Lights & Switches Flashcards by Jonathan Walmsley

What information is provided by the “IR” units?

What information is provided by the “ADR” units?

IR UNITS Provide

F-Flight Path Vector A-Airplane Position T-Track H-Heading A-Attitude A-Acceleration G-Groundspeed

ADR UNITS Provide

B-Barometric altitude O-Overspeed warnings A-AOA

T-Temperatures S-Speed/Mach

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ADIRS Panel Data Selector Knob TEST

Display shows all 8s

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ADIRS Panel Data Selector Knob TK/GS

Displays True Track and Groundspeed

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ADIRS Panel Data Selector Knob PPOS

Displays Present LAT/LONG

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ADIRS Panel Data Selector Knob WIND

Displays True Wind Direction/Speed

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ADIRS Panel Data Selector Knob HDG

Displays True HDG and TTN (Time to Nav)

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ADIRS Panel Data Selector Knob STS

Displays Action Code

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ADIRS Panel SYS Selector Knob 1/2/3 OFF

1/2/3 = Selects IR to Display/Input Data Off = Display Unpowered

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ADIRS Panel ADIRS ON BAT Light (Amber)

1 - One or more of the IRs are on BAT power.

2 - Self Test during a full allignment.

3 - External horn will sound.

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ADIRS Panel

IR 1/2/3 Fault Light
Steady Amber

Fault in IR

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ADIRS Panel
IR 1/2/3 Fault Light
Flashing Amber

Attitude and Heading may be recovered using ATT mode

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ADIRS Panel

IR 1/2/3 Align Light
Steady White

Normal during Alignment

(approx. 10 minutes)

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ADIRS Panel

IR 1/2/3 Align Light
Flashing White

No position entered within 10 minutes
Bad position (1º or 60nm)
Fault (A/C moved during Alignment)

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ADIRS Panel

IR 1/2/3 Rotary Selector
NAV

Normal Mode Supplying Full Inertial Data

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ADIRS Panel

IR 1/2/3 Rotary Selector
ATT

Attitude and Heading only

Supplied when GPS operational then data entered automatically.

Otherwise manually

Enter magnetic Heading using keyboard (i.e. H9990)
every 10 Minutes
4th Digit is Tenths
Converts to True HDG

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ADIRS Panel

IR 1/2/3 Rotary Selector
OFF

ADIRU Unpowered
Wait 10 seconds before un-powering A/C Electric System

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ADIRS Panel

ADR 1/2/3 Fault Light
(Amber)

Fault in Air Data

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ADIRS Panel

ADR 1/2/3 OFF Light
(White)

No ADR Output

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ADIRS Panel

How long will each ADIRU stay on battery power

ADIRS 2 and 3 will remain on battery power for 5 minutes to hold alignment until a generator can be restored.

ADIRU 1 (ADIRU 3 if captain selected ATT HDG CAPT 3) will remain on battery power until generator power is restored or battery #2 fails

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FLT CTL Panel

ELAC 1/2
Pushed (dark)

Elevator Aileron Computer
PARAAA
Pitch in ALL laws (NAD)
Abnormal Attitudes
Roll in Normal/Direct law (ND)
Autopilot Acquisition of orders
Aileron Droop
Activates the protections

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FLT CTL Panel
ELAC 1/2

1 - FAULT light is amber
2 - OFF light is white

1 - FAULT or Self test during start up

2 - Computer is off

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FLT CTL Panel

SEC 1/2/3
Pushed (dark)

Spoiler Elevator Computer
PARSS
Pitch in Alternate/Direct law
Abnormal Attitudes
Roll in Normal (spoilers) / Direct law
Speed Brakes (FLT surface 2,3,4)
Spoilers (grnd spoilers sec 1/3) (all flt surfaces)

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FLT CTL Panel

1 - SEC Fault Light is amber

2 - OFF light is white

1 - Fault

2 - computer is off.

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FLT CTL Panel

FAC 1/2
Pushed (dark)

Flight Augmentation Computer
BSWFTRATTY
Beta Target
Speed (Flaps/2000ft/100ft/Warns/Alpha Floor)
Windshear Protections
Flight Envelope Protections
Tail Controls
Rudder Limiting
Alternate Law Yaw
Turn Coordination
Trim
Yaw Damping

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FLT CTL Panel FAC 1/2 1 - Fault light amber 2 - Off light white

1- Fault 2- Computer is off

GPWS TERR PB Fault

EGPWS Failure (Turn off airborne if airport not in database)

GPWS TERR PB Off

Terrain Function Inhibited

GPWS SYS PB Fault

Modes 1-5 Failed

GPWS G/S Mode pb OFF Flap Mode pb OFF

**G/S Mode OFF =** GPWS is disabled/inhibited **Flap Mode OFF =** "Too Low Flaps" warning disabled/inhibited

GPWS LDG Flap 3 PB OFF

LDG Memo Changed to display Flaps 3 | (Used when landing Flaps 3 instead of Full)

RCDR GND CTL ON Light Blue

Cockpit Voice and Digital Flt data Rec are temporarily/manually ON

RCDR GND CTL AUTO PB Pushed

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 / In Flight

RCDR CVR ERASE PB Pushed

Erases Tape (2 Hours) when: Held for 2 seconds On the Ground Parking Brake On

RCDR CVR TEST PB Pushed

Activates Tests when: CVR is powered Parking Brake is ON

OXYGEN MASK MAN AUTO or MASK MAN ON pb

When Cabin ALT exceeds 14000 (when in auto) or the MASK MAN is manually pushed the masks will deploy and pre-recorded instructions on how to use mask will be broadcast.

OXYGEN PASSENGER SYS ON Light (White)

SYS ON indicates a signal has been sent to open the OXY mask doors.

OXYGEN With the PASSENGER SYS ON Light (White)... How can this be reset?

Light remains on until MX have reset

OXYGEN CREW SUPPLY OFF Light (White) CREW SUPPLY (pb dark)

pb OFF illuminated = Valve CLOSED....... pb DARK = Valve OPEN..... With this pb in the off position or the pb dark will simply reflect that there is no or is O2 available to the crew

OXYGEN How many masks in each row? How long will they last for?

4 per row 13/15 minutes

SIGNS NO SMOKING AUTO ON/OFF

AUTO No smoking and exit signs Illuminate/Extinguish along with a chime when landing gear extended (illuminate) and retracted (extinguish) ON/OFF (switch) No smoking and exit signs Illuminate/Extinguish along with a chime when the switch is placed in the on (illuminate) or off (extinguish) position.

SIGNS EMER EXIT LT ARM Loss of AC BUS 1 causes Illumination of Loss of DC ESS SHED causes illumination of

Loss of AC BUS 1 causes Illumination of- Overhead Lights Loss of DC ESS SHED causes illumination of - Path Lighting Overhead Lights Exit Signs

EMER EXIT LT ON

Overhead EXIT signs and proximity marking system Lights illuminate

APU Master Switch PB FAULT

Auto Shutdown for many reasons. Fire will only cause auto shutdown on the ground

APU Master Switch PB ON Light (Blue)

**Fuel** pump on Fuel **ISOLOATION** valve opens * *Flap** Opens * *ECAM** Page Appears * *Self** Test ECB **FIFES**

APU Master Switch pb is turned OFF - what is happening

Master Switch ON light and Start AVAIL lights extinguish although shutdown is delayed for approx 2mins assuming the APU Bleed was in use.. Flap closes.

APU START pb AVAIL Light (Green)

N \> 99.5% N \> 99 % for 2 seconds

APU START pb ON Light Blue

APU Starts

CABIN PRESS MAN V/S CTL UP/DN

With the MODE SEL switch in manual the the MAN V/S CTL UP/DN can be controlled manually by the pilot.

CABIN PRESS MODE SEL PB AUTO

The 2 modes run automatically and no pilot intervention is required when managing the pressurization system.

CABIN PRESS MODE SEL PB FAULT

Both Auto Systems Failed

CABIN PRESS MODE SEL PB MAN (White)

Activates MAN V/S CTL Toggle switch

CABIN PRESS LDG ELEV AUTO

Landing Elevation from FMGS being used to control pressurization schedule.

CABIN PRESS LDG ELEV -2 through 14

Pull Out and Turn to select landing field elevation if not in FMGS database

CABIN PRESS DITCHING PB ON

PARO PACK flow valves close Avionics in/outlet valves close RAM Air inlet valve closes Outflow Valve closes

PROBE/WINDOW HEAT pb AUTO / ON

AUTO (light out) = Automatic heating of probes/windows inflight and on the ground if an engine is running (TAT probes excluded on grnd). ON = Continuous heating of probes/windows.

ANTI ICE WING PB FAULT Light (Amber)

Low Pressure Either Valve Disagreement with PB or Either Valve in Transit

ANTI ICE WING PB ON Light (Blue)

ECAM - Wing A.ICE. Air available then both valves will open. Ground Ops will result in a 30sec self test.

ANTI ICE ENG 1/2 PB FAULT

Valve Disagreement Valve in Transit

ANTI ICE ENG 1/2 PB ON (Blue)

Respective Valve Open if Air Avail ECAM - ENG Anti Ice

WING ANTI ICE Which Slats are heated? Default Valve Position?

Which Slats are heated? - Outboard 3 Default Valve Position? - Closed

ENG ANTI ICE Default Valve Position?

Open

AIR COND What is the Temp Selector range

Cold 64F 12 o'clock 76F Hot 86F

AIR COND PACK FLOW selector LO/NORM/HI - what are the parameters?

LO - 80% Less than 115 PAX NORM - 100% More than 115 PAX HI - 120% Select if abnormally Hot/Humid

AIR COND PACK 1/2 PB Pushed

Opens Pack Valve UNLESS: Start in Progress Air Press Low Ditch Switch Selected Fire PB released Overheat in Comp outlet SADFO

AIR COND PACK 1/2 PB FAULT

- Overheat of compressor and/or pack outlets - Disagreement of valve position

AIR COND 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 LOOSAFA

AIR COND ENG 1/2 BLEED PB FAULT

Leak Overheat Overpressure Start In Progress and Valve open APU Bleed On and Valve open LOOSA

AIR COND RAM AIR PB ON

-RAM AIR Inlet Opens -Outflow Valve Opens 50% if: Differential PSI \<1 and not being controlled manually

AIR COND APU BLEED PB FAULT

Leak

AIR COND APU BLEED PB ON Light

Opens Valve when pushed and N\>95% No Leak

AIR COND X BLEED Selector SHUT

Closed

AIR COND X BLEED Selector AUTO

- Opens if APU Bleed Valve is Open. - Closes if APU Bleed Valve is Closed and/or a leak in Wing/APU/Pylon

AIR COND HOT AIR PB FAULT

Overheat detected Closes Hot Air Valve and Trim Air Valve

AIR COND HOT AIR PB OFF

Hot Air Valve Closed Trim Air Valve Closed

ELEC COMMERCIAL pb ON COMMERCIAL pb OFF

Powers the LODGE Lights for Cabin/Cargo Oval Office / Toilets Drain Mast Ice Protection Galleys Entertainment system IFE OFF = All Unpowered except Coffee

ELEC GALLEY PB AUTO

Powers: - Galleys - Entertainment Equipment -One GEN only during any operations will result in main galley and entertainment equipment to be shed and can only be recovered by using an operational APU or EXT GRD power

ELEC GALLEY PB FAULT

Any Generator Load \>100%

ELEC GALLEY PB OFF

Galleys and Entertainment equipment are ALL off.

ELEC BAT 1/2 PB AUTO

_{When AUTO the contactors open/close auto under certain conditions.} _{OPEN -} * _{On ground with BAT volt LOW and no PWR avlb..} _{CLOSE -} * _{APU Starts} * _{BAT VOLT <26.5 until 4amps} * _{AC Busses (1/2) unpowered and <100kts and emer gen not supplying power.}

ELEC BAT 1/2 PB FAULT

Battery charger current is out of limits

ELEC BAT 1/2 PB OFF

Battery Contactors are Open pb Light powered by Hot Battery Bus

ELEC IDG 1/2 PB FAULT

High Oil Temp Low Oil Pressure (inhibited below 14% N2)

ELEC IDG 1/2 PB Pushed

- Disconnects IDG - Can only be reconnected on ground -----------CAUTION - Holding PB for more than 3 sec or disconnecting an engine that is not running or windmilling may cause damage

ELEC GEN 1/2 PB FAULT

GCU Trip Line Contactor Open (other than by pb)

ELEC APU GEN PB FAULT

GCU Trip Line Contactor Open - (other than by pb or EXT PWR pb selected On) -inhibited at low speed

ELEC BUS TIE PB AUTO

Automatically closes one or both contactors to maintain power supply to AC1 and AC2 based on Aircraft priority system: Online ENG Gen - External Pwr - APU GEN - Offline ENG Gen

ELEC EXT PWR PB AVAIL Green

Plugged in and Good Power

ELEC EXT PWR PB ON Light Blue

EXT PWR PB is selected ON

ELEC AC ESS FEED PB FAULT

AC ESS Bus not Powered

ELEC AC ESS FEED PB ALTN Light (White)

AC2 Bus supplies AC ESS Bus

ELEC AC ESS FEED PB Normal

AC1 Bus supplies AC ESS Bus

EMER ELEC PWR EMER GEN TEST Guarded

Used by MX to test Emerg GEN

EMER ELEC PWR EMER GEN 1 LINE PB SMOKE

Smoke detected in Avionics Compartment | (Also triggers VENTILATION Blower and Extract FAULTS)

EMER ELEC PWR EMER GEN 1 LINE PB OFF

- Gen 1 is disconnected from AC Bus 1 thus Gen 2 powers AC Bus 1 - Powers one fuel pump in each wing tank

EMER ELEC PWR RAT & EMER GEN Fault Light RED

Emer GEN is not supplying Power but should AC bus 1 & 2 are not powered

EMER ELEC PWR RAT AUTO

With the AC Busses unpowered the RAT auto deploys and powers the BLUE hydraulic system which then drives the EMER Gen when the speed is in excess of \>100kts

EMER ELEC PWR RAT MAN ON

Manually selecting ON will deploy the RAT and activate the emergency generator.

FUEL L/R TK PUMPS 1/2 PB Pushed (DARK)

Pump is on and will operate when CTR TNK Pump has low pressure

FUEL L/R TK PUMPS 1/2 PB FAULT

Low Pressure

FUEL CTR TK PUMP 1/2 PB Pushed (DARK)

Pump Commanded on and activates the associated center tank pump

FUEL CTR TK PUMP 1/2 PB FAULT

Low Pressure

FUEL MODE SEL PB AUTO

When in auto the CTR TNK Pumps Operate for - 2 Mins after each engine start (reach grnd idle) - 5 Mins after CTR TNK reaches low level (550lbs) - Slats retracted

FUEL MODE SEL PB FAULT

Fault light illuminates when the CTR tank fuel is +550 and either wing tank is -11000lbs of fuel.

FUEL X FEED PB OPEN Green

Valve Fully Open

HYD ENG 1/2 PUMP ON

Pump runs when ENG is running

HYD ENG 1/2 PUMP FAULT

PROLL = Low **PUMP** pressure RESERVOIR -Overheated oil -Low Air Pressure -Low Level

HYD ENG 1/2 PUMP OFF

Turns Pump Off | (FAULT Light goes out except for Overheat)

HYD RAT MAN ON PB Pushed

Extends RAT and Powers Blue System (2500psi)

HYD BLUE ELEC PUMP PB ON (AUTO)

Pump Operates when electric Power is available * In Flight * On Ground with at least one engine running

HYD BLUE ELEC PUMP PB FAULT

POROLL = PUMP - Pressure is low - Overheat RESERVOIR - Overheated oil - Low Air Pressure - Low Level

HYD YELLOW ELEC PUMP ON

Pump operates when electric power available

HYD YELLOW ELEC PUMP PB FAULT

POROLL = PUMP - Pressure is low - Overheat RESERVOIR - Overheated oil - Low Air Pressure - Low Level

HYD YELLOW ELEC PUMP PB OFF

Pump is OFF except when Cargo Door operated

HYD PTU AUTO

* Auto Runs when the Green/Yellow diff pressure exceeds 500psi * Self Test during 2nd engine start up **PTU IS INHIBITED** * During Cargo door operations for 40 seconds * One ENG master switch on and TOW pin in * One ENG master switch on and parking brake set

HYD PTU FAULT

RESERVOIR - Overheated oil - Low Air Pressure - Low Level (Note that these faults are indicated if either the Green or yellow reservoirs are effected)

ENG FIRE PB Released

2-1-2-1-2 2 - Silence CRC / Arms Squib 1 - Hydr Shutoff Valve Closes 2 - LP Fuel Valve closes / FADEC Deenergizes 1 - Deactivates the Generator 2 - Pack Valve and Engine Bleed Valve Close

APU FIRE PB Released

2-0-2-1-2 2 - Silence CRC / Arms Squib 0 - Hydraulics - Nothing 2 - Low Press Fuel Valve closes / Fuel pump turns off 1 - Deactivates APU GEN 2 - APU Bleed Valve Closes / Cross Bleed Valve Closes

ENG FIRE TEST PB

CRC & Master Warning Light ECAM ENG FIRE PB light Squib Light DISCH Light Fire Light on ENG Panel

APU FIRE TEST PB

CRC & Master Warning Light ECAM APU Fire PB Light\* Squib Light\* DISCH Light\* (\*if DC power only)

CARGO HEAT HOT AIR PB FAULT

Duct Overheat

CARGO HEAT HOT AIR PB OFF

Valve Closes

CARGO HEAT HOT AIR pb AUTO

Valve regulates Hot Air Pressure

CARGO HEAT AFT ISOL VALVE FAULT

Inlet or Outlet Valve Disagreement

CARGO HEAT AFT ISOL VALVE AUTO

-Valves Open (Inlet & Outlet Isloation) - Extraction Fan ON (if no smoke detected)

CARGO HEAT AFT ISOL VALVE OFF

- Inlet & Outlet Isolation Valves CLOSE - Trim Air Valve CLOSES - Extraction Fan Stops

CARGO SMOKE DISCH SWITCH Pushed

Ignites squib and discharges single bottle into corresponding compartment

CARGO SMOKE FWD/AFT SMOKE Light Red

Smoke Detected By - Both Channels or - One channel and the other has failed

CARGO SMOKE FWD/AFT DISCH Light

Bottle Pressure Low

VENTILATION BLOWER PB FAULT

Smoke Air Press Low\* Computer Fault\* Overheat\* \*(Horn sounds on Ground)

VENTILATION BLOWER PB OVRD (White)

Goes to Closed Configuration (Inlet and Extract Valves Close) AC Air added Blower Fan stops

VENTILATION BLOWER & EXTRACT PB Both AUTO

On the Ground: Prior to T/O power - Open Config After T/O power - Closed Config

VENTILATION EXTRACT PB FAULT

Smoke Air Pressure Low\* Computer Fault (\*Horn sounds if on Ground no Engines running.)

VENTILATION EXTRACT PB OVRD (White)

Goes to Closed Configuration (Inlet and Extract Valves Close) AC Air added

VENTILATION BLOWER & EXTRACT PB OVRD

Intermediate Config AC Air added Blower Fan Stops (SMOKE CONFIG)

``` LANDING GEAR UNLK Light (Red) ```

Not Locked in Selected Position | (LGCIU 1)

LANDING GEAR ARROW (Green)

Down & Locked | (LGCIU 1)

LANDING GEAR Isolated from Hydraulics by Computers? Speed?

ADR's 1 & 3 260 kts

AUTO BRAKE pb LO MED MAX

Ground Spoiler Extension AND LO - 4 Seconds MED - 2 Seconds MAX - Immediately \> 40 kts GRND Spoilers extend at 72 kts (rejected TakeOff)

``` AUTO BRAKE DECEL Light (Green) ```

Deceleration is 80% of selected rate

PARKING BRAKE Pressure Maintained for

12 Hours

ENGINE MODE Selector CRANK

Start Valve OPENS if ENG MAN START pb ON

ENGINE MODE Selector NORM

IGN Energises when EIU Fails Flameout Detected

IGN/START

PACE Pack valve closes IGN Armed Continuous IGN when ENG 1/2 Switch ON & N2 above Idle ECAM page displayed

ENG 1/2 Switch ON

With the ENG(s) switch turned to on this will - Open LP Fuel Valve and Start Valve - APU Air Increases - Energizes IGN when N2 +16% (immediate in flight)

ENG 1/2 FAULT Light

Automatic Start ABORT HP Fuel Valve Disagreement

During Start, When Does HP Fuel Valve OPEN?

N2 \> 22% on Ground N2 \> 15% In-Flight

During Start, What Occurs @ 50% N2

VALVES - Start closes and Pack open after 30secs IGN De-energized APU Speed back to normlal

Wingtip Brake Activation

Runaway Overspeed (to quick of movement) Asymmetrical Movement/Position Movement Uncommanded R-O-A-M

Flaps Auto-Retract when?

1 + F Selected Speed Exceeds 210 kts

4 Modes of Braking are

Normal Alternate w/ Anti-Skid Alternate w/o Anti-Skid Parking Brake

NORMAL BRAKING Which HYD System? Anti-Skid? Auto-Brakes? Cockpit Pressure Indication?

Green System YES - A/S YES - A/B NO - Indication

ALT BRAKING w/ ANTI-SKID Which HYD System? Auto-Brakes? Cockpit Pressure Indication?

Yellow System NO- A/B YES - Indication

ALT BRAKING w/o ANTI-SKID Which HYD System? Auto-Brakes? Cockpit Pressure Indication? How Many Full Brake Applications?

Yellow (Accumulator Only) NO- A/B YES - Indication 7 Applications

PARKING BRAKE Which HYD System? How Long is Pressure Maintained? Cockpit Indication?

Yellow or Accumulator 12 Hours YES - Triple Indicator

BRAKE TEMP. (Hottest Wheel) Green Arc Amber Arc

\> 100º C \> 300º C

ANTI-ICE HOT AIR heats?

3 outboard Slats Engine Nacelles

ANTI-ICE ELEC Heats?

Cockpit Windows Sensors, Probes & Static Ports Waste Water Drain Mast

WING ANTI-ICE (when Selected) N1 Limit Idle N1 Leak Causes?

N1 Limit Reduced Idle N1 Increases Leak Causes Valve to CLOSE

ENG ANTI-ICE Supplied by? What Happens When No Air? N1 Limit

HP Air Valve CLOSES N1 Limit Reduced N1 Increases to Maintain Pressure

PNEUMATIC System Supplies

Water Pressurization Engine Start Hydraulic RES Pressurization Air Conditioning Wing Anti Ice

ENG BLEED System Components?

PEV Pre Cooler Extractions - High HP and Intermediate IP Valves - Crossbleed / Bleed Shutoff / HP Shutoff

BLEED LEAK Detection can be found where

Fuselage - APU Air (1 Loop) ``` Engine Pylons (1 Loop) Wings (2 Loops) ```

BLEED PRIORITY

APU Bleed over ENG Bleed

AVIONICS VENTILATION Cools?

Avionics Compartment Flight Deck Instruments CB Panels

Lights & Switches Flashcards

(164 cards)