Indicating System, Lights, CIDS, and Ice & Rain Protection

It displays the data from the Air Data and Inertial Reference System (ADIRS) plus navigation data from the Flight Management and Guidance System (FMGS) is fed directly to the DMCs.

It processes the data and generates the images to display in the EFIS.

It used adjust the brightness of the associated PFD and ND, and to turn the displays off.

Are used to select what is displayed on the EFIS screens.

A single electrical ............. Gives the Universal Time Coordinated (UTC) and date as time references for the crew and all peripheral systems.

The clock cannot be synchronized with satellite GPS time.

The location where time can be seen in System Display (SD)

Drain mast heating faults may be displayed on the

Drain mast heating faults may be displayed on the

Wing and engine anti-ice valve position and the valves P/BSW position are monitored by

All 3 PHCs, both WHCs, and the ice detectors are connected directly to the

Remove the _____________ from the probes before activating the probe ice protection system.

Do not touch the________ , ________ , and ________ until they are cool. Those items stay hot for some time after the engine shuts down.

The window heat system is designed in order to keep the windows fogged (in flight) in case of a WHC failure.

If the PHC or WHC power Circuit Breakers (C/Bs) are pulled, the probe and window heat will come on.

Pulling the EIU C/B will have the probe and window heat to come on.

The probe heat system is a fail-safe system in order to keep the probes and static ports de-iced (in flight) in case of a PHC failure.

It centralizes and memorizes all information concerning AIRCRAFT system failures.

Reading or printing of the failure information is done in the cockpit with any _______.

It enables a dialogue between the CFDIU and a system computer.

The heart of the DFDRS.

On the _______, there is a DFDR EVENT P/B which can be used to set an event mark on the SSFDR memory.

Used to select the desired computer to be loaded.

Data loading system includes a stowage box with a _____ -disk maximum capacity.

It is an interface between the aircraft computers and ground data processing equipment used to update software (S/W) and data base or to retrieve aircraft system data.

It measures the acceleration of the AIRCRAFT in all three axes.

It helps the maintenance crew to make a correlation for easier troubleshooting.

AIDS

Heart of ECAM

Main function of AIDS

Collection, processing and recording of various AIRCRAFT parameters, including the mandatory parameters given by the _____.

FDIMU

FDIMU has ____ to upload DMU software and upload DMU data.

PCMCIA

To initiate communication with the AIDS via either ______, the user has to press the AIDS line select key from the ______ MENU page.

The FDMIU has a PCMCIA card slot to upload DMU data and download DMU software

Modified True or False: Replace the word inside the parenthesis if false. The Data Management Unit is the heart of (ECAM).

CFDS means:

The DFDRS and AIDS computers are located in the

The FDIMU computer on the Enhanced system is located in the

The SSFDR is installed, the Cockpit Voice Recorder (CVR)

The SSFDR stores, in a solid-state memory located in a

The linear accelerometer is near the aircraft _______.

The SSFDR stores, in a solid-state memory located in a crash- and fire-protected housing, the data of the last hours collected by the FDIU.

It sends the accelerations according to the 3 axes (pitch, roll and yaw) to the .

Using the , you can have access to the fault messages of all the indicating/recording systems

When conducting indicating tests, make sure that all persons are more than _______ meters from the weather radar.

It is used for the control and management of all the cabin systems presented in the graphic.

Composed of two directors, one in active mode, and one in hot standby.

Used to program and test the CIDS.

The director communicates through _____ with the cabin, passengers, and crew systems.

Integrated within Forward Attendant Panel are; except.

These signs are controlled from the cockpit; except.

Control of pre-recorded announcement and music contained in the PRAM is performed from this panel.

CIDS stands for

PRAM stands for

OBRM stands for

The emergency evacuation command may be activated from the purser station or from an optionally-installed __________?

The emergency evacuation command and reset pushbuttons at the purser station are located on the____?

On the Enhanced FAP, emergency evacuation command and reset pushbuttons are located on the ______?

It is possible to control and monitor aircraft systems from the ____ and from the____.

The CIDS and related cabin systems are controlled and monitored from the FAP by its associated page. The cabin systems are:

_________ is equipped with the FAP

_________ is located next to the FAP behind a hinged access door

Contains all the software for specific customer layouts and defined parameters

Tells the crew about the status of the cabin systems

On the Enhanced CIDS system, the PTP is removed

Located on AFT section

Located on FWD section

An Additional Attendant Panel (AAP) and an Attendant Indication Panel (AIP) is located in the

Indicates crew calls, passenger call, lavatory call, and lavatory smoke detection

Color for lavatory call

Color for passenger call

Color for cabin crew call (cabin to cabin)

Color for cabin crew call (pilot to cabin)

Color for lavatory smoke detection

CIDS stands for_______

The passenger entertainment system is composed of the audio reproducer, the DIU, and the main multiplexer. What is DIU?

In the passenger entertainment system, what does IFE stands for?

What does PRAM stands for?

TRUE OR FALSE: The number of DEUs installed depends on fuselage length and configuration of passenger entertainment systems.

What does DEU stands for?

The main components of the CIDS are the directors. Director 1 is ________ and director 2 is __________, in normal operation.

On the Enhanced system, the CIDS Director BITE is only accessible from the CFDIU through the MCDU.

In the Classic system, CIDS Bite is accessible through the following except:

Do not touch the lamp glass with your fingers. The oils from your skin will quickly cause deterioration of the lamp.

If you accidentally touch the lamp glass, clean it with a clean rag.

Number of lighting systems in the A320:

Which is not included in the cockpit light system?

Cockpit Lights control are located in:

The Captain and First Officer reading lights contain a ______ for brightness control and a slider for beam control.

The ______ contains the controls for the overhead panel integral lighting, standby compass integral light, the dome lights, and the annunciator lights.

Controls the integral lighting of the glareshield and Flight Control Unit (FCU) displays.

The side console light controls are on panels located on the center pedestal of the main instrument panel.

The ambient lighting is supplied by:

Map lights bring light to: the side consoles, briefcase areas, and the floor around the pilot seats

Various cabin light and sign systems are controlled, tested, and monitored by the

The ___ communicates through Decoder Encoder Units (DEUs) with the cabin, passenger and crew systems.

The ___ is used to program and test the CIDS and the related light systems.

Emergency lights inside the cabin includes:

The emergency lights are provided by several of these units.

How many exterior emergency lights housed in the fuselage are there?

The exterior emergency lights automatically activate when an overwing emergency exit door ________ in the armed configuration.

Exterior lights controls are on the EXT LT panel located on the _____.

Taxi, turn off lights, navigation, strobe, beacon, wing lights, takeoff and landing lights are all under

Are high intensity white lights which flash at a regular interval. They are the brightest lights on the aircraft and are used to signal that an aircraft is entering or approaching an active runway, or for visibility in the dark, clear sky.

Consist of a red light on the left/port wing tip, a green light on the right/starboard wing tip and a white light on the aircraft tail.

Helps ensure that both flight crew and vehicle drivers follow the correct taxiway routes at night and in low visibility and correctly stop as their ATC clearance limits.

Are similar to taxi lights except they are mounted on an angle pointing to the left and right of the aircraft nose. These lights will illuminate taxiways or obstacles on either side of the aircraft.

A light mounted on the fuselage, which lights up the wing leading edges to indicate to the pilot the buildup of ice on the wing at night.

It is an anti-collision light and is always red. They are found at the top of the fuselage and the bottom of the fuselage.

CIDS related lights system can be monitored and tested via _____ and PTP

CIDS related lights system can be monitored and tested via MCDU and ______.

_________ switch on PTP starts test procedure of complete lights system

_________ switch on PTP tests battery condition in each power supply unit.

Enhanced System: CIDS BITE only accessible from MCDU through the ______.

When you work on the lights system, make sure that you obey __________.

Do not disconnect the electrical connections for at least _______ after you de-energize the electrical circuits.

Do not remove a strobe light for at least _______ after you de-energize the electrical circuits. The high voltage electrical current in the capacitor of the strobe light is dangerous.

Do not touch the strobe lights for at least ________ after operation. The strobe light will still be hot.

Which of these can be used for anti-icing?

Hot air from the pneumatic system is supplied for the anti-icing of the three _____ of each wing

Bleed air from the engines or the APU is supplied to each wing through a pressure regulating and shut off valve called _____.

Whenever WAI is selected, the engine idle is _____and the Takeoff/Go Around (TOGA) limit (max thrust) is ______by the FADEC.

Whenever WAI is selected, the engine idle is increased and the Takeoff/Go Around (TOGA) limit (max thrust) is decreased by the FADEC. This signal is sent to the FADEC through the ______.

For testing purposes, WAI can be selected on the ground but will be automatically limited to _______ of operation to prevent damage to the wing leading edge.

Each engine air intake is protected from ice by an independent air bleed supply from the _______ compressor of that engine.

Each engine air intake is protected from ice by an independent air bleed supply from the High Pressure (HP) compressor of that engine. The air is supplied through the _________.

True or False ; Engine anti-ice is manually selected by the crew and is available in flight or on the ground with the engine running.

Where does the air go after it circulates around the engine inlet for Anti-Icing?

TRUE or FALSE : In the event of an electrical power supply failure, the engine air intake anti-ice valve will automatically open when the engine is running.

Whenever engine anti-ice is selected, the engine idle is increased and the TOGA limit (max thrust) is decreased by the FADEC. The FADEC also turns on continuous ignition. This signal is sent to the FADEC through the _____.

What is the meaning of ZC?

The heating system for each channel is controlled and monitored by a ______

________ is supplied for windshield anti-icing and cockpit side window de-fogging.

The ________ (normally in the AUTO position) may be used to select the window heating ON with the engines shut down.

The heating system for each side is controlled and monitored by a _______

The ________ is discharged onto the left or right windshield from a pressurized canister installed at the rear of the cockpit.

In order to give reliable information to the air data systems, the air data probes are heated automatically when all the engine is running

The sensors turn off the heat when the temperature reaches the limit and the windows are heated at a lower power on the ground than in flight.

Rain removal from the windshield is only done by a rain repellent system in heavy rain.

Ice protection of the Angle of Attack (AOA) sensors, pitot probes, static ports, and Total Air Temperature (TAT) probes is achieved by electrical heating.

LGCIU means ___

The Electronic Instrument System (EIS) has _____ display units.

ECAM means?

EFIS stands for?

DMC means?

TRUE OR FALSE: In a classic ECAM setup, the SDAC receives data from the AIRCRAFT system sensors and sends it to the FWC before it is sent to the DMC by the FWC.

TRUE OR FALSE: The ECAM Master Warning indicator glows RED when there is a warning that needs immediate action. It is placed below the ECAM Master Caution indicator, which glows AMBER when an action needs the attention of a flight crew, but not of utmost urgency.

TRUE OR FALSE: In a classic ECAM setup, during regular operation, the DMC 1 supplies the upper ECAM display, while DMC 2 supplies the lower ECAM display. DMC 3 acts as a backup when one fails.

TRUE OR FALSE: The main difference between the Classic and Enhanced setups of the ECAM is that, in the Enhanced system, the DMC 2 supplies both ECAM displays, and DMC 1 and 3 acts as a backup. On the other hand, in the Classic system, the upper ECAM display is supplied by DMC 1, and the lower ECAM display is supplied by the DMC 2, which leaves the DMC 3 as the singular backup.

This is the heart of the ECAM system, which receives data from the AIRCRAFT systems to generate red warnings, and the SDACs to generate amber cautions.

The upper part of the EWD is used for?

The FAP is located in/at

The Cabin lights are normally operated at the

When the emergency escape slide is deployed, which emergency lights turn on automatically?

To provide sufficient lighting of the aisle, exits and emergency exits, lights are installed on _ side/s.

The Exterior Lights comes on _ whenever the escape slide is deployed

The lights are supplied from the _

Emergency Lights are installed in the cabin and on the _

The enhanced forward attendant panel is known as the

The Programming and Testing Panel has been removed since:

Cabin Emergency Lights are located on the

In the enhanced CIDS, how many directors are there?

Among the choices, which one is not included in the enhanced CIDS?

In what format are the CAM, OBRM, and PRAM integrated within enhanced FAP?

In the cids, it converts analog to digital and digital to analog for the directors and from the directors respectively?

Enhanced FAP means..

Which of the following is included in the cabin lights controlled by CIDS?

Where is the FAP located?

In the CIDS, the PTP is located where?