self test during second engine start NOTE: PTU is inhibited: -during first engine start -for 40 seconds after cargo door is opened or closed -ONLY one ENG master switch on AND Tow Pin in -ONLY one ENG master switch on AND Parking Brake Set
81
HYD Panel PTU Fault light (amber)
- Reservoir problem: - Low level - Fluid Overheat - Low Air Pressure
82
HYD Panel PTU Off light (white)
- Power transfer stops | - Turns off Fault Light except for overheat
83
ENG FIRE Panel ENG 1 2 FIRE pb Released
- Silences CRC - Arms squibs -Closes Hydraulic Shutoff valve - Closes LP fuel valve - De-energizes FADEC -Deactivates IDG - Closes Bleed valve - Closes Pack flow control valve
84
ENG FIRE Panel APU FIRE pb Released
- Silences CRC - Arms squib - Closes LP fuel valve (APU shuts down) - Turns off APU fuel pump -Deactivates APU Generator - Closes APU Bleed valve - Closes X Bleed Valve
85
ENG FIRE Panel AGENT 1 2 SQUIB Light (white)
-Squib is armed (after FIRE pb popped)
86
ENG FIRE Panel AGENT 1 2 DISCH Light (amber)
-Bottle empty
87
ENG FIRE Panel ENG 1 2 Test pb Pushed
- CRC + MASTER WARN Light - ECAM - ENG FIRE pb Light - SQUIB Light - DISCH Light - FIRE Light on ENG panel
88
ENG FIRE Panel APU Test pb Pushed
-CRC + MASTER WARN Light -ECAM -APU FIRE pb Light* -SQUIB Light* -DISCH Light* (* If DC power only)
89
CARGO HEAT Panel HOT AIR pb Fault Light (amber)
-Duct overheat
90
CARGO HEAT Panel AFT ISOL VALVE Fault Light (amber)
-Inlet or Outlet valve disagreement
91
CARGO HEAT Panel AFT ISOL VALVE OFF Light (white)
- Inlet & Outlet Isolation valves close - Trim air valve closes - Extraction fan stops
92
CARGO HEAT Panel AFT ISOL VALVE - AUTO
- Inlet & Outlet Isolation valves open | - Extraction fan on (if no smoke detected)
93
CARGO SMOKE Panel DISCH switch Pushed
-Ignites squib and discharges single bottle into corresponding compartment
94
CARGO SMOKE Panel FWD/AFT SMOKE Light (red)
Smoke detected: - By both channels - By one channel + other failed
95
CARGO SMOKE Panel FWD/AFT DISCH Light (amber)
-Bottle pressure low
96
VENTILATION Panel BLOWER pb Fault Light (amber)
Smoke Air pressure low * Computer Fault Overheat* *horn sounds if on the ground + no engines running
97
VENTILATION Panel BLOWER pb OVRD (white)
- Goes to Closed Configuration (inlet and extract valves close) - Air Conditioning air added - Blower Fan stops
98
VENTILATION Panel EXTRACT pb Fault Light (amber)
Smoke Air pressure low* Computer Fault *horn sounds if on the ground + no engines running
99
VENTILATION Panel EXTRACT pb OVRD (white)
- Goes to Closed Configuration (inlet and extract valves close) - Air Conditioning air added
100
VENTILATION Panel BLOWER and EXTRACT pb Both AUTO
On the ground: - prior to takeoff power, OPEN configuration - after takeoff power, CLOSED configuration *May be in Closed Config prior to takeoff power if skin temperature is too cold
101
VENTILATION Panel BLOWER and EXTRACT pb Both OVRD
- Smoke Configuration - Air Conditioning air added - Blower Fan stops - Small door on extract valve opens
102
ENGINE CONTROL Panel Fault Light 1 2 (amber)
- Automatic start abort | - HP fuel valve disagreement
103
CABIN PRESS MODE SEL pb AUTO
2 Auto modes automatically transfer control: -70 seconds after each landing -if operating system fails Deselect for 10 seconds may switch AUTO system being used
104
CABIN PRESS Mode SEL FAULT Light (amber)
Both Auto systems failed
105
ANTI ICE WING pb FAULT Light (amber)
- Low pressure - Either valve disagreement with pb - Either valve in transit
106
ANTI ICE ENG 1 2 pb FAULT Light (amber)
- Valve disagreement | - Valve in transit
107
``` GEAR EXTN Handle Pulled and Turned clockwise ```
- First turn, isolates landing gear from Green system - Second turn, opens landing gear doors (mains and nose) - Third turn, releases landing gear - Gear doors remain open
108
``` Cockpit Door Fault Light (red) ```
System Failure (i.e. latch, control unit, pressure sensor, etc)
109
CABIN PRESS DITCHING pb ON - white light
``` Closes: -Avionics ventilation inlet valve -Avionics ventilation extract valve -Both pack flow control valves -Ram air inlet valve Outflow valve (If under AUTO control) ```
110
When does the AUTO LAND light illuminate?
Accompanied by a triple-click, this light flashes when: - At least one RA indicates below 200 ft, and - At least one autopilot is engaged in the LAND or FLARE mode, and - At least one of the following occurs: —- LOC exceeds 1/4 dot above 15 RA —- The g/s exceeds 1 dot above 100 RA —- Loss of LOC signal above 15 RA —- Loss of g/s above 100 RA —- Difference between both RA exceeds 15 RA —- Last autopilot disengages —- FMGS detects a long flare —- FMGS detects and untimely flare. This occurs when one RA is union and the time between LAND and FLARE is less than 2 seconds
111
FUEL Panel MODE SEL - AUTO - a/c with center tank transfer valves
- The valves open if the associated inner tank is not full. - The valves close 5 minutes after center tank low level is reached (550 lbs).

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