54806217 Airbus CBTquiz1

8/21/2019 54806217 Airbus CBTquiz1

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8/21/2019 54806217 Airbus CBTquiz1


To decrease the cabin temperature.To decrease the cabin temperature.

To decrease the HOT AIR demand fromTo decrease the HOT AIR demand from

the engine bleeds.the engine bleeds.

With only a few passengers on the aircraft, the

pack flow control selector should be set to LO:

With only a few passengers on the aircraft, theWith only a few passengers on the aircraft, the

pack flow control selector should be set to LO:pack flow control selector should be set to LO:

To decrease the BLEED AIR demand fromTo decrease the BLEED AIR demand from

the engines and therefore to save fuel.the engines and therefore to save fuel.

To decrease the BLEED AIR demand fromTo decrease the BLEED AIR demand from

the APU.the APU.

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Temperature regulation is completely lost.Temperature regulation is completely lost.

Have a look at the ECAM “COND” page : “ALTN

MODE” is displayed.What happened?

Have a look at the ECAMHave a look at the ECAM ““CONDCOND”” page :page : ““ALTNALTN

MODEMODE”” is displayed.is displayed.

What happened?What happened?

Channel 1 of ZONE CONTROLLER hasChannel 1 of ZONE CONTROLLER has

failed and the pilot has closed the HOTfailed and the pilot has closed the HOT

AIR and TRIM AIR valves.AIR and TRIM AIR valves.

Channel 1 of ZONE CONTROLLER hasChannel 1 of ZONE CONTROLLER has

failed and channel 2 has taken over, thusfailed and channel 2 has taken over, thus

the HOT AIR and TRIM AIR valves havethe HOT AIR and TRIM AIR valves have

closed automatically.closed automatically.

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Looking at the ECAM BLEED page and AIR CONDoverhead panel, what can be concluded?

Looking at the ECAM BLEED page and AIR CONDLooking at the ECAM BLEED page and AIR COND

overhead panel, what can be concluded?overhead panel, what can be concluded?

The RAM AIR inlet has been opened.The RAM AIR inlet has been opened.

On the ECAM SD, the RAM AIR inlet valveOn the ECAM SD, the RAM AIR inlet valve

should be amber if it is fully open in flight.should be amber if it is fully open in flight.

Aircraft is depressurized, but after theAircraft is depressurized, but after the

RAM AIR valve opens at least one packRAM AIR valve opens at least one pack

should be pressurized again.should be pressurized again.

Aircraft is depressurized, but the XAircraft is depressurized, but the X

BLEED valve should be open since bothBLEED valve should be open since both

engines are running.engines are running.

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To HI, in order to help reduce the cabinTo HI, in order to help reduce the cabin

temperature.temperature.

To HI and cockpit TEMP SELECTOR toTo HI and cockpit TEMP SELECTOR to

HOT in order to have maximum coolingHOT in order to have maximum cooling

air to the cabin.air to the cabin.

During taxi, with a full load of passengers and in a

high temperature area, how should the pack flow

be set?

During taxi, with a full load of passengers and in aDuring taxi, with a full load of passengers and in a

high temperature area, how should the pack flowhigh temperature area, how should the pack flow

be set?be set?

To LO, in order to minimize the amount ofTo LO, in order to minimize the amount of

hot air sent to the cabin zones.hot air sent to the cabin zones.

To NORM, as the system is fully automaticTo NORM, as the system is fully automatic

apart from temperature settings.apart from temperature settings.

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To regulate the hot air pressure.To regulate the hot air pressure.

To regulate the pack outlet pressure toTo regulate the pack outlet pressure to

each zone.each zone.

In the AIR COND system what is the function of theTRIM AIR valve?

In the AIR COND system what is the function of theIn the AIR COND system what is the function of the

TRIM AIR valve?TRIM AIR valve?

To optimize the zone temperature byTo optimize the zone temperature by

adding cold air.adding cold air.

To optimize the zone temperature byTo optimize the zone temperature by

adding hot air.adding hot air.

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For the Normal Operation of the CARGO CONDSYSTEM :

For the Normal Operation of the CARGO CONDFor the Normal Operation of the CARGO COND

SYSTEM :SYSTEM :

The pilot ensures that there are no lightsThe pilot ensures that there are no lights

illuminated on theilluminated on the pbpb swsw and that theand that the

temperature is set as required.temperature is set as required.

The system display will be found on theThe system display will be found on the

ECAM BLEED page.ECAM BLEED page.

The pilot has no control of the systemThe pilot has no control of the system


The system display will be found on theThe system display will be found on the

ECAM PRESS page.ECAM PRESS page.

Aft

Cargo

Ventilation

Controller

Forward

Cargo

Ventilation

Controller

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Which of the following statements is correct?Which of the following statements is correct?Which of the following statements is correct?

Crew should SWITCH OFF both packs justCrew should SWITCH OFF both packs just

before engines start.before engines start.

Crew should SWITCH OFF both engineCrew should SWITCH OFF both engine

bleed valves just before engine start.bleed valves just before engine start.

During engine start, all the currentDuring engine start, all the current

indications on ECAM BLEED page andindications on ECAM BLEED page and

COND overhead panel are correct.COND overhead panel are correct.

Crew should select X bleed valve selectorCrew should select X bleed valve selector

to SHUT position to pressurize the leftto SHUT position to pressurize the left

side first.side first.

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The X BLEED should have remainedThe X BLEED should have remained

open.open.

All the indications are correct.All the indications are correct.

The crew should set X BLEED valveThe crew should set X BLEED valve

selector to SHUT position.selector to SHUT position.

The ENGINE H.P valve must be closedThe ENGINE H.P valve must be closed

with the engine at idle power.with the engine at idle power.

Both engines are running and the APU bleed has

been switched OFF.

Which statement is correct?

Both engines are running and the APU bleed hasBoth engines are running and the APU bleed has

been switched OFF.been switched OFF.

Which statement is correct?Which statement is correct?

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If the PACK FLOW CONTROL valves close, what

will be the subsequent position of the TRIM AIR

valves and the HOT AIR valve?

If the PACK FLOW CONTROL valves close, whatIf the PACK FLOW CONTROL valves close, what

will be the subsequent position of the TRIM AIRwill be the subsequent position of the TRIM AIR

valves and the HOT AIR valve?valves and the HOT AIR valve?

-- The TRIM AIR valves remain open.The TRIM AIR valves remain open.

-- The HOT AIR valve closes.The HOT AIR valve closes.

-- The TRIM AIR valves remain open.The TRIM AIR valves remain open.

-- The HOT AIR valve remains open.The HOT AIR valve remains open.

-- The TRIM AIR valves close.The TRIM AIR valves close.

-- The HOT AIR valve remains openThe HOT AIR valve remains open

-- The TRIM AIR valves close.The TRIM AIR valves close.

-- The HOT AIR valve closes.The HOT AIR valve closes.

Hot Air

Valve

Hot Air

Valve

Hot

Bleed Air

HOT

AIR

Mixing Unit

Pack

1

Pack

2

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The lower value is the temperature of theThe lower value is the temperature of the

air entering a zone (DUCT INLETair entering a zone (DUCT INLET

temperature). The upper value is thetemperature). The upper value is the

actual zone temperature monitored by theactual zone temperature monitored by thezone control computer.zone control computer.

Have a look at the ECAM “COND” page. Why are

two different temperature values displayed for each

zone of the aircraft?

Have a look at the ECAMHave a look at the ECAM ““CONDCOND”” page. Why arepage. Why are

two different temperature values displayed for eachtwo different temperature values displayed for each

zone of the aircraft?zone of the aircraft?

The lower value is the pack outletThe lower value is the pack outlet

temperature. The upper value is the actualtemperature. The upper value is the actual

zone temperature monitored by the zonezone temperature monitored by the zone

control temperature.control temperature.

The lower value is the temperature of theThe lower value is the temperature of the

air controlled by the HOT AIR valve. Theair controlled by the HOT AIR valve. The

upper value is the pack outlet airupper value is the pack outlet air


The lower value is the actual zoneThe lower value is the actual zone

temperature. The upper value is thetemperature. The upper value is the

selected zone temperature.selected zone temperature.

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Accelerating the cabin zonesAccelerating the cabin zones

pressurization.pressurization.

Accelerating the removal of cabin smoke.Accelerating the removal of cabin smoke.

What is the function of the CABIN AIR FANS?What is the function of the CABIN AIR FANS?What is the function of the CABIN AIR FANS?

Extracting air from the AVIONICS BAY.Extracting air from the AVIONICS BAY.

Reducing the BLEED AIR requirement andReducing the BLEED AIR requirement and

therefore saving fuel.therefore saving fuel.

HOT

AIR

Mixing Unit

Pack

1

Pack

2 Cabin

Fan

Cabin

FanCabin

Fan

Cabin

Fan

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To provide backup pressure if the cabinTo provide backup pressure if the cabin

pressure controllers should fail.pressure controllers should fail.

In the CABIN PRESSURIZATION system, thefunction of the safety valves is...

In the CABIN PRESSURIZATION system, theIn the CABIN PRESSURIZATION system, the

function of the safety valves is...function of the safety valves is...

Monitor the function of the outflow valve.Monitor the function of the outflow valve.

Protect against excessive cabin altitude.Protect against excessive cabin altitude.

Protect against excessive differentialProtect against excessive differential

pressure.pressure.

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Yes, SYS1 is still controlling the cabin Yes, SYS1 is still controlling the cabin

altitude through the safetyaltitude through the safety valvevalve..

No, in this case the cabin altitude has toNo, in this case the cabin altitude has to

be controlled throughbe controlled through the LDG ELEVthe LDG ELEV

selector.selector.

On the CABIN PRESS panel with a LDG ELEV set

manually, is there still an automatic control of the

cabin altitude?

On the CABIN PRESS panel with a LDG ELEV setOn the CABIN PRESS panel with a LDG ELEV set

manually, is there still an automatic control of themanually, is there still an automatic control of the

cabin altitude?cabin altitude?

No, in this case the cabin altitude has toNo, in this case the cabin altitude has to

be controlled through the MAN V/S CTL.be controlled through the MAN V/S CTL.

Yes, SYS1 is still controlling the cabin Yes, SYS1 is still controlling the cabin

altitude through thealtitude through the outflowoutflow valve.valve.

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7.67.6 psipsi

8.68.6 psipsi

In the CABIN PRESSURIZATION system, what is themaximum allowable differential pressure?

In the CABIN PRESSURIZATION system, what is theIn the CABIN PRESSURIZATION system, what is the

maximum allowable differential pressure?maximum allowable differential pressure?

5.35.3 psipsi

6.96.9 psipsi

??

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1.01.0 psipsi

8.68.6 psipsi

Regarding the CABIN PRESSURIZATION system,

what should the differential pressure be on the

ground, while at the gate?

Regarding the CABIN PRESSURIZATION system,Regarding the CABIN PRESSURIZATION system,

what should the differential pressure be on thewhat should the differential pressure be on the

ground, while at the gate?ground, while at the gate?

00 psipsi

0.50.5 psipsi

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Are controlled with the DITCHINGAre controlled with the DITCHING pbpb..

Can not be controlled manually and areCan not be controlled manually and are

fully automatic.fully automatic.

On the CABIN PRESSURIZATION system, thesafety valves….

On the CABIN PRESSURIZATION system, theOn the CABIN PRESSURIZATION system, the

safety valvessafety valves……..

Are controlled with the MAN V/S CTL.Are controlled with the MAN V/S CTL.

Are controlled with the MODE SELAre controlled with the MODE SEL pbpb..

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600 ft.600 ft.

6000 ft.6000 ft.

On the CABIN PRESS panel, the LDG ELEV has

been set manually.

What is the approximate value ?

On the CABIN PRESS panel, the LDG ELEV hasOn the CABIN PRESS panel, the LDG ELEV has

been set manually.been set manually.

What is the approximate value ?What is the approximate value ?

6 ft.6 ft.

60 ft.60 ft.

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The air outlet valve.The air outlet valve.

The safety valve.The safety valve.

On the CABIN PRESS panel, pushing on the MODESEL pb sw gives control over

On the CABIN PRESS panel, pushing on the MODEOn the CABIN PRESS panel, pushing on the MODE

SELSEL pbpb swsw gives control over gives control over

The outflow valve.The outflow valve.

The air intake valve.The air intake valve.

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5900 ft.5900 ft.

6500 ft.6500 ft.

On the ECAM STATUS page, as you can see cabin

pressure control is manual. You want descend from

FL 390 to FL 330. What is your target CABIN ATL?

On the ECAM STATUS page, as you can see cabinOn the ECAM STATUS page, as you can see cabin

pressure control is manual. You want descend frompressure control is manual. You want descend from

FL 390 to FL 330. What is your target CABIN ATL?FL 390 to FL 330. What is your target CABIN ATL?

0 ft.0 ft.

5000 ft.5000 ft.

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Closes, the cabin altitude raises.Closes, the cabin altitude raises.

Closes, the cabin altitude drops.Closes, the cabin altitude drops.

On the CABIN PRESS panel, with the MODE SEL set

to MAN and the MAN V/S CTL held in the DN

position, the outflow valve...

On the CABIN PRESS panel, with the MODE SEL setOn the CABIN PRESS panel, with the MODE SEL set

to MAN and the MAN V/S CTL held in the DNto MAN and the MAN V/S CTL held in the DN

position, the outflow valve...position, the outflow valve...

Opens, the cabin altitude raises.Opens, the cabin altitude raises.

Opens, the cabin altitude drops.Opens, the cabin altitude drops.

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What ventilation configuration is displayed on theCAB PRESS page?

What ventilation configuration is displayed on theWhat ventilation configuration is displayed on the

CAB PRESS page?CAB PRESS page?

Open configuration (a/c on ground).Open configuration (a/c on ground).

Closed configuration (a/c in flight).Closed configuration (a/c in flight).

Intermediate configuration (a/c in flight,Intermediate configuration (a/c in flight,

high skin temperature).high skin temperature).

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What ventilation configuration is displayed on theCAB PRESS page?

What ventilation configuration is displayed on theWhat ventilation configuration is displayed on the

CAB PRESS page?CAB PRESS page?

Open configuration (a/c on ground).Open configuration (a/c on ground).

Closed configuration (a/c in flight).Closed configuration (a/c in flight).

Intermediate configuration (a/c in flight,Intermediate configuration (a/c in flight,

high temperature).high temperature).

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Please indicate the position of the VENTILATIONpanel.

Please indicate the position of the VENTILATIONPlease indicate the position of the VENTILATION

panel.panel.

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Please indicate the ECAM E/WD screen.Please indicate the ECAM E/WD screen.Please indicate the ECAM E/WD screen.

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It is an indication that the aircraft has notIt is an indication that the aircraft has not

yet reached the shutdown status.yet reached the shutdown status.

It is an indication that at least one systemIt is an indication that at least one system

requires crew attention.requires crew attention.

It is an indication that there is at least oneIt is an indication that there is at least one

inoperative system in the STS.inoperative system in the STS.

It is an indication that an aircraft systemIt is an indication that an aircraft system

requires maintenance attention.requires maintenance attention.

On the ECAM E/WD page, after the engine

shutdown, you observe a pulsing STS message.

What does it mean?

On the ECAM E/WD page, after the engineOn the ECAM E/WD page, after the engine

shutdown, you observe a pulsing STS message.shutdown, you observe a pulsing STS message.

What does it mean?What does it mean?

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Press and hold the corresponding buttonPress and hold the corresponding button

on the ECP.on the ECP.

Switch the SD to one of the NDSwitch the SD to one of the ND’’s.s.

Switch the SD to one of theSwitch the SD to one of the PFDPFD’’ss..

The upper ECAM DU failed. To see the differentsystem pages on the lower DU, you have to:

The upper ECAM DU failed. To see the differentThe upper ECAM DU failed. To see the different

system pages on the lower DU, you have to:system pages on the lower DU, you have to:

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The E/WD is automatically transferred toThe E/WD is automatically transferred to

one of the NDone of the ND’’s.s.

The E/WD is automatically transferred toThe E/WD is automatically transferred to

one of theone of the PFDPFD’’ss..

To get E/WD information, it must beTo get E/WD information, it must be

manually transferred to one of the NDmanually transferred to one of the ND’’s.s.

To get E/WD information, it must beTo get E/WD information, it must be

manually transferred to one of themanually transferred to one of the PFDPFD’’ss..

Both ECAM screens failed. What happens to theE/WD indication?

Both ECAM screens failed. What happens to theBoth ECAM screens failed. What happens to the

E/WD indication?E/WD indication?

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Only ECAM cautions are lost.Only ECAM cautions are lost.

ECAM cautions and warnings and auralECAM cautions and warnings and aural

warnings are lost.warnings are lost.

MASTER CAUTION light, MASTERMASTER CAUTION light, MASTER

WARNING light and aural warnings areWARNING light and aural warnings are

lost.lost.

MASTER CAUTION light, MASTERMASTER CAUTION light, MASTER

WARNING light, aural warnings andWARNING light, aural warnings and

ECAM cautions and warnings are lost.ECAM cautions and warnings are lost.

On the ECAM SYSTEM in case of a double FWCfailure...

On the ECAM SYSTEM in case of a double FWCOn the ECAM SYSTEM in case of a double FWC

failure...failure...

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The failure message has been previouslyThe failure message has been previously

cancelled with the EMER CANCcancelled with the EMER CANC pbpb..

The failure message had occurred duringThe failure message had occurred during

the previous flight.the previous flight.

The FWC is working in a degraded modeThe FWC is working in a degraded mode

and is not able anymore to detect thisand is not able anymore to detect this

failure.failure.

Because it was a false warning,Because it was a false warning,

maintenance inhibited it.maintenance inhibited it.

On the ECAM STATUS page , what does aCANCELLED CAUTION mean?

On the ECAM STATUS page , what does aOn the ECAM STATUS page , what does a

CANCELLED CAUTION mean?CANCELLED CAUTION mean?

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By resetting the appropriate circuitBy resetting the appropriate circuit

breaker.breaker.

By pressing and holding any CLRBy pressing and holding any CLR pbpb for for

more than 3 seconds.more than 3 seconds.

Only maintenance can reset this function.Only maintenance can reset this function.

By pressing and holding the RCLBy pressing and holding the RCL pbpb forfor

more than 3 seconds.more than 3 seconds.

On the ECAM STATUS page, how can you removethe CANCELLED CAUTION message?

On the ECAM STATUS page, how can you removeOn the ECAM STATUS page, how can you remove

the CANCELLED CAUTION message?the CANCELLED CAUTION message?

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The location of the DFDR (Digital Flight DataRecorder) is :

The location of the DFDR (Digital Flight DataThe location of the DFDR (Digital Flight Data

Recorder) is :Recorder) is :

Inside the Cockpit.Inside the Cockpit.

Installed in the tail Section of the aircraft,Installed in the tail Section of the aircraft,

and the data is stored on a tapeand the data is stored on a tape

Contained in fire and shock proof box.Contained in fire and shock proof box.

In the passenger Cabin for protectionIn the passenger Cabin for protection

reason.reason.

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When is the DFDR automatically energized?When is the DFDR automatically energized?When is the DFDR automatically energized?

The DFDR will be only energized after theThe DFDR will be only energized after the

first engine start.first engine start.

The DFDR is energized during 5 minutesThe DFDR is energized during 5 minutes

and then after the first engine start.and then after the first engine start.

The DFDR will be energized at lift off.The DFDR will be energized at lift off.

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When aircraft lighting is selected OFF.When aircraft lighting is selected OFF.

When the GND CTL pb sw light is illuminated blue,it will be automatically extinguished :

When the GND CTL pbWhen the GND CTL pb swsw light is illuminated blue,light is illuminated blue,

it will be automatically extinguished :it will be automatically extinguished :

On landing.On landing.

After first engine start.After first engine start.

When both engines are started.When both engines are started.

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On the pedestal the DFDR EVENT pb can be used tomark an event on the DFDR tape.

On the pedestal the DFDR EVENT pb can be used toOn the pedestal the DFDR EVENT pb can be used to

mark an event on the DFDR tape.mark an event on the DFDR tape.

False.False.

True.True.

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When a DFDR fault occurs, it will be signaled by :When a DFDR fault occurs, it will be signaled by :When a DFDR fault occurs, it will be signaled by :

A fault light illuminating amber onA fault light illuminating amber on

overhead panel.overhead panel.

An ECAM caution message.An ECAM caution message.

A low frequency signal sounds throughA low frequency signal sounds through

the cockpit loud speaker.the cockpit loud speaker.

A MAINTENANCE message in the statusA MAINTENANCE message in the status

page.page.

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Please indicate the PFD.Please indicate the PFD.Please indicate the PFD.

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Please indicate the SD.Please indicate the SD.Please indicate the SD.

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Please indicate the ND 2.Please indicate the ND 2.Please indicate the ND 2.

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Red.Red.

Amber.Amber.

Green.Green.

White.White.

Color coding on the ECAM screens: which colorindicates that crew awareness is required?

Color coding on the ECAM screens: which colorColor coding on the ECAM screens: which color

indicates that crew awareness is required?indicates that crew awareness is required?

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Red.Red.

Amber.Amber.

Green.Green.

White.White.

Color coding on the ECAM screens: which colorindicates that there is immediate action required?


indicates that there is immediate action required?indicates that there is immediate action required?

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Red.Red.

Amber.Amber.

Green.Green.

White.White.

Color coding on the ECAM screens: which colorindicates a normal condition?


indicates a normal condition?indicates a normal condition?

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On the ECAM SD page, what does an advisorymessage mean?

On the ECAM SD page, what does an advisoryOn the ECAM SD page, what does an advisory

message mean?message mean?

The parameter is about to reach a limit.The parameter is about to reach a limit.

The parameter is out ofThe parameter is out of limitslimits..

The parameter has a faulty indication.The parameter has a faulty indication.

1.1 5.1

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You have an ENG 1 FIRE warning. On the ECAM

E/WD page, what does the green arrow at the

bottom of the page mean?

You have an ENG 1 FIRE warning. On the ECAM You have an ENG 1 FIRE warning. On the ECAM

E/WD page, what does the green arrow at theE/WD page, what does the green arrow at the

bottom of the page mean?bottom of the page mean?

It indicates that there is aIt indicates that there is a STSSTS pagepage

behind.behind.

It indicates that there is a system pageIt indicates that there is a system page

behind.behind.

It means that there is more informationIt means that there is more information

to be seen.to be seen.

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On the ECAM ENGINE system page, you observe

the VIB (N2) indication. What is the name of such an

indication pulsing?

On the ECAM ENGINE system page, you observeOn the ECAM ENGINE system page, you observe

the VIB (N2) indication. What is the name of such anthe VIB (N2) indication. What is the name of such an

indication pulsing?indication pulsing?

Alert.Alert.

Warning.Warning.

Caution.Caution.

Advisory.Advisory.

1.1 5.1

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On the PFD, what is the actual speed?On the PFD, what is the actual speed?On the PFD, what is the actual speed?

150150 ktkt..

160160 ktkt..

169169 ktkt..

185185 ktkt..

140

160

180

200

F

120

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In flight with the following display on the PFDspeed scale, which statement is correct?

In flight with the following display on the PFDIn flight with the following display on the PFD

speed scale, which statement is correct?speed scale, which statement is correct?

The present speed is 250The present speed is 250 ktskts selected byselected by

the crew and the MAX speed for loweringthe crew and the MAX speed for lowering

landing gear is VLE 230landing gear is VLE 230 ktskts..

The aircraftThe aircraft’’s speed is 250s speed is 250 ktskts which is awhich is amanaged speed. The symbol at 230managed speed. The symbol at 230 ktskts

represents the VFE corresponding to therepresents the VFE corresponding to the

next flap lever position.next flap lever position.

The present speed of 250The present speed of 250 ktskts is selectedis selected

by the crew. The circle at the bottom ofby the crew. The circle at the bottom of

the scale represents green dot speedthe scale represents green dot speed

which is the engine out operating speedwhich is the engine out operating speed

in clean configuration.in clean configuration.

The = symbol at 230The = symbol at 230 ktskts represents arepresents a

speed constraint. The circle on thespeed constraint. The circle on the

bottom represents green dot speed whichbottom represents green dot speed which

is the holding speed.is the holding speed.

220

240

260

280

=

o

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On the PFD, the magenta symbols on the speed

scale represent:

On the PFD, the magenta symbols on the speedOn the PFD, the magenta symbols on the speed

scale represent:scale represent:

The ECON speed range during managedThe ECON speed range during managed

descent.descent.

The managed speed by the FMGS duringThe managed speed by the FMGS during

managed climb.managed climb.

The upper magenta for high speedThe upper magenta for high speed

protection, the lower for turbulenceprotection, the lower for turbulence

operating speed.operating speed.

The lower magenta symbol representsThe lower magenta symbol represents

VLS.VLS..636

300

320

340

360

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Is it possible to change the baro reference display

from Hecto Pascals to inches of mercury and vice

versa?

Is it possible to change theIs it possible to change the barobaro reference displayreference display

fromfrom HectoHecto PascalsPascals to inches of mercury and viceto inches of mercury and vice

versa?versa?

No, it is not possible because each airlineNo, it is not possible because each airline

has its own configuration.has its own configuration.

Yes, by rotating the outer scale of Yes, by rotating the outer scale of barobaro

reference selector on the EFIS panel.reference selector on the EFIS panel.

No, the crew should refer to a conversionNo, the crew should refer to a conversion

table.table.

Yes, but only the Captain side is equipped Yes, but only the Captain side is equipped

with this conversion.with this conversion.

1020

8/21/2019 54806217 Airbus CBTquiz1


On the PFD altimeter scale, which statement iscorrect ?

On the PFD altimeter scale, which statement isOn the PFD altimeter scale, which statement is

correct ?correct ?

The crew is pushing theThe crew is pushing the barobaro referencereference

selector to change from STD setting toselector to change from STD setting to

local QNH.local QNH.

Crew is pushing theCrew is pushing the barobaro referencereference

selector to change from local QNH to theselector to change from local QNH to the

STD setting.STD setting.

The rate of descent is 240 FPM.The rate of descent is 240 FPM.

Aircraft passing altitude is 8500 ft.Aircraft passing altitude is 8500 ft.

STD

FL 70

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the maximum speed for thepresent configuration?

On the PFD, what is the maximum speed for theOn the PFD, what is the maximum speed for the

present configuration?present configuration?

180180 ktkt..

191191 ktkt..

215215 ktkt..

250250 ktkt..

140

160

180

250

220

S

200

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the maximum speed to selectthe next flap setting?

On the PFD, what is the maximum speed to selectOn the PFD, what is the maximum speed to select

the next flap setting?the next flap setting?

140140 ktkt..

155155 ktkt..

175175 ktkt..

185185 ktkt..

140

160

180

200

=

F

120

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the meaning of the blue ribbonon the altitude scale?

On the PFD, what is the meaning of the blue ribbonOn the PFD, what is the meaning of the blue ribbon

on the altitude scale?on the altitude scale?

It marks the landing elevation.It marks the landing elevation.

It marks the selected altitude.It marks the selected altitude.

It marks theIt marks the preselectedpreselected altitude.altitude.

It marks the decision height.It marks the decision height.

STD

FL 7030.08QNH

7000

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the actual vertical speed?On the PFD, what is the actual vertical speed?On the PFD, what is the actual vertical speed?

80 ft/min in climb.80 ft/min in climb.

800 ft/min in descent.800 ft/min in descent.

80 ft/min in descent.80 ft/min in descent.

800 ft/min in climb.800 ft/min in climb.

STD

FL 70

30.08QNH

7000

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the actual heading?On the PFD, what is the actual heading?On the PFD, what is the actual heading?

069.069.

080.080.

084.084.

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the selected heading?On the PFD, what is the selected heading?On the PFD, what is the selected heading?

069.069.

080.080.

084.084.

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, what is the actual aircraft track?On the PFD, what is the actual aircraft track?On the PFD, what is the actual aircraft track?

069.069.

080.080.

084.084.

8/21/2019 54806217 Airbus CBTquiz1


On the PFD, which of the following statements istrue?

On the PFD, which of the following statements isOn the PFD, which of the following statements is

true?true?

The aircraft is in a climb, drifting to theThe aircraft is in a climb, drifting to the

left.left.

The aircraft is in a climb, drifting to theThe aircraft is in a climb, drifting to the

right.right.

The aircraft is in a descent, drifting to theThe aircraft is in a descent, drifting to the

left.left.

The aircraft is in a descent, drifting to theThe aircraft is in a descent, drifting to the

right.right.

8/21/2019 54806217 Airbus CBTquiz1


On the ND, which of the following statements istrue?

On the ND, which of the following statements isOn the ND, which of the following statements is

true?true?

The heading to the next waypoint PAS isThe heading to the next waypoint PAS is

108, it is at 28 NM, time left to the108, it is at 28 NM, time left to the

waypoint is 9 minutes and 8 seconds.waypoint is 9 minutes and 8 seconds.

The heading to the next waypoint PAS isThe heading to the next waypoint PAS is

108, it is at 28 NM, time to the destination108, it is at 28 NM, time to the destination

is 9 hours and 8 minutes.is 9 hours and 8 minutes.

The track to the next waypoint PAS isThe track to the next waypoint PAS is

108, it is at 28 NM, elapsed time of this108, it is at 28 NM, elapsed time of this

flight is 9 minutes and 8 seconds.flight is 9 minutes and 8 seconds.

The track to the next waypoint PAS isThe track to the next waypoint PAS is

108, it is at 28 NM, it will be108, it is at 28 NM, it will be overflownoverflown atat

9:08.9:08.

8/21/2019 54806217 Airbus CBTquiz1


ATC cleared you to FL 150. The PF sets the new

altitude on the FCU. What will happen if he pulls the

ALT selection knob?

ATC cleared you to FL 150. The PF sets the newATC cleared you to FL 150. The PF sets the new

altitude on the FCU. What will happen if he pulls thealtitude on the FCU. What will happen if he pulls the

ALT selection knob?ALT selection knob?

The aircraft will stop the climb at FL 60The aircraft will stop the climb at FL 60

until passing the constraint then continueuntil passing the constraint then continue

climb to FL 150.climb to FL 150.

The aircraft will disregard theThe aircraft will disregard the constraintconstraint

and climb to FL 150.and climb to FL 150.

As soon as the aircraft passes FL 60, theAs soon as the aircraft passes FL 60, the

target altitude on the PFD will change totarget altitude on the PFD will change to

FL 150 and the aircraft continues to climb.FL 150 and the aircraft continues to climb.

The aircraft will level off at FL 60. The PFThe aircraft will level off at FL 60. The PF

must pull the ALT selection knob amust pull the ALT selection knob a

second time to climb to FL 150.second time to climb to FL 150.

8/21/2019 54806217 Airbus CBTquiz1


The FCU target altitude is FL 150, you are climbing

toward an ALT constraint.

What will happen if the PF pushes the ALT

selection knob?

NOTE: The constraint alt is FL60.

The FCU target altitude is FL 150, you are climbingThe FCU target altitude is FL 150, you are climbing

toward an ALT constraint.toward an ALT constraint.

What will happen if the PF pushes the ALTWhat will happen if the PF pushes the ALT

selection knob?selection knob?

NOTE: The constraint alt is FL60.NOTE: The constraint alt is FL60.

The aircraft will level off at FL 60. The PFThe aircraft will level off at FL 60. The PF

must push or pull the ALT selection knobmust push or pull the ALT selection knob

a second time to climb to FL 150.a second time to climb to FL 150.

The aircraft will disregard theThe aircraft will disregard the constraintconstraint

and climb to FL 150.and climb to FL 150.

As soon as the aircraft passes FL 60, theAs soon as the aircraft passes FL 60, the

target on the PFD will change to FL 150target on the PFD will change to FL 150

and the aircraft continues to climb.and the aircraft continues to climb.

No change, the aircraft will stop the climbNo change, the aircraft will stop the climb

at FL 60 until passing the constraint thenat FL 60 until passing the constraint then

continue climb to FL 150.continue climb to FL 150.

8/21/2019 54806217 Airbus CBTquiz1


The FCU target altitude is FL 150, you are climbing

toward an ALT constraint.What will happen if the PF pulls the HDG/TRK

selection knob now?

The FCU target altitude is FL 150, you are climbingThe FCU target altitude is FL 150, you are climbing

toward an ALT constraint.toward an ALT constraint.

What will happen if the PF pulls the HDG/TRKWhat will happen if the PF pulls the HDG/TRK

selection knob now?selection knob now?

The aircraft will continue on the presentThe aircraft will continue on the present

heading, stop the climb at FL 60.heading, stop the climb at FL 60.

The aircraft will stay on the presentThe aircraft will stay on the present

heading, disregard the constraint andheading, disregard the constraint and

climb to FL 150.climb to FL 150.

The aircraft will follow the FThe aircraft will follow the F--PLN, stop thePLN, stop the

climb at FL 60 until passing the constraintclimb at FL 60 until passing the constraint

then continue climb to FL 150.then continue climb to FL 150.

The aircraft will follow the FThe aircraft will follow the F--PLN,PLN,

disregard the constraint and climb todisregard the constraint and climb to

FL 150.FL 150.

8/21/2019 54806217 Airbus CBTquiz1


On the MCDU, you notice that some waypoints have

a small triangle behind the name. What does it

stand for?

On the MCDU, you notice that some waypoints haveOn the MCDU, you notice that some waypoints have

a small triangle behind the name. What does ita small triangle behind the name. What does it

stand for?stand for?

It means these waypoints will beIt means these waypoints will be

overflownoverflown..

It means these waypoints are compulsoryIt means these waypoints are compulsory

reporting points.reporting points.

It indicates altitude constraints at theseIt indicates altitude constraints at these

waypoints.waypoints.

It indicates speed constraints at theseIt indicates speed constraints at these

waypoints.waypoints.

8/21/2019 54806217 Airbus CBTquiz1


You get the message DECCELERATE on the FMA.What does it mean?

You get the message DECCELERATE on the FMA. You get the message DECCELERATE on the FMA.


The FMGC warns you about a possibleThe FMGC warns you about a possible

overspeedoverspeed..

TCAS discovered a possible trafficTCAS discovered a possible traffic

conflict and warns you to decelerate toconflict and warns you to decelerate to

keep your separation.keep your separation.

Due to some environmentalDue to some environmental

circumstances, the aircraft missed acircumstances, the aircraft missed a

speed constraint.speed constraint.

You are advised to slow the aircraft to You are advised to slow the aircraft to

loose energy so that you will be able toloose energy so that you will be able to

intercept the descent path.intercept the descent path.

8/21/2019 54806217 Airbus CBTquiz1


The a/c is climbing to FL250 as set on the FCU, an

altitude constraint has been inserted at FL90.

What is the procedure when the a/c reaches FL90?

The a/c is climbing to FL250 as set on the FCU, anThe a/c is climbing to FL250 as set on the FCU, an

altitude constraint has been inserted at FL90.altitude constraint has been inserted at FL90.

What is the procedure when the a/c reaches FL90?What is the procedure when the a/c reaches FL90?

The pilot flying must push the ALT knob.The pilot flying must push the ALT knob.

The pilot flying must turn the ALT knob.The pilot flying must turn the ALT knob.

No procedure, the a/c will automaticallyNo procedure, the a/c will automatically

resume the climb after having sequencedresume the climb after having sequenced

the constrained waypoint.the constrained waypoint.

The a/c will not match the constraint, theThe a/c will not match the constraint, the

pilot has to climb by using V/S mode.pilot has to climb by using V/S mode.

8/21/2019 54806217 Airbus CBTquiz1


In dual mode of operation, one FMGC is the master.How is the master FMGC determined ?

In dual mode of operation, one FMGC is the master.In dual mode of operation, one FMGC is the master.

How is the master FMGC determined ?How is the master FMGC determined ?

It is the FMGC corresponding to the APIt is the FMGC corresponding to the AP

engaged or FMGC1 when both APengaged or FMGC1 when both AP

engaged.engaged.

Randomly at power up.Randomly at power up.

It is the FMGC corresponding to the PilotIt is the FMGC corresponding to the Pilot

Flying side.Flying side.

It is always FMGC1.It is always FMGC1.

8/21/2019 54806217 Airbus CBTquiz1


The autothrust system has two channels. Which

FMGC controls the A/THR (both FMGCs being

operative)?

TheThe autothrustautothrust system has two channels. Whichsystem has two channels. Which

FMGC controls the A/THR (bothFMGC controls the A/THR (both FMGCsFMGCs beingbeing

operative)?operative)?

The FMGC1.The FMGC1.

The FMGC2.The FMGC2.

The randomly chosen FMGC.The randomly chosen FMGC.

8/21/2019 54806217 Airbus CBTquiz1


Setting the thrust levers to TOGA will arm the

A/THR.

Where do you check that the A/THR is armed?

Setting the thrust levers to TOGA will arm theSetting the thrust levers to TOGA will arm the

A/THR.A/THR.

Where do you check that the A/THR is armed?Where do you check that the A/THR is armed?

On the FMA, in theOn the FMA, in the AutothrustAutothrust modemode

column.column.

On the FMA, in the AP/FD and A/THROn the FMA, in the AP/FD and A/THR

engagement status column.engagement status column.

On the thrust levers FLEX detent.On the thrust levers FLEX detent.

On the MCDU takeoff page.On the MCDU takeoff page.

8/21/2019 54806217 Airbus CBTquiz1


Dashes in the FCU window indicate the system has

enough information to manage the settings of thetargets.

Why is the altitude window not dashed?

Dashes in the FCU window indicate the system hasDashes in the FCU window indicate the system has

enough information to manage the settings of theenough information to manage the settings of the

targets.targets.

Why is the altitude window not dashed?Why is the altitude window not dashed?

The altitude window shows digits as theThe altitude window shows digits as the

target altitude is always set manually bytarget altitude is always set manually by

the pilot.the pilot.

The altitude selector knob has not beenThe altitude selector knob has not been

pushed.pushed.

The altitude selector knob has not beenThe altitude selector knob has not been

pulled.pulled.

Both autopilots must be engaged.Both autopilots must be engaged.

8/21/2019 54806217 Airbus CBTquiz1


The speed window on the FCU is dashed. Whatdoes it mean?

The speed window on the FCU is dashed. WhatThe speed window on the FCU is dashed. What

does it mean?does it mean?

The target speed is managed by theThe target speed is managed by the

FMGC.FMGC.

A speed target is selected.A speed target is selected.

The pilot has pulled the speed selectorThe pilot has pulled the speed selector

knob.knob.

TheThe autothrustautothrust mode is speed.mode is speed.

8/21/2019 54806217 Airbus CBTquiz1


You are in managed speed mode. If you pull the

speed selector knob, which speed value will appear

on the FCU window ?

You are in managed speed mode. If you pull the You are in managed speed mode. If you pull the

speed selector knob, which speed value will appearspeed selector knob, which speed value will appear

on the FCU window ?on the FCU window ?

The max limit speed according to theThe max limit speed according to the

aircraft configuration.aircraft configuration.

VLS + 20VLS + 20 ktkt..

The current speed.The current speed.

VMO or MMO.VMO or MMO.

8/21/2019 54806217 Airbus CBTquiz1


When can you engage autopilots 1+2 at the same

time?

When can you engage autopilots 1+2 at the sameWhen can you engage autopilots 1+2 at the same

time?time?

Never.Never.

For any kind of approach.For any kind of approach.

As soon as the APPR mode is armed forAs soon as the APPR mode is armed for

an ILS approach.an ILS approach.

As soon as the APPR mode is armed for aAs soon as the APPR mode is armed for a

non precision approach on managednon precision approach on managed

mode.mode.

8/21/2019 54806217 Airbus CBTquiz1


ALT magenta is displayed on the FMA.What does it mean?

ALT magenta is displayed on the FMA.ALT magenta is displayed on the FMA.


ALT is armed and an altitude constraintALT is armed and an altitude constraint

has been inserted in the Fhas been inserted in the F--PLN.PLN.

The aircraft is on descent and the targetThe aircraft is on descent and the target

altitude is higher than the current aircraftaltitude is higher than the current aircraft

altitude.altitude.

The target altitude is above the glideThe target altitude is above the glide

slope altitude capture.slope altitude capture.

ALT is armed, the target altitude is givenALT is armed, the target altitude is given

by the ALT window in the FCU.by the ALT window in the FCU.

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of A/THR white?What is the meaning of A/THR white?What is the meaning of A/THR white?

A/THR is armed.A/THR is armed.

A/THR is disconnected.A/THR is disconnected.

A/THR is available.A/THR is available.

A/THR is active.A/THR is active.

8/21/2019 54806217 Airbus CBTquiz1


Have a look at the MCDU F-PLN page. Notice the

small white arrow shown on the right top. It

indicates that :

Have a look at the MCDU FHave a look at the MCDU F--PLN page. Notice thePLN page. Notice the

small white arrow shown on the right top. Itsmall white arrow shown on the right top. It

indicates that :indicates that :

We can move this page to the right.We can move this page to the right.

Another page is automatically displayedAnother page is automatically displayed

in relation to the phase of the flight.in relation to the phase of the flight.

Another page is available and can beAnother page is available and can be

displayed by selecting the NEXT PAGEdisplayed by selecting the NEXT PAGE

key.key.

8/21/2019 54806217 Airbus CBTquiz1


As soon as a CO RTE or a CITY PAIR is entered inthe INIT PAGE A, the displayed coordinates are:

As soon as a CO RTE or a CITY PAIR is entered inAs soon as a CO RTE or a CITY PAIR is entered in

the INIT PAGE A, the displayed coordinates are:the INIT PAGE A, the displayed coordinates are:

The runway threshold position.The runway threshold position.

The aircraft present position.The aircraft present position.

The airport reference point position.The airport reference point position.

The alternate airport positionThe alternate airport position

8/21/2019 54806217 Airbus CBTquiz1


The F-PLN page shown in the MCDU is :The FThe F--PLN page shown in the MCDU is :PLN page shown in the MCDU is :

The FThe F--PLN page A.PLN page A.

The FThe F--PLN page B.PLN page B.

8/21/2019 54806217 Airbus CBTquiz1


The standard instrument departure is shown on the

navigation display, however an amber line can be

seen:

The standard instrument departure is shown on theThe standard instrument departure is shown on the

navigation display, however an amber line can benavigation display, however an amber line can be

seen:seen:

It is the secondary FIt is the secondary F--PLN.PLN.

It is a temporary FIt is a temporary F--PLN.PLN.

It is the engine out standard instrumentIt is the engine out standard instrument

departure.departure.

It is the standard departure for lightIt is the standard departure for light

airplanes.airplanes.

8/21/2019 54806217 Airbus CBTquiz1


Have a look at the MCDU, the ILS 23R is a currentlyselected approach, the green color means:

Have a look at the MCDU, the ILS 23R is a currentlyHave a look at the MCDU, the ILS 23R is a currently

selected approach, the green color means:selected approach, the green color means:

This approach is inserted into the activeThis approach is inserted into the active

FF--PLN.PLN.

This approach is displayed in greenThis approach is displayed in green

before insertion in the Fbefore insertion in the F--PLN.PLN.

This approach can not be selected.This approach can not be selected.

8/21/2019 54806217 Airbus CBTquiz1


The ILS 23L has been selected. On the MCDU, whatis the meaning of the yellow font?

The ILS 23L has been selected. On the MCDU, whatThe ILS 23L has been selected. On the MCDU, what

is the meaning of the yellow font?is the meaning of the yellow font?

The selection has been made on theThe selection has been made on the

secondary FPLN.secondary FPLN.

This selection is definitely done andThis selection is definitely done and

cannot be erased.cannot be erased.

The selection is temporary (not yetThe selection is temporary (not yet

inserted).inserted).

The crew has made a wrong selection.The crew has made a wrong selection.

8/21/2019 54806217 Airbus CBTquiz1


To enter VIA a beacon TO a waypoint.To enter VIA a beacon TO a waypoint.

To build routes using airways.To build routes using airways.

To enter VIA/GO TO a new airport.To enter VIA/GO TO a new airport.

The lateral revision page from a F-PLN waypointshows VIA/GO TO data field, it is used:

The lateral revision page from a FThe lateral revision page from a F--PLN waypointPLN waypoint

shows VIA/GO TO data field, it is used:shows VIA/GO TO data field, it is used:

To buildTo build--up a Fup a F--PLN waypoint byPLN waypoint by

waypoint.waypoint.

8/21/2019 54806217 Airbus CBTquiz1


After engines start, which page shall be used toenter any weight modification?

After engines start, which page shall be used toAfter engines start, which page shall be used to

enter any weight modification?enter any weight modification?

The PROG page.The PROG page.

The PERF takeoff page.The PERF takeoff page.

The A/C STATUS page.The A/C STATUS page.

The FUEL PRED page.The FUEL PRED page.

8/21/2019 54806217 Airbus CBTquiz1


Have a look at the PFD, the magenta digit valuedisplayed on the top of the speed scale is:

Have a look at the PFD, the magenta digit valueHave a look at the PFD, the magenta digit value

displayed on the top of the speed scale is:displayed on the top of the speed scale is:

V2 as manually set on the FCU.V2 as manually set on the FCU.

V1.V1.

V2 as entered on the MCDU takeoff page.V2 as entered on the MCDU takeoff page.

V2 + 10.V2 + 10.

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of RWY green on the FMA ?What is the meaning of RWY green on the FMA ?What is the meaning of RWY green on the FMA ?

The lateral guidance during takeoff roll isThe lateral guidance during takeoff roll is

linked to the ILS localizer signal.linked to the ILS localizer signal.

The aircraft is automatically guided toThe aircraft is automatically guided to

maintain the runway center line.maintain the runway center line.

The runway used for takeoff is confirmedThe runway used for takeoff is confirmed

by ATC.by ATC.

8/21/2019 54806217 Airbus CBTquiz1


The FCU selected altitude is FL150, the aircraft is

climbing toward FL60 as shown on PFD.

Why is FL60 displayed in magenta?

The FCU selected altitude is FL150, the aircraft isThe FCU selected altitude is FL150, the aircraft is

climbing toward FL60 as shown on PFD.climbing toward FL60 as shown on PFD.

Why is FL60 displayed in magenta?Why is FL60 displayed in magenta?

This is an altitude constraint.This is an altitude constraint.

A speed constraint is entered.A speed constraint is entered.

The active vertical mode is not OP CLB.The active vertical mode is not OP CLB.

The aircraft rate of climb is too low.The aircraft rate of climb is too low.

8/21/2019 54806217 Airbus CBTquiz1


Have a look at the ND. What is the meaning of thehighlighted magenta symbol?

Have a look at the ND. What is the meaning of theHave a look at the ND. What is the meaning of the

highlighted magenta symbol?highlighted magenta symbol?

The aircraft is in OP CLB mode.The aircraft is in OP CLB mode.

The altitude constraint cannot beThe altitude constraint cannot be

satisfied.satisfied.

The aircraft will level off at that point toThe aircraft will level off at that point to

satisfy the altitude constraint.satisfy the altitude constraint.

The aircraft will resume the climb at thatThe aircraft will resume the climb at that

point.point.

8/21/2019 54806217 Airbus CBTquiz1


On the climb flight path, 2 engines running, the SRS

(speed reference system) provides a pitch attitude

to maintain:

On the climb flight path, 2 engines running, the SRSOn the climb flight path, 2 engines running, the SRS

(speed reference system) provides a pitch attitude(speed reference system) provides a pitch attitude

to maintain:to maintain:

V2.V2.

V2 + 10.V2 + 10.

F speed.F speed.

Green dot speed.Green dot speed.

8/21/2019 54806217 Airbus CBTquiz1


In this situation, what will happen if you push theHDG knob?

In this situation, what will happen if you push theIn this situation, what will happen if you push the

HDG knob?HDG knob?

Nothing will happen as PERUS is theNothing will happen as PERUS is the

FROM WPT and as such, the active legFROM WPT and as such, the active leg

cannot be intercepted.cannot be intercepted.

NAV will be armed (blue) and an interceptNAV will be armed (blue) and an interceptpoint will be computed by the FM topoint will be computed by the FM to

intercept the active leg.intercept the active leg.

The aircraft will follow the selected HDGThe aircraft will follow the selected HDG

whatever the action on the FCU is.whatever the action on the FCU is.

The selected target will change from aThe selected target will change from a

HDG to a TRK.HDG to a TRK.

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of GA TRK, displayed on theFMA?

What is the meaning of GA TRK, displayed on theWhat is the meaning of GA TRK, displayed on the

FMA?FMA?

The aircraft is guided by theThe aircraft is guided by the autoflightautoflight

system along the programmed missedsystem along the programmed missed

approach navigation.approach navigation.

The aircraft is guided along a new routeThe aircraft is guided along a new routeas the navigation accuracy level revertedas the navigation accuracy level reverted

toto ““lowlow”” at the time of go around.at the time of go around.

The aircraft maintains the track followedThe aircraft maintains the track followed

at mode engagement.at mode engagement.

The aircraft proceeds on the fastest wayThe aircraft proceeds on the fastest way

to come back for a new approach.to come back for a new approach.

8/21/2019 54806217 Airbus CBTquiz1


Any time the alpha floor protection is triggered,

TOGA thrust is automatically set by the autothrust.

When is this protection available?

Any time the alpha floor protection is triggered,Any time the alpha floor protection is triggered,

TOGA thrust is automatically set by theTOGA thrust is automatically set by the autothrustautothrust..

When is this protection available?When is this protection available?

Throughout the whole flight envelope.Throughout the whole flight envelope.

Only available on configuration 2, 3 or fullOnly available on configuration 2, 3 or full

(with flaps extended).(with flaps extended).

From lift off until 20 feet on approach.From lift off until 20 feet on approach.

From lift off until 100 feet on approach.From lift off until 100 feet on approach.

8/21/2019 54806217 Airbus CBTquiz1


Why must the pilot press the take over pushbuttonon the side stick twice to disconnect the autopilot?

Why must the pilot press the take over pushbuttonWhy must the pilot press the take over pushbutton

on the side stick twice to disconnect the autopilot?on the side stick twice to disconnect the autopilot?

A first time to disconnect the autopilotA first time to disconnect the autopilot

and a second time to confirm theand a second time to confirm the

disconnection.disconnection.

A the first time to disconnect the autopilotA the first time to disconnect the autopilotand a second time to get a definite priorityand a second time to get a definite priority

on his side.on his side.


and a second time to reset all the relatedand a second time to reset all the related

warnings.warnings.


and a second time to reset the masterand a second time to reset the master

FMGC.FMGC.

8/21/2019 54806217 Airbus CBTquiz1


TheThe autothrustautothrust is active but the thrust isis active but the thrust is

limited by the thrust levers position.limited by the thrust levers position.

TheThe autothrustautothrust is still active but canis still active but can

control the thrust to IDLE only.control the thrust to IDLE only.

What does the “ AUTOFLT A/THR LIMITED” messagemean?

What does theWhat does the ““ AUTOFLT AUTOFLT A/THR LIMITED A/THR LIMITED”” messagemessage

mean?mean?

TheThe autothrustautothrust is active but only oneis active but only one

channel is operative.channel is operative.

The maximum engine thrust has beenThe maximum engine thrust has been

automatically reduced by theautomatically reduced by the FADECsFADECs..

8/21/2019 54806217 Airbus CBTquiz1


Both autopilots are engaged which FMGC ismaster?

Both autopilots are engaged which FMGC isBoth autopilots are engaged which FMGC is

master?master?

FMGC1.FMGC1.

FMGC2.FMGC2.

It depends on the active flight phase.It depends on the active flight phase.

None as the twoNone as the two FMGCFMGC’’ss are actingare acting

independently.independently.

FMGC 2FMGC 1

8/21/2019 54806217 Airbus CBTquiz1


FD1 +2 are ON, no AP is engaged, which FMGC ismaster?

FD1 +2 are ON, no AP is engaged, which FMGC isFD1 +2 are ON, no AP is engaged, which FMGC is

master?master?

The switching occurs at every FMGCThe switching occurs at every FMGC

power up.power up.

It depends on which ATHR channel isIt depends on which ATHR channel is

engaged.engaged.

FMGC2.FMGC2.

FMGC1.FMGC1.

FMGC 2FMGC 1

8/21/2019 54806217 Airbus CBTquiz1


In independent operation mode which FMGC ismaster?

In independent operation mode which FMGC isIn independent operation mode which FMGC is

master?master?

FMGC1.FMGC1.

FMGC2.FMGC2.

None, the twoNone, the two FMGCFMGC’’ss are actingare acting

independently.independently.

It depends on which FMGC was theIt depends on which FMGC was the

master at the time of dual mode failure.master at the time of dual mode failure.

FMGC 2FMGC 1

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of “OPP FMGC IN PROCESS”,

the message displayed here in the scratchpad of

MCDU1?

What is the meaning ofWhat is the meaning of ““OPP FMGC IN PROCESSOPP FMGC IN PROCESS””,,

the message displayed here in the scratchpad ofthe message displayed here in the scratchpad of

MCDU1?MCDU1?

MCDU1 is driven by FMGC2.MCDU1 is driven by FMGC2.

The FMGC2 is now master.The FMGC2 is now master.

The FMGC2 performance became betterThe FMGC2 performance became better

than the FMGC1.than the FMGC1.

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of “SET OFFSIDE RNG/MODE”which appears on ND1?

What is the meaning ofWhat is the meaning of ““SET OFFSIDE RNG/MODESET OFFSIDE RNG/MODE””

which appears on ND1?which appears on ND1?

The selection of the offside range modeThe selection of the offside range mode

will allow the display of the navigationwill allow the display of the navigation

map on this side.map on this side.

The selection of the offside range modeThe selection of the offside range modewill make the FMGCwill make the FMGC’’s resynchronizations resynchronization

shorter.shorter.


will make the return on FMGC dual modewill make the return on FMGC dual mode

easier.easier.


will reduce the FMGC1 reset duration atwill reduce the FMGC1 reset duration at

one minute.one minute.

8/21/2019 54806217 Airbus CBTquiz1


FCU 1 failure has no consequences on theFCU 1 failure has no consequences on the

FCU utilization, as the second channelFCU utilization, as the second channel

has automatically taken over.has automatically taken over.

The FCU is totally unserviceable.The FCU is totally unserviceable.

Only the lateral modes can be set from theOnly the lateral modes can be set from the

FCU panel.FCU panel.

Some FCU functions LOC and APPSome FCU functions LOC and APP

pushbuttons are not available.pushbuttons are not available.

The FCU1 has failed, how can we use the FCU now?The FCU1 has failed, how can we use the FCU now?The FCU1 has failed, how can we use the FCU now?

8/21/2019 54806217 Airbus CBTquiz1


The FCU 1 and 2 have failed, how the pilot cancontrol the vertical and lateral modes?

The FCU 1 and 2 have failed, how the pilot canThe FCU 1 and 2 have failed, how the pilot can

control the vertical and lateral modes?control the vertical and lateral modes?

Both APBoth AP’’s are lost but the FCU controlss are lost but the FCU controls

and indications are still available.and indications are still available.

Only the FD1 and 2 are available.Only the FD1 and 2 are available.

The vertical and lateral modes cannot beThe vertical and lateral modes cannot be

controlled from the FCU. Only the manualcontrolled from the FCU. Only the manual

flight on raw data is possible.flight on raw data is possible.

The pilot can control the lateral andThe pilot can control the lateral and

vertical modes using the MCDU.vertical modes using the MCDU.

8/21/2019 54806217 Airbus CBTquiz1


What does “INDEPENDENT OPERATION”,displayed in both MCDU scratchpads, mean?

What doesWhat does ““INDEPENDENT OPERATIONINDEPENDENT OPERATION””,,

displayed in both MCDU scratchpads, mean?displayed in both MCDU scratchpads, mean?

The pilot can engage both AP in allThe pilot can engage both AP in all

phases of flight.phases of flight.

The cross talk function is lost, eachThe cross talk function is lost, eachFMGC will work independently, the sameFMGC will work independently, the same

entry has to be made on bothentry has to be made on both MCDUsMCDUs..

There is no more radio updating of theThere is no more radio updating of the

FMGC position and only the mix IRSFMGC position and only the mix IRS

coordinates are provided for thecoordinates are provided for the

navigation.navigation.

8/21/2019 54806217 Airbus CBTquiz1


The FMGC1 failed and “OPP FMGC IN PROCESS” is

displayed on the MCDU1. The FMGC2 has taken

over automatically :

The FMGC1 failed andThe FMGC1 failed and ““OPP FMGC IN PROCESSOPP FMGC IN PROCESS”” isis

displayed on the MCDU1. The FMGC2 has takendisplayed on the MCDU1. The FMGC2 has taken

over automatically :over automatically :

The entry can be done from either MCDU.The entry can be done from either MCDU.

The entry can be done from MCDU 1 only.The entry can be done from MCDU 1 only.

The entry can be done from MCDU 2 only.The entry can be done from MCDU 2 only.

FMGC 2FMGC 1

8/21/2019 54806217 Airbus CBTquiz1


You are in “THR IDLE/DES” modes with autopilot 1

engaged and the FCU 1 fails.

What is the action required?

You are in You are in ““THR IDLE/DESTHR IDLE/DES”” modes with autopilot 1modes with autopilot 1

engaged and the FCU 1 fails.engaged and the FCU 1 fails.

What is the action required?What is the action required?

As the autopilot 1 disengages, engageAs the autopilot 1 disengages, engage

autopilot 2.autopilot 2.

The PFD barometric reference is now onlyThe PFD barometric reference is now only

available on standard and the pilot mustavailable on standard and the pilot must

set the currentset the current barobaro setting on thesetting on the

standby altimeter.standby altimeter.

The FCU2 has taken over automaticallyThe FCU2 has taken over automatically

and theand the barobaro reference must be crossreference must be cross

checked.checked.

8/21/2019 54806217 Airbus CBTquiz1


What happens if the HDG selector knob is pushed?What happens if the HDG selector knob is pushed?What happens if the HDG selector knob is pushed?

The aircraft reverts to TRK.The aircraft reverts to TRK.

The HDG/TRK target changes.The HDG/TRK target changes.

Nothing, the aircraft follows indefinitelyNothing, the aircraft follows indefinitely

the selected HDG/TRK.the selected HDG/TRK.

The aircraft continues to followThe aircraft continues to follow

the current HDG until Fthe current HDG until F--PLN interception.PLN interception.

8/21/2019 54806217 Airbus CBTquiz1


What happens if the HDG selector knob is pulled?What happens if the HDG selector knob is pulled?What happens if the HDG selector knob is pulled?

The aircraft reverts to the original FThe aircraft reverts to the original F--PLN.PLN.

The HDG target changes to TRK.The HDG target changes to TRK.

The aircraft follows the selected HDG untilThe aircraft follows the selected HDG until

intercepting the lateral Fintercepting the lateral F--PLN.PLN.

Nothing, the aircraft continues on HDGNothing, the aircraft continues on HDG

140 indefinitely.140 indefinitely.

8/21/2019 54806217 Airbus CBTquiz1


Please indicate the position of the two FLIGHTDIRECTOR (FD) controls.

Please indicate the position of the two FLIGHTPlease indicate the position of the two FLIGHT

DIRECTOR (FD) controls.DIRECTOR (FD) controls.

8/21/2019 54806217 Airbus CBTquiz1


Is the aircraft following a track or a heading?Is the aircraft following a track or a heading?Is the aircraft following a track or a heading?

TrackTrack

HeadingHeading

8/21/2019 54806217 Airbus CBTquiz1


Look at the FMA. LOC in blue is...Look at the FMA. LOC in blue is...Look at the FMA. LOC in blue is...

The active lateral mode which is aThe active lateral mode which is a

constraint.constraint.

The armed lateral mode.The armed lateral mode.

The armed lateral mode which is aThe armed lateral mode which is a


The active lateral mode.The active lateral mode.

8/21/2019 54806217 Airbus CBTquiz1


Look at the FMA. NAV in green is...Look at the FMA. NAV in green is...Look at the FMA. NAV in green is...

The active lateral mode which is aThe active lateral mode which is a


The armed lateral mode.The armed lateral mode.

The armed lateral mode which is aThe armed lateral mode which is a


The active lateral mode.The active lateral mode.

8/21/2019 54806217 Airbus CBTquiz1


A/THR in blue means it is...A/THR in blue means it is...A/THR in blue means it is...

disconnected.disconnected.

armed.armed.

active.active.

8/21/2019 54806217 Airbus CBTquiz1


The yaw bar, when displayed on the PFD instead ofthe flight director roll bar, is used to :

The yaw bar, when displayed on the PFD instead ofThe yaw bar, when displayed on the PFD instead of

the flight director roll bar, is used to :the flight director roll bar, is used to :

Provide guidance, if a localizer isProvide guidance, if a localizer is

available for takeavailable for take--off and rolloff and roll--out phases.out phases.

Provide guidance after takeProvide guidance after take--off up to 1000off up to 1000feat AGL to maintain the runway centerfeat AGL to maintain the runway center

line.line.

Confirm that the aircraft is wellConfirm that the aircraft is well

established in the glide slope on ILS finalestablished in the glide slope on ILS final

approach.approach.

Change over automatically in case ofChange over automatically in case of

localizer failure on ILS final approach.localizer failure on ILS final approach.

8/21/2019 54806217 Airbus CBTquiz1


What does MAN TOGA indicate on the FMAcolumn?

What does MAN TOGA indicate on the FMAWhat does MAN TOGA indicate on the FMA

column?column?

The thrust has been manually set toThe thrust has been manually set to

TOGA.TOGA.

TheThe autothrustautothrust system is inoperative.system is inoperative.

The FMGC guidanceThe FMGC guidance autothrustautothrust commandcommand

is unserviceable.is unserviceable.

The pilot has disconnected theThe pilot has disconnected the autothrustautothrust

system.system.

8/21/2019 54806217 Airbus CBTquiz1


TheThe autothrustautothrust will be automaticallywill be automatically

activated by the FMGC without any pilotactivated by the FMGC without any pilot

action when crossing the thrust reductionaction when crossing the thrust reduction

altitude.altitude.

TheThe autothrustautothrust will become active whenwill become active whenthe pilot sets the thrust levers in the climbthe pilot sets the thrust levers in the climb

detent.detent.

The thrust levers must be set to idle andThe thrust levers must be set to idle and

then in the climb detent to activate thethen in the climb detent to activate the

autothrustautothrust..

With all engines operative and A/THR armed, howdoes a pilot activate the autothrust?

With all engines operative and A/THR armed, howWith all engines operative and A/THR armed, how

does a pilot activate thedoes a pilot activate the autothrustautothrust??

8/21/2019 54806217 Airbus CBTquiz1


“LVR CLB” white flashing on the FMA indicates :““LVR CLBLVR CLB”” white flashing on the FMA indicates :white flashing on the FMA indicates :

We have crossed the thrust reductionWe have crossed the thrust reduction

altitude.altitude.

TheThe autothrustautothrust levers are stuck and canlevers are stuck and can

not be put in the climb detent.not be put in the climb detent.

The pilot has forgotten to enter the FLEXThe pilot has forgotten to enter the FLEX

temperature on the MCDU taketemperature on the MCDU take--off pageoff page

before taking off.before taking off.

The thrust levers will automatically moveThe thrust levers will automatically move

to the climb detent.to the climb detent.

8/21/2019 54806217 Airbus CBTquiz1


The constant rate of climb is maintainedThe constant rate of climb is maintained

by the autopilot.by the autopilot.

You are established in climb, THR CLB mode isactive:

You are established in climb, THR CLB mode is You are established in climb, THR CLB mode is

active:active:

The speed is controlled by the thrust andThe speed is controlled by the thrust and

the rate of climb by the autopilot.the rate of climb by the autopilot.

A/THR commands CLB thrust and APA/THR commands CLB thrust and AP

maintains the target speed by using pitchmaintains the target speed by using pitch

adjustments.adjustments.

The speed and the rate of climb areThe speed and the rate of climb are

controlled by the thrust.controlled by the thrust.

8/21/2019 54806217 Airbus CBTquiz1


The aircraft has leveled off at 13000 feet, ALT is

green on the FMA and the autothrust is in SPEED

mode:

The aircraft has leveled off at 13000 feet, ALT isThe aircraft has leveled off at 13000 feet, ALT is

green on the FMA and thegreen on the FMA and the autothrustautothrust is in SPEEDis in SPEED

mode:mode:

The target speed and the altitude areThe target speed and the altitude are

maintained by the autopilot.maintained by the autopilot.

The target speed is maintained by theThe target speed is maintained by theautopilot and the altitude is controlled byautopilot and the altitude is controlled by

thethe autothrustautothrust..

TheThe autothrustautothrust system controls the thrustsystem controls the thrust

to maintain the target speed and theto maintain the target speed and the

autopilot maintain the altitude byautopilot maintain the altitude by

adjusting the pitch.adjusting the pitch.

The altitude and speed are maintained byThe altitude and speed are maintained by

the A/THR.the A/THR.

8/21/2019 54806217 Airbus CBTquiz1


To disconnect the A/THR.To disconnect the A/THR.

Why do you set the thrust levers to IDLE forlanding?

Why do you set the thrust levers to IDLE forWhy do you set the thrust levers to IDLE for

landing?landing?

To engage the manual mode of theTo engage the manual mode of the

autothrustautothrust..

To be prepared in case of touch and go.To be prepared in case of touch and go.

8/21/2019 54806217 Airbus CBTquiz1


According to these indications, what is the correctstatement?

According to these indications, what is the correctAccording to these indications, what is the correct

statement?statement?

The A/THR is armed.The A/THR is armed.

The A/THR is active.The A/THR is active.

The A/THR has failed.The A/THR has failed.

The A/THR is disconnected.The A/THR is disconnected.

8/21/2019 54806217 Airbus CBTquiz1


ALT mode is engaged, MCDU PERF page indicatesCLB. Why?

ALT mode is engaged, MCDU PERF page indicatesALT mode is engaged, MCDU PERF page indicates

CLB. Why?CLB. Why?

The FMGS is unable to control the climb.The FMGS is unable to control the climb.

FL290 is above the initial CRZ FL.FL290 is above the initial CRZ FL.

The FMGS 1 has failed.The FMGS 1 has failed.

FL290 is the FCU selection, and is belowFL290 is the FCU selection, and is below

the CRZ FL.the CRZ FL.

C

8/21/2019 54806217 Airbus CBTquiz1


ALT mode is engaged at FL290, MCDU PERF page

indicates CLB. How do you obtain ALT CRZ on the

FMA at that flight level (FL290) ?

ALT mode is engaged at FL290, MCDU PERF pageALT mode is engaged at FL290, MCDU PERF page

indicates CLB. How do you obtain ALT CRZ on theindicates CLB. How do you obtain ALT CRZ on the

FMA at that flight level (FL290) ?FMA at that flight level (FL290) ?

Set the new altitude clearance FL290 onSet the new altitude clearance FL290 on

the MCDU PROG page.the MCDU PROG page.

Set the new altitude clearance on the FCU.Set the new altitude clearance on the FCU.

Push the altitude selector knob toPush the altitude selector knob to

continue the climb as programmedcontinue the climb as programmed

before.before.

8/21/2019 54806217 Airbus CBTquiz1


We are in OP DES and THR IDLE modes :We are in OP DES and THR IDLE modes :We are in OP DES and THR IDLE modes :

TheThe autothrustautothrust maintain the thrust at idlemaintain the thrust at idle

and the auto pilot adjust the pitch toand the auto pilot adjust the pitch to

maintain the target speed.maintain the target speed.

TheThe autothrustautothrust adjust the thrust toadjust the thrust tomaintain the target speed and themaintain the target speed and the

autopilot control the descent flight path.autopilot control the descent flight path.

TheThe autothrustautothrust maintain the thrust at idlemaintain the thrust at idle

and the autopilot control the verticaland the autopilot control the vertical

speed.speed.

TheThe autothrustautothrust control the target speedcontrol the target speed

and the rate of descent.and the rate of descent.

8/21/2019 54806217 Airbus CBTquiz1


The approach phase activation can be done:The approach phase activation can be done:The approach phase activation can be done:

Automatically when the aircraft overfly theAutomatically when the aircraft overfly the

deceleration point or manually by the pilotdeceleration point or manually by the pilot

on the PERF pageon the PERF page

Only manually by the pilot through theOnly manually by the pilot through theMCDU PERF. Page.MCDU PERF. Page.

Only automatically at the decelerationOnly automatically at the deceleration

point.point.

8/21/2019 54806217 Airbus CBTquiz1


As soon as the approach phase is activated, themanaged speed will depend on:

As soon as the approach phase is activated, theAs soon as the approach phase is activated, the

managed speed will depend on:managed speed will depend on:

Which autopilot is engaged.Which autopilot is engaged.

The vertical mode previously flown.The vertical mode previously flown.

Which FMGC is the master.Which FMGC is the master.

The aircraft configuration.The aircraft configuration.

8/21/2019 54806217 Airbus CBTquiz1


At 400 feet RA the LAND mode engages.How can this mode be disengaged:

At 400 feet RA the LAND mode engages.At 400 feet RA the LAND mode engages.

How can this mode be disengaged:How can this mode be disengaged:

By pulling the heading selector knob.By pulling the heading selector knob.

By pulling the V/SBy pulling the V/S -- FPA knob.FPA knob.

By pressing the approach modeBy pressing the approach mode

pushbutton.pushbutton.

By setting TOGA to engage the go aroundBy setting TOGA to engage the go around

mode.mode.

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of the small magenta dotdisplayed by the altitude scale?

What is the meaning of the small magenta dotWhat is the meaning of the small magenta dot

displayed by the altitude scale?displayed by the altitude scale?

It warns the pilot about a possible wrongIt warns the pilot about a possible wrong

altitude setting on the FCU.altitude setting on the FCU.

It warns the pilot that the speed must beIt warns the pilot that the speed must be

reduced to regain the computed descentreduced to regain the computed descent

profile.profile.

It indicates that the expedite mode mustIt indicates that the expedite mode must

be engaged.be engaged.

It highlights any vertical deviation of theIt highlights any vertical deviation of theaircraft from the computed descentaircraft from the computed descent

profile.profile.

You want to speak to the mechanic He is

You want to speak to the mechanic He isYou want to speak to the mechanic He is

8/21/2019 54806217 Airbus CBTquiz1


I use the MECH pbI use the MECH pb swsw on the CALLSon the CALLSpanel.panel.

I use VHF 3 to call him.I use VHF 3 to call him.

I select the MECH transmission keyI select the MECH transmission key

on the ACP.on the ACP.

You want to speak to the mechanic. He is

somewhere around the aircraft but you can’t see

him. How do you get his attention?

You want to speak to the mechanic. He is You want to speak to the mechanic. He is

somewhere around the aircraft but you cansomewhere around the aircraft but you can’’t seet see

him. How do you get his attention?him. How do you get his attention?

I open the side window and try toI open the side window and try to

get his attention.get his attention.

8/21/2019 54806217 Airbus CBTquiz1


On the RCDR control panel, press theOn the RCDR control panel, press theGND CTL pb to switch the CVR ON, thenGND CTL pb to switch the CVR ON, then

press the CVR TEST pb.press the CVR TEST pb.

The CVR TEST can only be performedThe CVR TEST can only be performed

after one engine is started thenafter one engine is started then ““BB””

answer is applied.answer is applied.

Be sure the PARKING BRK is ON thenBe sure the PARKING BRK is ON then

repeatrepeat ““BB”” answer.answer.

During Preflight, check of the CVR operation isperformed as follow.

During Preflight, check of the CVR operation isDuring Preflight, check of the CVR operation is

performed as follow.performed as follow.

The system being operative as soon asThe system being operative as soon as

aircraftaircraft ElecElec Power network is powered,Power network is powered,

on the RCDR Control panel, press theon the RCDR Control panel, press the

CVR TEST pb, you get an audio signal forCVR TEST pb, you get an audio signal for

correct operation.correct operation.

8/21/2019 54806217 Airbus CBTquiz1


The aircraft must be on the ground withThe aircraft must be on the ground withat least one engine running.at least one engine running.

The aircraft must be off the ground.The aircraft must be off the ground.

The engines must be shut down for atThe engines must be shut down for at

least 5 minutes.least 5 minutes.

After landing, to erase the CVR...After landing, to erase the CVR...After landing, to erase the CVR...

The aircraft must be on the ground withThe aircraft must be on the ground with

the parking brake set.the parking brake set.

8/21/2019 54806217 Airbus CBTquiz1


It is an indication that the VHF used onIt is an indication that the VHF used onRMP 2 is not the standard one.RMP 2 is not the standard one.

It indicates that RMP1 is configured toIt indicates that RMP1 is configured to

tune VFH2.tune VFH2.

It indicates that RMP2 is configured toIt indicates that RMP2 is configured to

tune VHF2.tune VHF2.

On the RMP control panel, what does the white SELlight mean?

On the RMP control panel, what does the white SELOn the RMP control panel, what does the white SEL

light mean?light mean?

It is an indication for a SELCAL.It is an indication for a SELCAL.

RMP 2RMP 2

RMP 1RMP 1

8/21/2019 54806217 Airbus CBTquiz1


Pressing the VHF 1 and SEL pb on RMP 1.Pressing the VHF 1 and SEL pb on RMP 1.

Pressing the SEL pb on RMP 2.Pressing the SEL pb on RMP 2.

Pressing the VHF 2 on RMP 2.Pressing the VHF 2 on RMP 2.

How do you extinguish the white SEL light?How do you extinguish the white SEL light?How do you extinguish the white SEL light?

Pressing the SEL pb on RMP 1.Pressing the SEL pb on RMP 1.

RMP 2RMP 2

RMP 1RMP 1

O th VHF t i f RMP 1 f il VHF 1O th VHF t i f RMP 1 f il VHF 1

8/21/2019 54806217 Airbus CBTquiz1


False.False.

On the VHF system, in case of RMP 1 failure, VHF 1is lost.

On the VHF system, in case of RMP 1 failure, VHF 1On the VHF system, in case of RMP 1 failure, VHF 1

is lost.is lost.

True.True.

O S C G C

With th AUDIO SWITCHING k b i th CAPT 3With th AUDIO SWITCHING k b i th CAPT 3

8/21/2019 54806217 Airbus CBTquiz1


False.False.

With the AUDIO SWITCHING knob in the CAPT 3position, the captain substitutes ACP 3 for ACP 1.

With the AUDIO SWITCHING knob in the CAPT 3With the AUDIO SWITCHING knob in the CAPT 3

position, the captain substitutes ACP 3 for ACP 1.position, the captain substitutes ACP 3 for ACP 1.

True.True.

On the communication control panel, the amber

On the communication control panel, the amberOn the communication control panel, the amber

8/21/2019 54806217 Airbus CBTquiz1


False.False.

On the communication control panel, the amber

CALL light indicates that somebody is trying to

reach you via VHF 3.

p ,p ,

CALL light indicates that somebody is trying toCALL light indicates that somebody is trying to

reach you via VHF 3.reach you via VHF 3.

True.True.

You are in an ELECTRICAL EMERGENCY

CONFIGURATION, shortly after the fault occurred,

You are in an ELECTRICAL EMERGENCY You are in an ELECTRICAL EMERGENCY

CONFIGURATION, shortly after the fault occurred,CONFIGURATION, shortly after the fault occurred,

8/21/2019 54806217 Airbus CBTquiz1


CO GU O , s o t y a te t e au t occu ed,

you notice the red FAULT light on the RAT & EMER

GEN pushbutton.

How do you interpret this indication ?

, y ,y

you notice the red FAULT light on the RAT & EMERyou notice the red FAULT light on the RAT & EMER

GEN pushbutton.GEN pushbutton.

How do you interpret this indication ?How do you interpret this indication ?

The EMER GEN is not supplying theThe EMER GEN is not supplying the

system.system.

The fault light on the RAT & EMER GENThe fault light on the RAT & EMER GENpbpb will extinguish by depressing it.will extinguish by depressing it.

The FAULT light is always on when youThe FAULT light is always on when you

are in ELEC EMER CONFIG.are in ELEC EMER CONFIG.

You are in an ELECTRICAL EMERGENCY

CONFIGURATION, on ELEC panel you have

You are in an ELECTRICAL EMERGENCY You are in an ELECTRICAL EMERGENCY

CONFIGURATION, on ELEC panel you haveCONFIGURATION, on ELEC panel you have

8/21/2019 54806217 Airbus CBTquiz1


, p y

depressed the GEN 1 and GEN 2 pb for reset.

The reset was unsuccessful.

Why must you push the BUS TIE pb sw to OFF ?

p y

depressed the GEN 1 and GEN 2depressed the GEN 1 and GEN 2 pbpb for reset.for reset.

The reset was unsuccessful.The reset was unsuccessful.

Why must you push the BUS TIEWhy must you push the BUS TIE pbpb swsw to OFF ?to OFF ?

To separate both sides of the electricalTo separate both sides of the electrical

system.system.

To connect both generators directly to theTo connect both generators directly to theAC ESS BUS.AC ESS BUS.

To connect both sides of the electricalTo connect both sides of the electrical

system.system.

To switch both generators to the oppositeTo switch both generators to the opposite

side AC BUS.side AC BUS.

In an ELECTRICAL EMERGENCY CONFIGURATION,

after performing the initial ECAM procedure you

In an ELECTRICAL EMERGENCY CONFIGURATION,In an ELECTRICAL EMERGENCY CONFIGURATION,

after performing the initial ECAM procedure youafter performing the initial ECAM procedure you

8/21/2019 54806217 Airbus CBTquiz1


after performing the initial ECAM procedure, youhave separated both sides of the electrical system.

Why do you have to try another generator reset ?

after performing the initial ECAM procedure, youafter performing the initial ECAM procedure, you

have separated both sides of the electrical system.have separated both sides of the electrical system.

Why do you have to try another generator reset ?Why do you have to try another generator reset ?

If there was a short circuit, you mightIf there was a short circuit, you might

recover one generator now.recover one generator now.

Because the generators had time to coolBecause the generators had time to cooldown and now a reset might bedown and now a reset might be

successful.successful.

You should always try two resets if you You should always try two resets if you

have a generator failure.have a generator failure.

The purpose of the Integrated Drive Generator (IDG)

The purpose of the Integrated Drive Generator (IDG)The purpose of the Integrated Drive Generator (IDG)

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Reconnect the generator to its driveReconnect the generator to its drivemechanism.mechanism.

Disconnect the corresponding generatorDisconnect the corresponding generator

from its drive shaft.from its drive shaft.

The purpose of the Integrated Drive Generator (IDG)pb sw is to:

The purpose of the Integrated Drive Generator (IDG)The purpose of the Integrated Drive Generator (IDG)

pbpb swsw is to:is to:

Cut the corresponding generator supplyCut the corresponding generator supply

to AC bus 1 or 2.to AC bus 1 or 2.

Cut the corresponding generator supplyCut the corresponding generator supply

to the ESS AC bus.to the ESS AC bus.

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The engine driven generators are running.The engine driven generators are running.The engine driven generators are running.

At the engine RPM trough their gearboxAt the engine RPM trough their gearbox

connection.connection.

At constant speed by a drive mechanismAt constant speed by a drive mechanismbetween the generator and ENG gearbox.between the generator and ENG gearbox.

At a intermediate speed controlled by anAt a intermediate speed controlled by an

electronic computer.electronic computer.

No necessity to control the generatorNo necessity to control the generator

speed because the AC network operatesspeed because the AC network operates

under variable frequency.under variable frequency.

GEN 1 GEN 2

IDG 1 IDG 2

The Electrical System includes two buses: AC ESS

The Electrical System includes two buses: AC ESSThe Electrical System includes two buses: AC ESS

BUS d DC ESS BUS

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BUS and DC ESS BUS.

In normal configuration :

BUS and DC ESS BUS.BUS and DC ESS BUS.

In normal configuration :In normal configuration :

AC ESS bus is fed by AC bus 1.AC ESS bus is fed by AC bus 1.

DC ESS bus is fed by DC bus 1.DC ESS bus is fed by DC bus 1.

AC ESS bus is fed by AC bus 2.AC ESS bus is fed by AC bus 2.DC ESS bus is fed by DC bus 1.DC ESS bus is fed by DC bus 1.

To balance theTo balance the ElecElec load GEN 1 is directlyload GEN 1 is directly

supplying the AC ESS BUS.supplying the AC ESS BUS.

To balance theTo balance the ElecElec load GEN 2 is directlyload GEN 2 is directly

supplying the AC ESS bus.supplying the AC ESS bus.

The purpose of AC ESS FEED pb sw is to enable

The purpose of AC ESS FEED pbThe purpose of AC ESS FEED pb swsw is to enableis to enable

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The purpose of AC ESS FEED pb sw is to enablethe pilot to switchover the supply of AC ESS bus.

The purpose of AC ESS FEED pbThe purpose of AC ESS FEED pb swsw is to enableis to enable

the pilot to switchover the supply of AC ESS bus.the pilot to switchover the supply of AC ESS bus.

From AC bus 2 to AC bus 1.From AC bus 2 to AC bus 1.

From AC bus 1 to AC bus 2.From AC bus 1 to AC bus 2.

From the APU generator.From the APU generator.

From ESS DC bus.From ESS DC bus.

Pl i di t th iti f th ELEC lPl i di t th iti f th ELEC l

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Please indicate the position of the ELEC panel.Please indicate the position of the ELEC panel.Please indicate the position of the ELEC panel.

Please indicate the position of the EMERG ELEC

Please indicate the position of the EMERG ELECPlease indicate the position of the EMERG ELEC

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Please indicate the position of the EMERG ELECPWR panel.

pp

PWR panel.PWR panel.

The emergency electrical generator used as a back

up is hydraulically driven by the RAT which

t ti ll t d h b th AC BUS 1 d AC

The emergency electrical generator used as a backThe emergency electrical generator used as a back

up is hydraulically driven by the RAT whichup is hydraulically driven by the RAT which

automatically extends when both AC BUS 1 and ACautomatically extends when both AC BUS 1 and AC

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automatically extends when both AC BUS 1 and AC

BUS 2 are lost and the aircraft speed is above

100kts.

automatically extends when both AC BUS 1 and ACautomatically extends when both AC BUS 1 and AC

BUS 2 are lost and the aircraft speed is aboveBUS 2 are lost and the aircraft speed is above

100kts.100kts.

True.True.

False.False.

From ECAM ELEC page, the APU GEN box

From ECAM ELEC page, the APU GEN boxFrom ECAM ELEC page, the APU GEN box

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p g ,information indicates that:

p g

information indicates that:information indicates that:

The APU GEN does not have priority overThe APU GEN does not have priority over

the external power.the external power.

The APU GENThe APU GEN pbpb SW on overhead panelSW on overhead panelis off.is off.

The APU is not fully available yet.The APU is not fully available yet.

There is defect on the APU GEN out put.There is defect on the APU GEN out put.

Looking at the ECAM ELEC Page, to connect APU

Looking at the ECAM ELEC Page, to connect APULooking at the ECAM ELEC Page, to connect APU

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g g ,GEN:GEN:GEN:

Push APU GEN pbPush APU GEN pb swsw located overheadlocated overhead

panel.panel.

Wait until 1st Engine is Started.Wait until 1st Engine is Started.

Deselect EXT PWR.Deselect EXT PWR.

SWITCH OFF BAT 1+2.SWITCH OFF BAT 1+2.

What does the APU GEN % indication mean ?

What does the APU GEN % indication mean ?What does the APU GEN % indication mean ?

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What does the APU GEN % indication mean ?What does the APU GEN % indication mean ?What does the APU GEN % indication mean ?

APU GEN shares 36% of theAPU GEN shares 36% of the elecelec networknetwork

load, the remaining 64% being taken byload, the remaining 64% being taken by

the external power.the external power.

APU GEN is supplying the network at 36%APU GEN is supplying the network at 36%of its maximum load.of its maximum load.

The external power is supplying theThe external power is supplying the

network.network.

During preliminary procedure to check the battery

During preliminary procedure to check the batteryDuring preliminary procedure to check the battery

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voltage, the associated BATT pb sw should be:voltage, the associated BATTvoltage, the associated BATT pbpb swsw should be:should be:

Switched ON.Switched ON.

Switched OFF.Switched OFF.

Any position, the voltage indication beingAny position, the voltage indication being

all time available.all time available.

The minimum battery voltage for normal operation

The minimum battery voltage for normal operationThe minimum battery voltage for normal operation

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should be:should be:should be:

24V.24V.

25,5V.25,5V.

28V.28V.

The EXT PWR AVAIL illuminated green on the

The EXT PWR AVAIL illuminated green on theThe EXT PWR AVAIL illuminated green on the

h d l th th d l th t

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overhead panel means that :overhead panel means that :overhead panel means that :

The ground cart is supplying the aircraftThe ground cart is supplying the aircraft

network.network.

The external power is plugged in andThe external power is plugged in anddelivers bleed air.delivers bleed air.

The connected ground cart voltage andThe connected ground cart voltage and

frequency are normal.frequency are normal.

On EXT PWR pb sw, the illuminated cyan light

On EXT PWROn EXT PWR pbpb swsw, the illuminated cyan light, the illuminated cyan light

th tth t

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means that:means that:means that:

The ground cart is supplying the aircraftThe ground cart is supplying the aircraft

electrical network.electrical network.

External power is plugged in but notExternal power is plugged in but notsupplying the network.supplying the network.

External power is plugged in and deliversExternal power is plugged in and delivers

bleed air only.bleed air only.

After starting engine n°2, is the present ECAMELEC t fi ti ?

After starting engine nAfter starting engine n°°2, is the present ECAM2, is the present ECAM

ELEC t fi ti ?ELEC page a correct config ration?

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ELEC page a correct configuration?ELEC page a correct configuration?ELEC page a correct configuration?

No. ENG GEN nNo. ENG GEN n°°2 should power all2 should power all

aircraft network.aircraft network.

No. The APU GEN should continueNo. The APU GEN should continuepowering all aircraft network.powering all aircraft network.

Yes. ENG GEN n Yes. ENG GEN n°°2 is now powering its2 is now powering its

own side.own side.

As you enter in the dark cockpit you first check the

battery voltages.Wh t th h k b f h ki th

As you enter in the dark cockpit you first check theAs you enter in the dark cockpit you first check the

battery voltages.battery voltages.

What are the necessary checks before checking theWhat are the necessary checks before checking the

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You have to switch each battery on by its You have to switch each battery on by its

associatedassociated pbpb swsw to check the voltage.to check the voltage.

What are the necessary checks before checking the

voltages?

What are the necessary checks before checking theWhat are the necessary checks before checking the

voltages?voltages?

You must check that the external power is You must check that the external power is

available and then switch it on.available and then switch it on.

You can read the battery voltages You can read the battery voltagesimmediately. No actions are required.immediately. No actions are required.

In flight, following an AC BUS 1 FAULT, AC ESSFEED b t b d d i d t

In flight, following an AC BUS 1 FAULT, AC ESSIn flight, following an AC BUS 1 FAULT, AC ESS

FEED pbFEED pb swsw must be depressed in order to:must be depressed in order to:

8/21/2019 54806217 Airbus CBTquiz1


FEED pb sw must be depressed in order to:FEED pbFEED pb swsw must be depressed in order to:must be depressed in order to:

Recover AC ESS FEED from AC BUS 2.Recover AC ESS FEED from AC BUS 2.

Recover AC1 bus.Recover AC1 bus.

Recover AC2 bus.Recover AC2 bus.

AC BUS 1 FAULT will definitively lead to the DCand AC ESS buses loss:

AC BUS 1 FAULT will definitively lead to the DCAC BUS 1 FAULT will definitively lead to the DC

and AC ESS buses loss:and AC ESS buses loss:

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and AC ESS buses loss:and AC ESS buses loss:and AC ESS buses loss:

Yes. Yes.

No. Only AC ESS bus is recoverable.No. Only AC ESS bus is recoverable.

No. DC and AC ESS buses will beNo. DC and AC ESS buses will be

recovered by pushing on the AC ESSrecovered by pushing on the AC ESS

FEEDFEED pbpb swsw..

Following an AC BUS 1 fault, pushing the AC ESSFEED pb sw on ELEC overhead panel allows you:

Following an AC BUS 1 fault, pushing the AC ESSFollowing an AC BUS 1 fault, pushing the AC ESS

FEEDFEED pbpb swsw on ELEC overhead panel allows you:on ELEC overhead panel allows you:

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FEED pb sw on ELEC overhead panel allows you:FEEDFEED pbpb swsw on ELEC overhead panel allows you:on ELEC overhead panel allows you:

To recover the AC ESS BUS power only.To recover the AC ESS BUS power only.

To recover the DC ESS BUS power only.To recover the DC ESS BUS power only.

To recover AC and DC ESS buses.To recover AC and DC ESS buses.

To recover AC BUS 1 power.To recover AC BUS 1 power.

Following the RAT extension due to ELEC EMER

CONF, the RAT and EMER GEN FAULT light isilluminated

Following the RAT extension due to ELEC EMERFollowing the RAT extension due to ELEC EMER

CONF, the RAT and EMER GEN FAULT light isCONF, the RAT and EMER GEN FAULT light is

illuminatedilluminated

8/21/2019 54806217 Airbus CBTquiz1


illuminated.

What does it mean?

illuminated.illuminated.


We had an ELEC EMER configuration, theWe had an ELEC EMER configuration, the

RAT is extended.RAT is extended.

The fault stays illuminated even afterThe fault stays illuminated even afteremergency generator connection.emergency generator connection.

The emergency generator is notThe emergency generator is not

connected.connected.

In case of ELEC EMER CONF, LAND ASAP in red is

displayed on the E/WD.

In case of ELEC EMER CONF, LAND ASAP in red isIn case of ELEC EMER CONF, LAND ASAP in red is

displayed on the E/WD.displayed on the E/WD.

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This message will stay:This message will stay:This message will stay:

As long as the Red warning ELEC EMERAs long as the Red warning ELEC EMER

CONF persists.CONF persists.

Even after having reset one generatorEven after having reset one generatorsuccessfully.successfully.

Even if BUS TIE pbEven if BUS TIE pb swsw is pushed.is pushed.

Even if APU is started.Even if APU is started.

In case of an ELEC EMER CONFIG situation, how

can the two sides of the electrical system be

In case of an ELEC EMER CONFIG situation, howIn case of an ELEC EMER CONFIG situation, how

can the two sides of the electrical system becan the two sides of the electrical system be

?t d t i l t h t i it ?

8/21/2019 54806217 Airbus CBTquiz1


segregated e.g to isolate a short circuit ?segregated e.g to isolate a short circuit ?segregated e.g to isolate a short circuit ?

Push BUS TIEPush BUS TIE pbpb SW located on ELECSW located on ELEC

system overhead panel.system overhead panel.

Reset each AC generator.Reset each AC generator.

Manually lower RAT by pushing itsManually lower RAT by pushing its pbpb SWSW

Nothing has to be done because theNothing has to be done because the

segregation is done automatically.segregation is done automatically.

Being in an EMER ELEC configuration what ishappening when A/C speed drops below 140 kts?

Being in an EMER ELEC configuration what isBeing in an EMER ELEC configuration what is

happening when A/C speed drops below 140happening when A/C speed drops below 140 ktskts??

8/21/2019 54806217 Airbus CBTquiz1


happening when A/C speed drops below 140 kts?happening when A/C speed drops below 140happening when A/C speed drops below 140 ktskts??

AC generators are less powerful due toAC generators are less powerful due to

RAT speed decrease.RAT speed decrease.

Electrical network is automaticallyElectrical network is automaticallytransferred to the batteries.transferred to the batteries.

You have to stop AC generator by You have to stop AC generator by

pressing thepressing the ““MAN ONMAN ON--AUTOAUTO”” pbpb switch.switch.

You have to switch ON the both batteries. You have to switch ON the both batteries.

In ELEC EMER CONF, you are in single display

mode on the ECAM.

C ll ll ECAM ?

In ELEC EMER CONF, you are in single displayIn ELEC EMER CONF, you are in single display

mode on the ECAM.mode on the ECAM.

C ll ll ECAM t ?C ll ll ECAM t ?

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Can you manually call an ECAM system page ?Can you manually call an ECAM system page ?Can you manually call an ECAM system page ?

No. The upper ECAM screen is only usedNo. The upper ECAM screen is only used

for E/WD display.for E/WD display.

Yes, by pressing and holding its Yes, by pressing and holding its

associatedassociated pbpb SW on the ECAM controlSW on the ECAM controlpanel.panel.

In EMER ELEC CONF, when the RAT stalls due to

A/C speed decreasing, the static inverter will

b ti i d t l

In EMER ELEC CONF, when the RAT stalls due toIn EMER ELEC CONF, when the RAT stalls due to

A/C speed decreasing, the static inverter willA/C speed decreasing, the static inverter will

become acti e in order to s pplbecome active in order to supply:

8/21/2019 54806217 Airbus CBTquiz1


become active in order to supply:become active in order to supply:become active in order to supply:

The DC ESS.The DC ESS.

The complete DC network.The complete DC network.

The AC ESS.The AC ESS.

The AC and DC ESS.The AC and DC ESS.

In case of avionics bay smoke, GEN 1 LINE pb is

selected OFF.

Wh t ill h ?

In case of avionics bay smoke, GEN 1 LINEIn case of avionics bay smoke, GEN 1 LINE pbpb isis

selected OFF.selected OFF.

What will happen?What will happen?

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What will happen?What will happen?What will happen?

All warnings will be reset.All warnings will be reset.

The smoke in the avionic bay will beThe smoke in the avionic bay will beevacuated.evacuated.

GEN1 will be disconnected from theGEN1 will be disconnected from the

network.network.

Fire extinguisher bottle will be armed.Fire extinguisher bottle will be armed.

According to these indications, which statement istrue ?

According to these indications, which statement isAccording to these indications, which statement is

true ?true ?

8/21/2019 54806217 Airbus CBTquiz1


Both battery voltages are above theBoth battery voltages are above the

minimum of 20 V.minimum of 20 V.

Both battery voltages are below theBoth battery voltages are below theminimum of 25.5 V.minimum of 25.5 V.

I can only check the battery voltages onI can only check the battery voltages on

the ECAM ELEC page.the ECAM ELEC page.

I can only check the battery voltages, withI can only check the battery voltages, with

batteries on.batteries on.

You want to recharge the batteries.How do you proceed?

You want to recharge the batteries. You want to recharge the batteries.

How do you proceed?How do you proceed?

8/21/2019 54806217 Airbus CBTquiz1


y p

External power is available. I only have toExternal power is available. I only have to

switch the batteries to on and they will beswitch the batteries to on and they will be

charged.charged.

I have to switch the external power andI have to switch the external power and

the batteries to on and the batteries willthe batteries to on and the batteries willbe charged.be charged.

I have to switch the external power to ONI have to switch the external power to ON

and the batteries will be charged.and the batteries will be charged.

I have to call a mechanic because theI have to call a mechanic because the

batteries can only be charged bybatteries can only be charged by

maintenance.maintenance.

What is the meaning of the green AVAIL light ?

What is the meaning of the green AVAIL light ?What is the meaning of the green AVAIL light ?

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The external power is plugged in and theThe external power is plugged in and the

voltage and frequency parameters arevoltage and frequency parameters are

normal.normal.

The external power is plugged in.The external power is plugged in.

The external power panel door has beenThe external power panel door has been

opened.opened.

The AVAIL light always illuminates onThe AVAIL light always illuminates on

ground.ground.

After having switched the external power to ON,

you get the following indications. How do youinterpret the amber generator parameters and the

After having switched the external power to ON,After having switched the external power to ON,

you get the following indications. How do youyou get the following indications. How do you

interpret the amber generator parameters and theinterpret the amber generator parameters and the

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generator fault lights ?generator fault lights ?generator fault lights ?

You have to switch the generators to ON. You have to switch the generators to ON.

A failure has been detected. TheA failure has been detected. The

generators will not be able to supply thegenerators will not be able to supply theelectrical system after engine startelectrical system after engine start

There is an internal self test in progress.There is an internal self test in progress.

The fault lights and the amber indicationsThe fault lights and the amber indications

should disappear after 30 seconds.should disappear after 30 seconds.

On ground these indications are normalOn ground these indications are normal

when the engines are not running.when the engines are not running.

Both batteries are now being charged by the

external power unit.Approximately how long does the charging process

Both batteries are now being charged by theBoth batteries are now being charged by the

external power unit.external power unit.

Approximately how long does the charging processApproximately how long does the charging process

t k ?

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take ?take ?take ?

10 minutes10 minutes

One hour One hour

20 minutes20 minutes

Several hoursSeveral hours

After 20 minutes you check the ECAM ELEC page

again.

Which statement is true ?

After 20 minutes you check the ECAM ELEC pageAfter 20 minutes you check the ECAM ELEC page

again.again.

Which statement is true ?Which statement is true ?

8/21/2019 54806217 Airbus CBTquiz1


Which statement is true ?Which statement is true ?Which statement is true ?

Both battery voltages are still below theBoth battery voltages are still below the

minimum voltage.minimum voltage.

To check the battery voltages I have toTo check the battery voltages I have toswitch them OFF first.switch them OFF first.

To check the battery voltages I have toTo check the battery voltages I have to

disconnect external power first.disconnect external power first.

Both battery voltages are now above theBoth battery voltages are now above the

minimum voltage.minimum voltage.

You have started the APU.

Observe ECAM ELEC page !Why is the electrical system still supplied by

You have started the APU. You have started the APU.

Observe ECAM ELEC page !Observe ECAM ELEC page !

Why is the electrical system still supplied byWhy is the electrical system still supplied by

t l l ?t l l ?

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external power only ?external power only ?external power only ?

External power was connected first.External power was connected first.

External power has priority over the APUExternal power has priority over the APUgenerator.generator.

The APU generator is still switched off.The APU generator is still switched off.

The external power voltage is more stable.The external power voltage is more stable.

The APU generator is supplying the electrical

system.By the way, do you know the order of priority for

th diff t t ?

The APU generator is supplying the electricalThe APU generator is supplying the electrical

system.system.

By the way, do you know the order of priority forBy the way, do you know the order of priority for

th diff t t ?the different generators ?

8/21/2019 54806217 Airbus CBTquiz1


the different generators ?the different generators ?the different generators ?

engines, external power, APU.engines, external power, APU.

APU, engines, external power.APU, engines, external power.

external power, engines, APU.external power, engines, APU.

APU, external power, engines.APU, external power, engines.

On the ELEC Panel, you have lifted the IDG red

guard.

How do you disconnect the IDG now ?

On the ELEC Panel, you have lifted the IDG redOn the ELEC Panel, you have lifted the IDG red

guard.guard.

How do you disconnect the IDG now ?How do you disconnect the IDG now ?

8/21/2019 54806217 Airbus CBTquiz1


How do you disconnect the IDG now ?yy

I push the disconnect button and releaseI push the disconnect button and release

it immediately in order to prevent theit immediately in order to prevent the

disconnect mechanism from beingdisconnect mechanism from being

damaged.damaged.

I push the disconnect button until theI push the disconnect button until the

GEN FAULT light comes on and then forGEN FAULT light comes on and then forat least 3 more seconds in order to ensureat least 3 more seconds in order to ensure

the disconnection.the disconnection.

I push the disconnect button for at leastI push the disconnect button for at least

10 seconds to ensure the disconnection.10 seconds to ensure the disconnection.

I push the disconnect button until theI push the disconnect button until the

GEN FAULT light comes on but not moreGEN FAULT light comes on but not more

than 3 seconds otherwise the disconnectthan 3 seconds otherwise the disconnect

mechanism may be damaged.mechanism may be damaged.

Is the ELEC ECAM system page in accordance withthe both engines running electrical configuration ?

Is the ELEC ECAM system page in accordance withIs the ELEC ECAM system page in accordance with

the both engines running electrical configuration ?the both engines running electrical configuration ?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Yes.

No. The APU should continue poweringNo. The APU should continue poweringthe aircraft until crew switch it off.the aircraft until crew switch it off.

No. GEN1 should supply AC1 and AC2.No. GEN1 should supply AC1 and AC2.

No. GEN2 should supply AC1 and AC2.No. GEN2 should supply AC1 and AC2.

At the gate, with both engines shut down, is thisECAM ELEC page configuration correct ?

At the gate, with both engines shut down, is thisAt the gate, with both engines shut down, is this

ECAM ELEC page configuration correct ?ECAM ELEC page configuration correct ?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Yes.

No.No.

The crew should shut down one engine atThe crew should shut down one engine at

a time to reach this configuration.a time to reach this configuration.

The crew should select EXT POWER ON.The crew should select EXT POWER ON.

You are at the gate, APU GEN is supplying the

network, the EXT POWER is plugged in.What will happen when EXT POWER is selected

ON?

You are at the gate, APU GEN is supplying the You are at the gate, APU GEN is supplying the

network, the EXT POWER is plugged in.network, the EXT POWER is plugged in.

What will happen when EXT POWER is selectedWhat will happen when EXT POWER is selected

ON?ON?

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ON?ON?ON?

The APU GEN will be disconnected andThe APU GEN will be disconnected and

will stop.will stop.

The EXT POWER will supply the A/CThe EXT POWER will supply the A/Cnetwork.network.

The APU and ground power will bothThe APU and ground power will both

supply the A/C network .supply the A/C network .

The transfer between APU supply andThe transfer between APU supply and

ground power will take place only afterground power will take place only after

depressing the APU/GEN pbdepressing the APU/GEN pb swsw to stopto stop

the APU supply.the APU supply.

GEN 1 is now inoperative due to the ECAM

procedure application following an IDG OIL LO PRcaution.

Is the associated AC BUS still available?

GEN 1 is now inoperative due to the ECAMGEN 1 is now inoperative due to the ECAM

procedure application following an IDG OIL LO PRprocedure application following an IDG OIL LO PR

caution.caution.

Is the associated AC BUS still available?Is the associated AC BUS still available?

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Is the associated AC BUS still available?Is the associated AC BUS still available?Is the associated AC BUS still available?

Yes. AC ESS is supplying the AC 1. Yes. AC ESS is supplying the AC 1.

Yes. GEN 2 has taken over. Yes. GEN 2 has taken over.

No. GEN 2 will be disconnected from ACNo. GEN 2 will be disconnected from AC

BUS 2 within 10 minutes.BUS 2 within 10 minutes.

No. APU must be started to recover ACNo. APU must be started to recover AC

BUS 1.BUS 1.

When executing ECAM action following an IDG OIL

LO PR, the crew will have to hold IDG pb sw

pressed for:

When executing ECAM action following an IDG OILWhen executing ECAM action following an IDG OIL

LO PR, the crew will have to hold IDG pbLO PR, the crew will have to hold IDG pb swsw

pressed for:pressed for:

8/21/2019 54806217 Airbus CBTquiz1


Minimum 3 seconds.Minimum 3 seconds.

Maximum 3 seconds.Maximum 3 seconds.

Until fault amber light goes out.Until fault amber light goes out.

No time limit.No time limit.

In case of GEN 2 OVERLOAD ECAM caution, howdo you off load the generator?

In case of GEN 2 OVERLOAD ECAM caution, howIn case of GEN 2 OVERLOAD ECAM caution, how

do you off load the generator?do you off load the generator?

8/21/2019 54806217 Airbus CBTquiz1


By starting the APU to connect a thirdBy starting the APU to connect a third

generator to share the load.generator to share the load.

By switching OFF the galley.By switching OFF the galley.

By transferring load on GEN1 in order toBy transferring load on GEN1 in order to

keep the galley operating.keep the galley operating.

Following a GEN 2 OVERLOAD and the shedding ofthe galley is the ELEC page correct?

Following a GEN 2 OVERLOAD and the shedding ofFollowing a GEN 2 OVERLOAD and the shedding of

the galley is the ELEC page correct?the galley is the ELEC page correct?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Yes.

No. The GEN overload should stay amber.No. The GEN overload should stay amber.

No. The GALLEY SHED message shouldNo. The GALLEY SHED message should

be removed.be removed.

Which of those area, has NO fire extinguishingsystem installed?

Which of those area, has NO fire extinguishingWhich of those area, has NO fire extinguishing

system installed?system installed?

CabinCabin

8/21/2019 54806217 Airbus CBTquiz1


Avionic bay.Avionic bay.

Cargo compartments.Cargo compartments.

Engine / APU.Engine / APU.

Cabin.Cabin.

Please identify which of those area has a FIRE andOVERHEAT DETECTION system installed.

Please identify which of those area has a FIRE andPlease identify which of those area has a FIRE and

OVERHEAT DETECTION system installed.OVERHEAT DETECTION system installed.

CabinCabin.

8/21/2019 54806217 Airbus CBTquiz1


Avionic bay.Avionic bay.

Cargo compartments.Cargo compartments.

Engine / APU.Engine / APU.

Cabin.Cabin.

It is the first flight of the day.

Before performing the APU fire test, you have to

check that...

It is the first flight of the day.It is the first flight of the day.

Before performing the APU fire test, you have toBefore performing the APU fire test, you have to

check that...check that...

8/21/2019 54806217 Airbus CBTquiz1


The APU FIREThe APU FIRE pbpb is in and guarded andis in and guarded and

AC power is supplied.AC power is supplied.

The APU FIREThe APU FIRE

pbpb

is in and guarded andis in and guarded and

the APU is running.the APU is running.

The APU FIREThe APU FIRE pbpb is in with the guard inis in with the guard in

the UP position and the AGENT light isthe UP position and the AGENT light is

extinguished.extinguished.

The APU FIREThe APU FIRE pbpb is in and guardedis in and guarded

and the AGENT light is extinguished.and the AGENT light is extinguished.

The aircraft is not yet supplied with AC power.Can you perform the APU FIRE test?

The aircraft is not yet supplied with AC power.The aircraft is not yet supplied with AC power.

Can you perform the APU FIRE test?Can you perform the APU FIRE test?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Yes.

No.No.

In this case, during the preliminary cockpit

preparation the APU FIRE test will trigger the

following indications:

In this case, during the preliminary cockpitIn this case, during the preliminary cockpit

preparation the APU FIRE test will trigger thepreparation the APU FIRE test will trigger the

following indications:following indications:

8/21/2019 54806217 Airbus CBTquiz1


On the FIRE Control Panel, the APU FIREOn the FIRE Control Panel, the APU FIRE

light, the SQUIB and DISCH lights willlight, the SQUIB and DISCH lights will

illuminate. Additionally, APU FIREilluminate. Additionally, APU FIRE

warning will be triggered on ECAM.warning will be triggered on ECAM.

On the FIRE Control Panel, the APU FIREOn the FIRE Control Panel, the APU FIRE

red light and SQUIB light will illuminate.red light and SQUIB light will illuminate.

But the APU FIRE warning will not beBut the APU FIRE warning will not be

triggered on ECAM.triggered on ECAM.

No test is possible until AC power isNo test is possible until AC power is

connected on the Electrical network.connected on the Electrical network.

The APU FIRE test is successful.

The APU FIRE test is successful.The APU FIRE test is successful.

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

Does the APU fire test on battery trigger the CRCand MASTER WARN?

Does the APU fire test on battery trigger the CRCDoes the APU fire test on battery trigger the CRC

and MASTER WARN?and MASTER WARN?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Yes.

No.No.

With the following indication on ECAM, what is theFIRE DETECTION status?

With the following indication on ECAM, what is theWith the following indication on ECAM, what is the

FIRE DETECTION status?FIRE DETECTION status?

FDU

8/21/2019 54806217 Airbus CBTquiz1


One fire detection loop has failed.One fire detection loop has failed.

Fire detection for both engines is stillFire detection for both engines is still

available.available.

Both fire detection loops of engine 1 haveBoth fire detection loops of engine 1 have

failed. Fire detection for engine 1 isfailed. Fire detection for engine 1 isinoperative.inoperative.

One fire detection loop of engine 1 hasOne fire detection loop of engine 1 has

failed. Fire detection for engine 1 is stillfailed. Fire detection for engine 1 is still

available.available.

One fire detection loop of engine 1 hasOne fire detection loop of engine 1 has

failed. Fire detection for engine 1 isfailed. Fire detection for engine 1 is

inoperative.inoperative.

According to this ECAM E/WD page, the associatedprocedure is

According to this ECAM E/WD page, the associatedAccording to this ECAM E/WD page, the associated

procedure isprocedure is

8/21/2019 54806217 Airbus CBTquiz1


An indication presenting the FWD CARGOAn indication presenting the FWD CARGO

SMOKE condition only.SMOKE condition only.

To press the illuminated red FWD SMOKETo press the illuminated red FWD SMOKE

DISCH pb.DISCH pb.

To lift the red guard and press the DISCHTo lift the red guard and press the DISCH

pb.pb.

This is an automaticThis is an automatic fonctionfonction and youand you

have to press FWD SMOKE pb to confirm.have to press FWD SMOKE pb to confirm.

On the CARGO SMOKE control PANEL both DISCHlights illuminated mean that:

On the CARGO SMOKE control PANEL both DISCHOn the CARGO SMOKE control PANEL both DISCH

lights illuminated mean that:lights illuminated mean that:

8/21/2019 54806217 Airbus CBTquiz1


The FWD and AFT fire bottles have bothThe FWD and AFT fire bottles have both

been discharged into their associatedbeen discharged into their associatedcompartment.compartment.

Now there is no longer any availableNow there is no longer any available

agent which can be discharged in eitheragent which can be discharged in either

the FWD or the AFT cargo compartment.the FWD or the AFT cargo compartment.

The FWD and AFT fire bottles have bothThe FWD and AFT fire bottles have both

been discharged into the FWDbeen discharged into the FWD compartcompart--

mentment..

There is only one fire bottle which hasThere is only one fire bottle which has

been discharged into both cargobeen discharged into both cargo

compartments.compartments.

According to these indications, which flight controllaw is active ?

According to these indications, which flight controlAccording to these indications, which flight control

law is active ?law is active ?

8/21/2019 54806217 Airbus CBTquiz1


Normal LawNormal Law

Alternate LawAlternate Law

Direct LawDirect Law

Mechanical Back UpMechanical Back Up




8/21/2019 54806217 Airbus CBTquiz1






Observe the PFD.Without any sidestick inputs...

Observe the PFD.Observe the PFD.

Without anyWithout any sidesticksidestick inputs...inputs...

8/21/2019 54806217 Airbus CBTquiz1


The aircraftThe aircraft’’s attitude wills attitude will sstay constant.tay constant.

The pitch will stay constant, theThe pitch will stay constant, the

bank angle will slowly decrease.bank angle will slowly decrease.

The bank angle will stayThe bank angle will stay constantconstant, the, the

pitch will slowly decrease.pitch will slowly decrease.

The aircraftThe aircraft’’s attitude will slowly tends attitude will slowly tend

towardstowards ““wings levelwings level”” andand ““pitch 0pitch 0””..

According to the following indications...

According to the following indications...According to the following indications...

8/21/2019 54806217 Airbus CBTquiz1


The Alpha Floor protection has beenThe Alpha Floor protection has been

triggered.triggered.

The Load Factor Limitation has beenThe Load Factor Limitation has been


There is no protection triggered yet.There is no protection triggered yet.

The High Angle Of Attack protection hasThe High Angle Of Attack protection has

been triggered.been triggered.

Let’s assume, you have set idle power and pulled

the sidestick back to maintain altitude. Observe the

PFD. If you release the sidestick now...

LetLet’’s assume, you have set idle power and pulleds assume, you have set idle power and pulled

thethe sidesticksidestick back to maintain altitude. Observe theback to maintain altitude. Observe the

PFD. If you release thePFD. If you release the sidesticksidestick now...now...

8/21/2019 54806217 Airbus CBTquiz1


The aircraft will descend at 150The aircraft will descend at 150 ktskts..

The aircraft will maintain altitude untilThe aircraft will maintain altitude until

120120 ktskts are reached .are reached .

The aircraft will maintain altitude until aThe aircraft will maintain altitude until a

stall occurs.stall occurs.

The aircraft will descend at 135The aircraft will descend at 135 ktskts..

According to these indications...

According to these indications...According to these indications...

8/21/2019 54806217 Airbus CBTquiz1


The Alpha Floor protection has beenThe Alpha Floor protection has been


The Load Factor Limitation has beenThe Load Factor Limitation has been


There is no triggered protection.There is no triggered protection.

The High Angle Of Attack protection hasThe High Angle Of Attack protection has

been triggered.been triggered.

According to these indications, if the sidestick isheld in the full back position...

According to these indications, if theAccording to these indications, if the sidesticksidestick isis

held in the full back position...held in the full back position...

8/21/2019 54806217 Airbus CBTquiz1


The speed will fall below 120The speed will fall below 120 ktskts..

The airplane might stall.The airplane might stall.

The speed will fall below 120The speed will fall below 120 ktskts..

To avoid a stall, climb power will beTo avoid a stall, climb power will beautomatically set.automatically set.

The High Angle Of Attack protection willThe High Angle Of Attack protection will

override theoverride the sidesticksidestick input. The pitch willinput. The pitch will

be lowered to maintain 120be lowered to maintain 120 ktskts..

The speed will fall further.The speed will fall further.

At 114At 114 ktskts the pitch will be lowered tothe pitch will be lowered to

maintain 114maintain 114 ktskts..

Observe the PFD.Which statement is true ?

Observe the PFD.Observe the PFD.


8/21/2019 54806217 Airbus CBTquiz1


The Alpha Floor protection hasThe Alpha Floor protection has

automatically set CLB power.automatically set CLB power.

The Alpha Floor protection hasThe Alpha Floor protection has

automatically set TO/GA power.automatically set TO/GA power.

The Alpha Floor protection will overrideThe Alpha Floor protection will override

sidesticksidestick inputs. The nose will beinputs. The nose will be

lowered.lowered.

A stall is detected.A stall is detected.

To fly a coordinated turn...

To fly a coordinated turn...To fly a coordinated turn...

8/21/2019 54806217 Airbus CBTquiz1


No rudder inputs are required.No rudder inputs are required.

You have to center the sideslip indicator You have to center the sideslip indicator

with the rudder pedals.with the rudder pedals.

Only small rudder inputs are required.Only small rudder inputs are required.

In Normal Law, is there a maximum pitch attitude ?

In Normal Law, is there a maximum pitch attitude ?In Normal Law, is there a maximum pitch attitude ?

8/21/2019 54806217 Airbus CBTquiz1


Yes, indicated by the green dashes (A). Yes, indicated by the green dashes (A).

Yes, indicated by the green dashes (B). Yes, indicated by the green dashes (B).

No.No.

Yes, pitch is limited to 20 Yes, pitch is limited to 20ºº nose up.nose up.

AA

BB

In Normal Law, is there a maximum bank angle ?

In Normal Law, is there a maximum bank angle ?In Normal Law, is there a maximum bank angle ?

aa

8/21/2019 54806217 Airbus CBTquiz1


No.No.

Yes, indicated by the green dashes (b). Yes, indicated by the green dashes (b).

Yes, indicated by the white dashes (a). Yes, indicated by the white dashes (a).

Yes, bank is limited to 80 Yes, bank is limited to 80ºº..

bb

How do you interpret the amber crosses on thePFD ?

How do you interpret the amber crosses on theHow do you interpret the amber crosses on the

PFD ?PFD ?

8/21/2019 54806217 Airbus CBTquiz1


TheThe autotrimautotrim is lost. You have to useis lost. You have to use

manual pitch trim.manual pitch trim.

The ailerons are controlled directly by theThe ailerons are controlled directly by the

sidestickssidesticks..

The bank angle limit protection is lost.The bank angle limit protection is lost.

The bank angle protection is active.The bank angle protection is active.

The CPT’s sidestick is deflected fully left and the

FO’s sidestick is simultaneously deflected fullyright.

Which indications do you expect ?

TheThe CPTCPT’’ss sidesticksidestick is deflected fully left and theis deflected fully left and the

FOFO’’ss sidesticksidestick is simultaneously deflected fullyis simultaneously deflected fully

right.right.

Which indications do you expect ?Which indications do you expect ?

8/21/2019 54806217 Airbus CBTquiz1


If both pilots deflect their sidesticks fully back...

If both pilots deflect theirIf both pilots deflect their sidestickssidesticks fully back...fully back...

8/21/2019 54806217 Airbus CBTquiz1


TheThe ““pitch uppitch up”” order is twice as great asorder is twice as great as

compared only one stick deflected.compared only one stick deflected.

TheThe ““pitch uppitch up”” order is 1.5 times greater order is 1.5 times greater

as compared to only one stick deflected.as compared to only one stick deflected.

No inputs are sent to the flight controlNo inputs are sent to the flight control

computers unless one pilot presses thecomputers unless one pilot presses the

take overtake over pbpb on his stick.on his stick.

TheThe ““pitch uppitch up”” order is equal to a singleorder is equal to a single

stick fully deflected.stick fully deflected.

If the FO presses the take over pb...

If the FO presses the take overIf the FO presses the take over pbpb......

8/21/2019 54806217 Airbus CBTquiz1


The CPT is unable to reThe CPT is unable to re--activate hisactivate his

sidesticksidestick..

TheThe CPTCPT’’ss sidesticksidestick is still active. It willis still active. It will

be debe de--activated after 40activated after 40 secssecs..

The CPT can reThe CPT can re--activate hisactivate his sidesticksidestick byby

pressing the take overpressing the take over pbpb for more thanfor more than

4040 secssecs..

The CPT can reThe CPT can re--activate hisactivate his sidesticksidestick

immediately by pressing his take overimmediately by pressing his take over pbpb..

FOFOCPTCPT

Let’s assume the FO presses his take over pb andreleases it after more than 40 secs...

LetLet’’s assume the FO presses his take overs assume the FO presses his take over pbpb andand

releases it after more than 40releases it after more than 40 secssecs......

8/21/2019 54806217 Airbus CBTquiz1


TheThe CPTCPT’’ss sidesticksidestick is deis de--activated unlessactivated unless

he presses his take overhe presses his take over pbpb..

The CPT is unable to reThe CPT is unable to re--activate hisactivate his

sidesticksidestick for the rest of the flight.for the rest of the flight.

BothBoth sidestickssidesticks are active.are active.

TheThe CPTCPT’’ss sidesticksidestick is active as long asis active as long as

the FOthe FO’’ss sidesticksidestick is in neutral positionis in neutral position

FOFOCPTCPT

40 sec40 sec40 sec

With either AP engaged, which statement is true ?

With either AP engaged, which statement is true ?With either AP engaged, which statement is true ?

8/21/2019 54806217 Airbus CBTquiz1


BothBoth sidestickssidesticks are locked in neutralare locked in neutral

position. The lock can not be overriddenposition. The lock can not be overridden

BothBoth sidestickssidesticks are deare de--activated untilactivated until

the AP is disengaged.the AP is disengaged.


position. By applying a certain force, theposition. By applying a certain force, the

lock can be overridden but the APlock can be overridden but the AP

remains engaged.remains engaged.


position. By applying a certain force, theposition. By applying a certain force, the

lock can be overridden and the AP islock can be overridden and the AP is

disengaged.disengaged.

What will happen next ?

What will happen next ?What will happen next ?

8/21/2019 54806217 Airbus CBTquiz1


The left SPLR 3 will be retracted, the rightThe left SPLR 3 will be retracted, the right

SPLR 3 will be inhibited to preventSPLR 3 will be inhibited to prevent

asymmetry.asymmetry.

The right SPLR 3 will be extended toThe right SPLR 3 will be extended to

prevent asymmetry.prevent asymmetry.

Left SPLR 3 remains extended, spoilerLeft SPLR 3 remains extended, spoiler

operation is not possible anymore.operation is not possible anymore.

After a turn, you have the following message. Whathappened ?

After a turn, you have the following message. WhatAfter a turn, you have the following message. What

happened ?happened ?

8/21/2019 54806217 Airbus CBTquiz1


The left SPRL 3 failed to extend.The left SPRL 3 failed to extend.

The right SPRL 3 failed to extend.The right SPRL 3 failed to extend.

The left SPRL 3 failed to retract.The left SPRL 3 failed to retract.

The right SPRL 3 failed to retract.The right SPRL 3 failed to retract.

What will happen just before the speed reaches VFESpeed (red barber pole)?

What will happen just before the speed reaches VFEWhat will happen just before the speed reaches VFE

Speed (red barber pole)?Speed (red barber pole)?

8/21/2019 54806217 Airbus CBTquiz1


Auto flap retraction at 210Auto flap retraction at 210 ktskts..

Auto flap and slat retraction at 210Auto flap and slat retraction at 210 ktskts..

High Speed protection will become active,High Speed protection will become active,

the autopilot will increase the pitch.the autopilot will increase the pitch.

High Speed protection will become active,High Speed protection will become active,

thethe autothrustautothrust will reduce thrust.will reduce thrust.

The message WING TIP BRK ON appears on theE/WD. What does it mean?

The message WING TIP BRK ON appears on theThe message WING TIP BRK ON appears on the

E/WD. What does it mean?E/WD. What does it mean?

8/21/2019 54806217 Airbus CBTquiz1


F/CTL FLAPS LOCKED

-WING TIP BRK ON

MAX SPEED . . . . . . . .

A hydraulic device locks the flaps in their A hydraulic device locks the flaps in their

present position.present position.

To reduce structural stress, the slatsTo reduce structural stress, the slats

movement is being slowed down throughmovement is being slowed down throughthe wing tip brakes.the wing tip brakes.

To avoid asymmetry, the outer slats areTo avoid asymmetry, the outer slats are

locked in their present position.locked in their present position.

Because of the locked flaps, the wing tipBecause of the locked flaps, the wing tip

brake also lock the slats.brake also lock the slats.

Which control surfaces are used for the mechanicalbackup?

Which control surfaces are used for the mechanicalWhich control surfaces are used for the mechanical

backup?backup?

8/21/2019 54806217 Airbus CBTquiz1


Ailerons and rudder.Ailerons and rudder.

THS and rudder.THS and rudder.

Elevator and ailerons.Elevator and ailerons.

THS and elevator.THS and elevator.

How many actuators are provided to control the

ailerons and how many hydraulic sources supply

these actuators?

How many actuators are provided to control theHow many actuators are provided to control the

ailerons and how many hydraulic sources supplyailerons and how many hydraulic sources supply

these actuators?these actuators?

8/21/2019 54806217 Airbus CBTquiz1


2 hydraulic sources with 4 actuators2 hydraulic sources with 4 actuators

1 hydraulic source with 2 actuators1 hydraulic source with 2 actuators

4 hydraulic sources with 44 hydraulic sources with 4 actuatorsactuators

3 hydraulic sources with 4 actuators3 hydraulic sources with 4 actuators

What does the white cross indicate?

What does the white cross indicate?What does the white cross indicate?

8/21/2019 54806217 Airbus CBTquiz1


It is an indicator for theIt is an indicator for the sidesticksidestick

deflections during the flight controldeflections during the flight control

check.check.

It is an indicator for the control surfacesIt is an indicator for the control surfaces

deflections during the flight controldeflections during the flight controlcheck.check.

It is an indication for the rudder pedalsIt is an indication for the rudder pedals

deflections during the flight controldeflections during the flight control

check.check.

In Normal Law, if one sidestick is rapidly pulled

fully back, can the airplane’s maximum allowable

“G” load be exceeded ?

In Normal Law, if oneIn Normal Law, if one sidesticksidestick is rapidly pulledis rapidly pulled

fully back, can the airplanefully back, can the airplane’’s maximum allowables maximum allowable

““GG”” load be exceeded ?load be exceeded ?

8/21/2019 54806217 Airbus CBTquiz1


Yes. Rapid Yes. Rapid sidesticksidestick deflection mustdeflection must

never be made.never be made.

Yes, until maximum pitch attitude is Yes, until maximum pitch attitude is

reached.reached.

No. At maximumNo. At maximum ““GG”” load, theload, the sidestickssidesticks

are deare de--activated for 5 seconds.activated for 5 seconds.

No. The load factor limitation overridesNo. The load factor limitation overrides

sidesticksidestick commands to avoid excessivecommands to avoid excessive

““GG”” loads.loads.

With the sidestick fully forward, what will be themaximum airspeed indication?

With theWith the sidesticksidestick fully forward, what will be thefully forward, what will be the

maximum airspeed indication?maximum airspeed indication?

8/21/2019 54806217 Airbus CBTquiz1


According to these indications, if you release thesidestick now...

According to these indications, if you release theAccording to these indications, if you release the

sidesticksidestick now...now...

8/21/2019 54806217 Airbus CBTquiz1


The bank angle will automatically returnThe bank angle will automatically return

to 33to 33ºº..

The bank angle will not change.The bank angle will not change.

The bank angle will return to wings level,The bank angle will return to wings level,

because the bank protection is active.because the bank protection is active.

The bank angle will return to 20The bank angle will return to 20ºº..

In Normal Law, what is the maximum bank angleyou can reach with the sidestick fully deflected ?

In Normal Law, what is the maximum bank angleIn Normal Law, what is the maximum bank angle

you can reach with theyou can reach with the sidesticksidestick fully deflected ?fully deflected ?

8/21/2019 54806217 Airbus CBTquiz1


3333ºº

There is no bank limitation.There is no bank limitation.

8080 ºº

6767 ºº




8/21/2019 54806217 Airbus CBTquiz1


Normal Law.Normal Law.

Alternate Law.Alternate Law.

Direct Law.Direct Law.

Mechanical Back Up.Mechanical Back Up.




8/21/2019 54806217 Airbus CBTquiz1






Which ECAM FUEL page corresponds to thisE/WD?

Which ECAM FUEL page corresponds to thisWhich ECAM FUEL page corresponds to this

E/WD?E/WD?

8/21/2019 54806217 Airbus CBTquiz1


Which ECAM FUEL page corresponds to thisE/WD?

Which ECAM FUEL page corresponds to thisWhich ECAM FUEL page corresponds to this

E/WD?E/WD?

8/21/2019 54806217 Airbus CBTquiz1


You are in cruise and according to those

indications, a failure occurred in the fuel system.

Why didn't you get a master caution or a chime?

You are in cruise and according to those You are in cruise and according to those

indications, a failure occurred in the fuel system.indications, a failure occurred in the fuel system.

Why didn't you get a master caution or a chime?Why didn't you get a master caution or a chime?

8/21/2019 54806217 Airbus CBTquiz1


The fuel system is not connected to theThe fuel system is not connected to the

Flight Warning Computer.Flight Warning Computer.

Inner tank pump failures never trigger aInner tank pump failures never trigger a

warning because the fuel can be used bywarning because the fuel can be used by

gravity feeding.gravity feeding.

Due to redundancy, loss of one pump isDue to redundancy, loss of one pump is

only level 1 caution.only level 1 caution.

You are in cruise and according to those

indications, a failure occurred in the fuel system.

Why didn't you get a master caution or a chime?

You are in cruise and according to those You are in cruise and according to those

indications, a failure occurred in the fuel system.indications, a failure occurred in the fuel system.

Why didn't you get a master caution or a chime?Why didn't you get a master caution or a chime?

8/21/2019 54806217 Airbus CBTquiz1


The fuel system is not connected to theThe fuel system is not connected to the

Flight Warning Computer.Flight Warning Computer.

Due to redundancy, loss of one pump isDue to redundancy, loss of one pump is

only level 1 caution.only level 1 caution.

Inner tank pump failures never trigger aInner tank pump failures never trigger a

warning because the fuel can be used bywarning because the fuel can be used by


In case of R TK PUMP 1 + 2 LO PR, can you still usefuel out of the right inner tank?

In case of R TK PUMP 1 + 2 LO PR, can you still useIn case of R TK PUMP 1 + 2 LO PR, can you still use

fuel out of the right inner tank?fuel out of the right inner tank?

8/21/2019 54806217 Airbus CBTquiz1


Yes, the fuel of this tank is available by Yes, the fuel of this tank is available by


No, the fuel of this tank is lost.No, the fuel of this tank is lost.

Yes, the fuel flows via transfer valves to Yes, the fuel flows via transfer valves to

the outer tank.the outer tank.

Yes, the fuel flows via spill valves to the Yes, the fuel flows via spill valves to the

center tank.center tank.

In case of R TK PUMP 1 + 2 LO PR, can you still usefuel out of the right inner tank?

In case of R TK PUMP 1 + 2 LO PR, can you still useIn case of R TK PUMP 1 + 2 LO PR, can you still use

fuel out of the right inner tank?fuel out of the right inner tank?

8/21/2019 54806217 Airbus CBTquiz1


Yes, the fuel of this tank is available by Yes, the fuel of this tank is available by


No, the fuel of this tank is lost.No, the fuel of this tank is lost.

Yes, the fuel flows via transfer valves to Yes, the fuel flows via transfer valves to


Yes, the fuel flows via spill valves to the Yes, the fuel flows via spill valves to the

center tank.center tank.

According to this SD FUEL page indications, onlythe Center Tank Pumps are feeding the engines.

According to this SD FUEL page indications, onlyAccording to this SD FUEL page indications, only

the Center Tank Pumps are feeding the engines.the Center Tank Pumps are feeding the engines.

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

According to this SD FUEL page indications, onlythe Center Tank Pumps are feeding the engines.

According to this SD FUEL page indications, onlyAccording to this SD FUEL page indications, only

the Center Tank Pumps are feeding the engines.the Center Tank Pumps are feeding the engines.

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

According to this FUEL SD page indications, whichpumps are feeding the engines?

According to this FUEL SD page indications, whichAccording to this FUEL SD page indications, which

pumps are feeding the engines?pumps are feeding the engines?

8/21/2019 54806217 Airbus CBTquiz1


The Center Tank Pumps alone.The Center Tank Pumps alone.

The Center Tank Pumps and the innerThe Center Tank Pumps and the inner

tank pumps.tank pumps.

The inner Tank Pumps alone.The inner Tank Pumps alone.

According to this FUEL SD page indications, whichpumps are feeding the engines?

According to this FUEL SD page indications, whichAccording to this FUEL SD page indications, which

pumps are feeding the engines?pumps are feeding the engines?

8/21/2019 54806217 Airbus CBTquiz1


The Center Tank Pumps alone.The Center Tank Pumps alone.

The Center Tank Pumps and the innerThe Center Tank Pumps and the inner

tank pumps.tank pumps.

The inner Tank Pumps alone.The inner Tank Pumps alone.

Why has the fuel been transferred from the outer tothe inner tanks?

Why has the fuel been transferred from the outer toWhy has the fuel been transferred from the outer to

the inner tanks?the inner tanks?

8/21/2019 54806217 Airbus CBTquiz1


The temperature in the outer tank was tooThe temperature in the outer tank was too

low.low.

The center tank quantity is 0.The center tank quantity is 0.

The temperature in the inner tank was tooThe temperature in the inner tank was too

low.low.

The quantity in the inner tanks isThe quantity in the inner tanks is

approaching low level.approaching low level.

Why has the fuel been transferred from the outer tothe inner tanks?

Why has the fuel been transferred from the outer toWhy has the fuel been transferred from the outer to

the inner tanks?the inner tanks?

8/21/2019 54806217 Airbus CBTquiz1


The temperature in the outer tank was tooThe temperature in the outer tank was too

low.low.

The center tank quantity is 0.The center tank quantity is 0.

The temperature in the inner tank was tooThe temperature in the inner tank was too

low.low.

The quantity in the inner tanks isThe quantity in the inner tanks is

approaching low level.approaching low level.

On the ECAM E/WD page the message REFUELGappears in the MEMO. What does it mean?

On the ECAM E/WD page the message REFUELGOn the ECAM E/WD page the message REFUELG

appears in the MEMO. What does it mean?appears in the MEMO. What does it mean?

8/21/2019 54806217 Airbus CBTquiz1


The aircraft systems are ready to startThe aircraft systems are ready to start

refueling.refueling.

The refueling control panel door is notThe refueling control panel door is not

closed.closed.

Refueling is completed, the requiredRefueling is completed, the required

amount of fuel has been pumped into theamount of fuel has been pumped into the

tanks.tanks.

A reminder that you still have to refuel.A reminder that you still have to refuel.

On the ECAM E/WD page the message REFUELGappears in the MEMO. What does it mean?

On the ECAM E/WD page the message REFUELGOn the ECAM E/WD page the message REFUELG


8/21/2019 54806217 Airbus CBTquiz1


The aircraft systems are ready to startThe aircraft systems are ready to start


The refueling control panel door is notThe refueling control panel door is not

closed.closed.

Refueling is completed, the requiredRefueling is completed, the required

amount of fuel has been pumped into theamount of fuel has been pumped into the

tanks.tanks.

A reminder that you still have to refuel.A reminder that you still have to refuel.

On this ECAM FUEL SD page what does an amber-boxed FOB indication mean?

On this ECAM FUEL SD page what does an amber On this ECAM FUEL SD page what does an amber --

boxed FOB indication mean?boxed FOB indication mean?

8/21/2019 54806217 Airbus CBTquiz1


Not all the fuel on board is useableNot all the fuel on board is useable

anymore.anymore.

The fuel temperature exceeds a limit.The fuel temperature exceeds a limit.

A fuel imbalance has been detected.A fuel imbalance has been detected.

A disagreement between fuel measuredA disagreement between fuel measured

and fuel entered on the MCDU has beenand fuel entered on the MCDU has been

detected.detected.

On this ECAM FUEL SD page what does an amber-boxed FOB indication mean?

On this ECAM FUEL SD page what does an amber On this ECAM FUEL SD page what does an amber --

boxed FOB indication mean?boxed FOB indication mean?

8/21/2019 54806217 Airbus CBTquiz1


Not all the fuel on board is useableNot all the fuel on board is useable

anymore.anymore.

The fuel temperature exceeds a limit.The fuel temperature exceeds a limit.

A fuel imbalance has been detected.A fuel imbalance has been detected.

A disagreement between fuel measuredA disagreement between fuel measured

and fuel entered on the MCDU has beenand fuel entered on the MCDU has been

detected.detected.

On the ECAM FUEL SD page what does thisindication of a Center Tank Pump mean?

On the ECAM FUEL SD page what does thisOn the ECAM FUEL SD page what does this

indication of a Center Tank Pump mean?indication of a Center Tank Pump mean?

8/21/2019 54806217 Airbus CBTquiz1


It is switched on with the Mode SELIt is switched on with the Mode SEL pbpb inin

AUTO and supplying fuelAUTO and supplying fuel


MAN and supplying fuel.MAN and supplying fuel.


AUTO but not supplying fuel.AUTO but not supplying fuel.


MAN and CTR TK pump not supplyingMAN and CTR TK pump not supplying

fuel.fuel.

On the ECAM FUEL SD page what does thisindication of a Center Tank Pump mean?

On the ECAM FUEL SD page what does thisOn the ECAM FUEL SD page what does this

indication of a Center Tank Pump mean?indication of a Center Tank Pump mean?

8/21/2019 54806217 Airbus CBTquiz1



MAN and CTR TK pump not supplyingMAN and CTR TK pump not supplying

fuel.fuel.


AUTO and supplying fuelAUTO and supplying fuel


MAN and supplying fuel.MAN and supplying fuel.


AUTO but not supplying fuel.AUTO but not supplying fuel.

This is your ECAM FUEL page after engine

shutdown. You notice the transfer valves are open.

What are your actions to close them?

This is your ECAM FUEL page after engineThis is your ECAM FUEL page after engine

shutdown. You notice the transfer valves are open.shutdown. You notice the transfer valves are open.

What are your actions to close them?What are your actions to close them?

8/21/2019 54806217 Airbus CBTquiz1


You have to switch the inner tank pumps You have to switch the inner tank pumps

off.off.

You have to push the MODE SEL You have to push the MODE SEL pbpb swsw toto

manual.manual.

You have to open and then close the You have to open and then close the

crossfeedcrossfeed valve again.valve again.

There are no actions required. The valvesThere are no actions required. The valves

will close automatically during the nextwill close automatically during the next


This is your ECAM FUEL page after engine

shutdown. You notice the transfer valves are open.

What are your actions to close them?

This is your ECAM FUEL page after engineThis is your ECAM FUEL page after engine

shutdown. You notice the transfer valves are open.shutdown. You notice the transfer valves are open.

What are your actions to close them?What are your actions to close them?

8/21/2019 54806217 Airbus CBTquiz1


You have to switch the inner tank pumps You have to switch the inner tank pumps

off.off.

You have to push the MODE SEL You have to push the MODE SEL pbpb swsw toto

manual.manual.

You have to open and then close the You have to open and then close the

crossfeedcrossfeed valve again.valve again.

There are no actions required. The valvesThere are no actions required. The valves

will close automatically during the nextwill close automatically during the next


On the ECAM, the message OUTER TK FUEL XFRDappears in the MEMO. What does it mean?

On the ECAM, the message OUTER TK FUEL XFRDOn the ECAM, the message OUTER TK FUEL XFRD


8/21/2019 54806217 Airbus CBTquiz1


Fuel is transferred from the inner tank toFuel is transferred from the inner tank to


Fuel is transferred from the outer tank toFuel is transferred from the outer tank to

the inner tank.the inner tank.


the center tank.the center tank.

Fuel is transferred from the center tank toFuel is transferred from the center tank to


On the ECAM, the message OUTER TK FUEL XFRDappears in the MEMO. What does it mean?

On the ECAM, the message OUTER TK FUEL XFRDOn the ECAM, the message OUTER TK FUEL XFRD


8/21/2019 54806217 Airbus CBTquiz1




Fuel is transferred from the outer tank toFuel is transferred from the outer tank to



the center tank.the center tank.

Fuel is transferred from the center tank toFuel is transferred from the center tank to


What is the reason the center tank pumps switch

automatically off when the slats are extended for

take-off?

What is the reason the center tank pumps switchWhat is the reason the center tank pumps switch

automatically off when the slats are extended forautomatically off when the slats are extended for

taketake--off?off?

8/21/2019 54806217 Airbus CBTquiz1


To keep the center of gravity as low asTo keep the center of gravity as low as

possible.possible.

During takeDuring take--off, the center tank fuel isoff, the center tank fuel is

pumped to the rear to trim the aircraft.pumped to the rear to trim the aircraft.

To feed the 2 engines from 2 differentTo feed the 2 engines from 2 different

sources ( the inner tanks ).sources ( the inner tanks ).

What is the reason the center tank pumps switch

automatically off when the slats are extended for

take-off?

What is the reason the center tank pumps switchWhat is the reason the center tank pumps switch

automatically off when the slats are extended forautomatically off when the slats are extended for

taketake--off?off?

8/21/2019 54806217 Airbus CBTquiz1


To keep the center of gravity as low asTo keep the center of gravity as low as

possible.possible.

During takeDuring take--off, the center tank fuel isoff, the center tank fuel is

pumped to the rear to trim the aircraft.pumped to the rear to trim the aircraft.

To feed the 2 engines from 2 differentTo feed the 2 engines from 2 different

sources ( the inner tanks ).sources ( the inner tanks ).

What is the minimum fuel quantity for take-off?

What is the minimum fuel quantity for takeWhat is the minimum fuel quantity for take--off?off?

8/21/2019 54806217 Airbus CBTquiz1


1000 kg.1000 kg.

1500 kg.1500 kg.

2000 kg.2000 kg.

2500 kg.2500 kg.

What is the minimum fuel quantity for take-off?

What is the minimum fuel quantity for takeWhat is the minimum fuel quantity for take--off?off?

8/21/2019 54806217 Airbus CBTquiz1


2400 lbs.2400 lbs.

3300 lbs.3300 lbs.

4700 lbs.4700 lbs.

5300 lbs.5300 lbs.

The normal pressure for the hydraulic system is2000 psi

The normal pressure for the hydraulic system isThe normal pressure for the hydraulic system is

20002000 psipsi

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

What is the normal pressure in the hydraulicsystem?

What is the normal pressure in the hydraulicWhat is the normal pressure in the hydraulic

system?system?

8/21/2019 54806217 Airbus CBTquiz1


20002000 psipsi

30003000 psipsi

500500 psipsi

10001000 psipsi

According to this indication, the BLUE system ispowered by...

According to this indication, the BLUE system isAccording to this indication, the BLUE system is

powered by...powered by...

8/21/2019 54806217 Airbus CBTquiz1


The PTU.The PTU.

Both the GREEN and YELLOWBoth the GREEN and YELLOW systemssystems..

The ELEC pump.The ELEC pump.

The RAT.The RAT.

We have completed the procedure for HYD Y RSVR

LO AIR PR, what does the YELLOW indication in

amber mean?

We have completed the procedure for HYD Y RSVRWe have completed the procedure for HYD Y RSVR

LO AIR PR, what does the YELLOW indication inLO AIR PR, what does the YELLOW indication in

amber mean?amber mean?

8/21/2019 54806217 Airbus CBTquiz1


Users connected to the YELLOW systemUsers connected to the YELLOW system

are no longer supplied with hydraulicare no longer supplied with hydraulic

pressure.pressure.

YELLOW is amber because ENG 2 is not YELLOW is amber because ENG 2 is not

running.running.

The ELEC pump hasThe ELEC pump has beenbeen switched off.switched off.

You get a Y RSVR LO AIR PR message.

The first step of the procedure asks you to switch

the PTU off. Why?

You get a Y RSVR LO AIR PR message. You get a Y RSVR LO AIR PR message.

The first step of the procedure asks you to switchThe first step of the procedure asks you to switch

the PTU off. Why?the PTU off. Why?

8/21/2019 54806217 Airbus CBTquiz1


You want to increase the air pressure by You want to increase the air pressure by

isolating the YELLOW system.isolating the YELLOW system.

You want to avoid the pressurization of You want to avoid the pressurization of

the yellow system by the PTU after youthe yellow system by the PTU after you

switch the ENG 2 pump off.switch the ENG 2 pump off.

Because it is faulty.Because it is faulty.

You want to You want to unpressurizeunpressurize the BLUEthe BLUE

system.system.

Which statement is true?

Which statement is true?Which statement is true?

8/21/2019 54806217 Airbus CBTquiz1


The BLUE and the YELLOW systems areThe BLUE and the YELLOW systems are

supplying the GREEN system.supplying the GREEN system.

The YELLOW system is supplying theThe YELLOW system is supplying the

GREEN system.GREEN system.

The GREEN system is supplied by theThe GREEN system is supplied by the

BLUE system.BLUE system.

The YELLOW system is supplying theThe YELLOW system is supplying the

BLUE and the GREEN system.BLUE and the GREEN system.

As part of the cockpit preparation, you must check

the hydraulic fluid level. What should the indication

look like?

As part of the cockpit preparation, you must checkAs part of the cockpit preparation, you must check

the hydraulic fluid level. What should the indicationthe hydraulic fluid level. What should the indication

look like?look like?

8/21/2019 54806217 Airbus CBTquiz1


What is the meaning of the RAT indication, asdisplayed on this HYD ECAM page?

What is the meaning of the RAT indication, asWhat is the meaning of the RAT indication, as

displayed on this HYD ECAM page?displayed on this HYD ECAM page?

8/21/2019 54806217 Airbus CBTquiz1


The RAT is pressurizing the BLUEThe RAT is pressurizing the BLUE

system.system.

The RAT is faulty.The RAT is faulty.

The RAT is deployed.The RAT is deployed.

What is the correct PTU indication if it is deliveringpower to the GREEN system?

What is the correct PTU indication if it is deliveringWhat is the correct PTU indication if it is delivering

power to the GREEN system?power to the GREEN system?

8/21/2019 54806217 Airbus CBTquiz1


On the ECAM BLEED SD page, what is the normalindication in flight with WING ANTI-ICE on?

On the ECAM BLEED SD page, what is the normalOn the ECAM BLEED SD page, what is the normal

indication in flight with WING ANTIindication in flight with WING ANTI--ICE on?ICE on?

8/21/2019 54806217 Airbus CBTquiz1


You are in flight. According to these indications….

You are in flight. According to these indications You are in flight. According to these indications……..

8/21/2019 54806217 Airbus CBTquiz1


Both wing antiBoth wing anti--ice valves failed to open.ice valves failed to open.

Both wing antiBoth wing anti--ice valves failed to close.ice valves failed to close.

The right wing antiThe right wing anti--ice valve failed toice valve failed to

open.open.

The left wing antiThe left wing anti--ice valve failed to close.ice valve failed to close.

In flight the ECAM SD page displays the followingindications. What does it mean?

In flight the ECAM SD page displays the followingIn flight the ECAM SD page displays the following

indications. What does it mean?indications. What does it mean?

8/21/2019 54806217 Airbus CBTquiz1


Both wing antiBoth wing anti--ice valves failed to open.ice valves failed to open.

Both wing antiBoth wing anti--ice valves failed to close.ice valves failed to close.

The right wing antiThe right wing anti--ice valve failed toice valve failed to

open.open.

The left wing antiThe left wing anti--ice valve failed to close.ice valve failed to close.

Concerning the PROBE/WINDOW HEAT pb, whichone of the following statements is true?

Concerning the PROBE/WINDOW HEAT pb, whichConcerning the PROBE/WINDOW HEAT pb, which

one of the following statements is true?one of the following statements is true?

8/21/2019 54806217 Airbus CBTquiz1


When in AUTO mode, the windows areWhen in AUTO mode, the windows are

only heated on ground.only heated on ground.

When pushed on, window heating willWhen pushed on, window heating will

perform a 30 seconds test on ground andperform a 30 seconds test on ground and

then switch off until takethen switch off until take--off.off.

When pushed prior to engine start, theWhen pushed prior to engine start, the

windows are manually heated.windows are manually heated.

When pushed on after takeWhen pushed on after take--off, theoff, the

windows are heated only when necessary.windows are heated only when necessary.

Which sources are used for ice and rain protection?

Which sources are used for ice and rain protection?Which sources are used for ice and rain protection?

8/21/2019 54806217 Airbus CBTquiz1


Electrical heating only.Electrical heating only.

Hot air only.Hot air only.

Electrical heating and warm air from theElectrical heating and warm air from the

cabin.cabin.

Electrical heating and hot air.Electrical heating and hot air.

If one engine anti-ice system fails, the second onetakes over and provides anti-icing for both engines.

If one engine antiIf one engine anti--ice system fails, the second oneice system fails, the second one

takes over and provides antitakes over and provides anti--icing for both engines.icing for both engines.

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

When flying in icing conditions, what will be the

correct ECAM BLEED system page indication with

both WING and ENG anti-ice systems ON?

When flying in icing conditions, what will be theWhen flying in icing conditions, what will be the

correct ECAM BLEED system page indication withcorrect ECAM BLEED system page indication with

both WING and ENG antiboth WING and ENG anti--ice systems ON?ice systems ON?

8/21/2019 54806217 Airbus CBTquiz1


In flight, after switching wing Anti Icing System ON,

the ECAM E/WD page displays “WING A.ICE SYS

FAULT”. What does it mean?

In flight, after switching wing Anti Icing System ON,In flight, after switching wing Anti Icing System ON,

the ECAM E/WD page displaysthe ECAM E/WD page displays ““WING A.ICE SYSWING A.ICE SYS

FAULTFAULT””. What does it mean?. What does it mean?

8/21/2019 54806217 Airbus CBTquiz1


Both wing Anti Ice failed to closed.Both wing Anti Ice failed to closed.

The left wing Anti Ice failed to OPEN.The left wing Anti Ice failed to OPEN.

The right wing Anti Ice failed to open.The right wing Anti Ice failed to open.

Both wing Anti Ice failed to open.Both wing Anti Ice failed to open.

In case of Icing condition, the engine Anti-Icesystem...

In case of Icing condition, the engine AntiIn case of Icing condition, the engine Anti --IceIce

system...system...

8/21/2019 54806217 Airbus CBTquiz1


Cannot be used simultaneously with theCannot be used simultaneously with the

wing antiwing anti--ice system due to engineice system due to engine

limitations.limitations.

Is controlled manually by the pilotIs controlled manually by the pilot

through the ENG1 and ENG2 antithrough the ENG1 and ENG2 anti --iceice pbpb..

Operates only in flight and is fullyOperates only in flight and is fully

automatic in case of icing conditions.automatic in case of icing conditions.

Operates automatically after engine start,Operates automatically after engine start,

the pilots can have manual controlthe pilots can have manual control

through the ENG1 and ENG2 antithrough the ENG1 and ENG2 anti --iceice pbpb..

According to the ECAM Memo Page theseindications mean:

According to the ECAM Memo Page theseAccording to the ECAM Memo Page these

indications mean:indications mean:

8/21/2019 54806217 Airbus CBTquiz1


Because of ice detection, the system asksBecause of ice detection, the system asks

the pilot to switch the A.ICE system on.the pilot to switch the A.ICE system on.

At least one ENG A.ICE switch is in theAt least one ENG A.ICE switch is in the

ON position.ON position.

The ENG A.ICE system is inoperative.The ENG A.ICE system is inoperative.

The ENG A.ICE has automatically startedThe ENG A.ICE has automatically started

without any crew action.without any crew action.

After a disagreement on landing gear position, you

have recycled the L/G but there are still indicationsas shown.

How do you perform the next ECAM action?

After a disagreement on landing gear position, youAfter a disagreement on landing gear position, you

have recycled the L/G but there are still indicationshave recycled the L/G but there are still indications

as shown.as shown.

How do you perform the next ECAM action?How do you perform the next ECAM action?

A di h d L/G GRAVITYA di t th d L/G GRAVITY

8/21/2019 54806217 Airbus CBTquiz1


Pull the GRAVITY GEAR EXTNPull the GRAVITY GEAR EXTN handcrankhandcrank

and turn it clockwise 3 turns.and turn it clockwise 3 turns.

Pull the GRAVITY GEAR EXTNPull the GRAVITY GEAR EXTN handcrankhandcrank

and turn it counterclockwise 3 turns.and turn it counterclockwise 3 turns.

According to the procedure L/G GRAVITYAccording to the procedure L/G GRAVITY

EXTENSION which is found in the QuickEXTENSION which is found in the Quick

Reference Hand book (QRH).Reference Hand book (QRH).

Recycle the L/G a second time. This timeRecycle the L/G a second time. This time

the gear will free fall automatically.the gear will free fall automatically.

After a disagreement on landing gear position, you

have performed the L/G GRAVITY EXTENSION

procedure.

According to these indications, which statement is

true ?

After a disagreement on landing gear position, youAfter a disagreement on landing gear position, you

have performed the L/G GRAVITY EXTENSIONhave performed the L/G GRAVITY EXTENSION

procedure.procedure.

According to these indications, which statement isAccording to these indications, which statement is

true ?true ?

8/21/2019 54806217 Airbus CBTquiz1


After GRAVITY EXTENSION the gear After GRAVITY EXTENSION the gear

indications on the ECAM WHEEL pageindications on the ECAM WHEEL page

are not reliable.are not reliable.

The gear is in theThe gear is in the downlockdownlock position.position.

The gear is down but not locked.The gear is down but not locked.

You perform a landing with AUTO/BRK selected to

MED. After touch down you observe the following

indications.

At this moment, which statement is true ?

You perform a landing with AUTO/BRK selected to You perform a landing with AUTO/BRK selected to

MED. After touch down you observe the followingMED. After touch down you observe the following

indications.indications.

At this moment, which statement is true ?At this moment, which statement is true ?

8/21/2019 54806217 Airbus CBTquiz1


The ANTI/SKID system for wheels 1 andThe ANTI/SKID system for wheels 1 and

3 is inoperative.3 is inoperative.

The AUTO/BRK is applying pressure toThe AUTO/BRK is applying pressure to

brake 2 and 4 only.brake 2 and 4 only.

The ANTI/SKID system is increasing brakeThe ANTI/SKID system is increasing brake

pressure for wheels 2 and 4.pressure for wheels 2 and 4.

The ANTI/SKID system is releasing brakeThe ANTI/SKID system is releasing brake

pressure for wheels 2 and 4.pressure for wheels 2 and 4.

You have just set the parking brake handle to ON.

Which indication CONFIRMS that the parking brake

is actually set ?

You have just set the parking brake handle to ON. You have just set the parking brake handle to ON.

Which indication CONFIRMS that the parking brakeWhich indication CONFIRMS that the parking brake

is actually set ?is actually set ?

8/21/2019 54806217 Airbus CBTquiz1


PARK BRKPARK BRK

On this E/WD, what does the “NW STRG DISC”memo mean?

On this E/WD, what does theOn this E/WD, what does the ““NW STRG DISCNW STRG DISC””

memo mean?memo mean?

8/21/2019 54806217 Airbus CBTquiz1


One of the pilots has pushed the PEDALSOne of the pilots has pushed the PEDALS

DISC pushbutton located on the steeringDISC pushbutton located on the steering

handwheelhandwheel..

The nose wheel steering computer hasThe nose wheel steering computer has

finished itfinished it’’s self test.s self test.

Nose wheel steering is now available.Nose wheel steering is now available.

The nose wheel steering has beenThe nose wheel steering has been

disconnected by ground personnel.disconnected by ground personnel.

A failure in the nose wheel steeringA failure in the nose wheel steering

system has been detected.system has been detected.

PARK BRK

NW STRG DISC

During push back, engine n° 2 is started, leading to

the “NW STRG DISC” memo.

What is the correct statement?

During push back, engine nDuring push back, engine n°° 2 is started, leading to2 is started, leading to

thethe ““NW STRG DISCNW STRG DISC”” memo.memo.

What is the correct statement?What is the correct statement?

NW STRG DISC

8/21/2019 54806217 Airbus CBTquiz1


The nose wheel steering has been reThe nose wheel steering has been re--

connected by ground personnel.connected by ground personnel.

The amber indication will disappear asThe amber indication will disappear as

soon as you start taxi.soon as you start taxi.

The nose wheel steering is stillThe nose wheel steering is still

disconnected. The memo has becomedisconnected. The memo has become

amber because one engine is running.amber because one engine is running.

The NW STRG disconnect mechanism hasThe NW STRG disconnect mechanism has

failed.failed.

The yellow hydraulic system has build upThe yellow hydraulic system has build up

pressure which might damage the NWpressure which might damage the NW

STRG system when set to towingSTRG system when set to towing

position.position.

APU BLEED

After starting to taxi you perform the brake check.

While pressing on top of the rudder pedals you feel

the airplane decelerating but the BRAKES pressure

indication remains 0.

Which statement is true ?

After starting to taxi you perform the brake check.After starting to taxi you perform the brake check.

While pressing on top of the rudder pedals you feelWhile pressing on top of the rudder pedals you feel

the airplane decelerating but the BRAKES pressurethe airplane decelerating but the BRAKES pressure

indication remains 0.indication remains 0.


8/21/2019 54806217 Airbus CBTquiz1


You must perform the check again and You must perform the check again and

press harder on the brakes until you getpress harder on the brakes until you get

an indication.an indication.

The indication is normal because withThe indication is normal because withmanual braking you are not able to applymanual braking you are not able to apply

enough pressure to be displayed on theenough pressure to be displayed on the

BRAKES indicator.BRAKES indicator.

The BRAKES pressure indicator hasThe BRAKES pressure indicator has

failed.failed.

The indication is normal because theThe indication is normal because the

““BRAKESBRAKES”” press indicator is active onpress indicator is active on

brake system alternate mode (yellowbrake system alternate mode (yellow

supply).supply).

According to these indications, the AUTO/BRAKE isactive.

According to these indications, the AUTO/BRAKE isAccording to these indications, the AUTO/BRAKE is

active.active.

8/21/2019 54806217 Airbus CBTquiz1


True.True.

False.False.

What is the meaning of the 2 triangles, appearing

below each landing gear, on the WHEEL ECAM

page?

What is the meaning of the 2 triangles, appearingWhat is the meaning of the 2 triangles, appearing

below each landing gear, on the WHEEL ECAMbelow each landing gear, on the WHEEL ECAM

page?page?

8/21/2019 54806217 Airbus CBTquiz1


Each triangle represents one brakingEach triangle represents one braking

system (normal/alternate) available for system (normal/alternate) available for

the associated gear.the associated gear.

The front triangle indicates thatThe front triangle indicates thatAUTO/BRK is available and the one in theAUTO/BRK is available and the one in the

back means that ANTI/SKID is availableback means that ANTI/SKID is available

for that gear.for that gear.

Each triangle represents one tire.Each triangle represents one tire.

There are two computers providingThere are two computers providing

information on the gear position. Eachinformation on the gear position. Each

triangle represents the position detectedtriangle represents the position detected

by its associated computer.by its associated computer.

/GTh L/G i l k d

You have just set the L/G selector to the DOWNposition. According to these indications...

You have just set the L/G selector to the DOWN You have just set the L/G selector to the DOWN

position. According to these indications...position. According to these indications...

8/21/2019 54806217 Airbus CBTquiz1


The L/G computer has failed.The L/G computer has failed.

The gear will not extend.The gear will not extend.

The L/G is locked.The L/G is locked.

The L/G doors are jammed open.The L/G doors are jammed open.

The L/G is up and not locked in theThe L/G is up and not locked in the

selected position. The L/G doors are openselected position. The L/G doors are open

The computers providing gear positionThe computers providing gear position

information have failed.information have failed.

How do you interpret the following indications?

How do you interpret the following indications?How do you interpret the following indications?

8/21/2019 54806217 Airbus CBTquiz1


One L/G control system is inoperative.One L/G control system is inoperative.

The nose landing gear is notThe nose landing gear is not downlockeddownlocked..

The nose gear is down and locked.The nose gear is down and locked.

The nose gear doors are open.The nose gear doors are open.

The nose gear is in transit.The nose gear is in transit.

All gears are down and locked.All gears are down and locked.

What is the meaning of the green arc appearingover wheel #2?

What is the meaning of the green arc appearingWhat is the meaning of the green arc appearing

over wheel #2?over wheel #2?

It k th h tt t b k ithIt k th h tt t b k ith

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The ANTI/SKID system is automaticallyThe ANTI/SKID system is automatically

releasing the pressure of that brake.releasing the pressure of that brake.

The L/G control system has detected aThe L/G control system has detected a

low tire profile.low tire profile.

It marks the hottest brake with aIt marks the hottest brake with a

temperature of more than 100temperature of more than 100 ºº Celsius.Celsius.

It indicates an abnormal high temperature.It indicates an abnormal high temperature.

The pilot flying asks you to perform ECAM actions.

What are your actions according to the first line of

the ECAM procedure ?

The pilot flying asks you to perform ECAM actions.The pilot flying asks you to perform ECAM actions.

What are your actions according to the first line ofWhat are your actions according to the first line of

the ECAM procedure ?the ECAM procedure ?

I t t th L/G l t t th UPI must put the L/G selector to the UP

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I must put the L/G selector to the UPI must put the L/G selector to the UP

position and immediately to the DOWNposition and immediately to the DOWN

position again.position again.


position, wait until the gear has retracted,position, wait until the gear has retracted,

and then to the DOWN position again.and then to the DOWN position again.


position.position.

The system is trying to recycle the gear The system is trying to recycle the gear

automatically. I must wait until the firstautomatically. I must wait until the first

line disappears.line disappears.

During your walk-around, you see that one lightneeds a new bulb. What is the purpose of this light?

During your walkDuring your walk--around, you see that one lightaround, you see that one light

needs a new bulb. What is the purpose of this light?needs a new bulb. What is the purpose of this light?

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T/O light.T/O light.

Taxi light.Taxi light.

Landing light.Landing light.

RWY turnoff light.RWY turnoff light.

Where is the location of the exterior light panel?

Where is the location of the exterior light panel?Where is the location of the exterior light panel?

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Where are the controls for the seat belts and nosmoking signs located?

Where are the controls for the seat belts and noWhere are the controls for the seat belts and no

smoking signs located?smoking signs located?

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On the EXT LT control panel, the STROBE light

selector is set to AUTO. In this position, when do

they stop flashing?

On the EXT LT control panel, the STROBE lightOn the EXT LT control panel, the STROBE light

selector is set to AUTO. In this position, when doselector is set to AUTO. In this position, when do

they stop flashing?they stop flashing?

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When the landing lights are switched off.When the landing lights are switched off.

When the last engine has been shutWhen the last engine has been shut

down.down.

When the aircraft touches down.When the aircraft touches down.

When the first reverser is opened.When the first reverser is opened.

STROBE BEACON NAV LAND T OSTROBE BEACON NAV LAND T O

According to these panels, which lights are actuallyilluminated?

According to these panels, which lights are actuallyAccording to these panels, which lights are actually

illuminated?illuminated?

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BEACON,LAND, STROBE, T.O. and NAVBEACON,LAND, STROBE, T.O. and NAV

lights.lights.

STROBE, BEACON, NAV and LAND lights.STROBE, BEACON, NAV and LAND lights.

STROBE, BEACON, NAV, LAND, T.O.STROBE, BEACON, NAV, LAND, T.O.

and RWY TURN OFF lights.and RWY TURN OFF lights.

NAV, BEACON, T.O. and LAND lights.NAV, BEACON, T.O. and LAND lights.

Which of these buttons control IR and ADR?

Which of these buttons control IR and ADR?Which of these buttons control IR and ADR?

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On the ND.What does the MAN indication mean?

On the ND.On the ND.

What does the MAN indication mean?What does the MAN indication mean?

It is an indication that at least oneIt is an indication that at least one navaidnavaid

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It is an indication that at least oneIt is an indication that at least one navaidnavaid

has been manually tuned.has been manually tuned.

It is an indication that the WX RADAR TiltIt is an indication that the WX RADAR Tilt

has been manually adjusted.has been manually adjusted.

It is an indication that the WX RADARIt is an indication that the WX RADAR

Gain has been manually adjusted.Gain has been manually adjusted.

MAN

M t iM t i

What is the meaning of the magenta color of someradar returns?

What is the meaning of the magenta color of someWhat is the meaning of the magenta color of some

radar returns?radar returns?

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Mountains.Mountains.

Turbulences.Turbulences.

Water.Water.

What is the meaning of the black color on the radarimage?

What is the meaning of the black color on the radarWhat is the meaning of the black color on the radar

image?image?

M t iMountains

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Mountains.Mountains.

Turbulences.Turbulences.

No precipitations or water.No precipitations or water.

On the GNADIRS control panel, during the IRS

alignment, the ALIGN lights start flashing.

What is wrong?

On the GNADIRS control panel, during the IRSOn the GNADIRS control panel, during the IRS

alignment, the ALIGN lights start flashing.alignment, the ALIGN lights start flashing.

What is wrong?What is wrong?

System discovered a discrepancySystem discovered a discrepancy

between the position in the database andbetween the position in the database and

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between the position in the database andbetween the position in the database and

the position entered on the MCDU.the position entered on the MCDU.

At least one of the IR lost the NAVAt least one of the IR lost the NAV

capability.capability.

The system is performing a test before theThe system is performing a test before the

final alignment.final alignment.

The alignment process stopped at 1The alignment process stopped at 1

minute of the end and is waiting for theminute of the end and is waiting for the

coordinates to be inserted.coordinates to be inserted.

Between the ND and MCDU you are performing aNAV ACCUR check. Does it satisfy you?

Between the ND and MCDU you are performing aBetween the ND and MCDU you are performing a

NAV ACCUR check. Does it satisfy you?NAV ACCUR check. Does it satisfy you?

Yes, raw data and FMGS position are the Yes, raw data and FMGS position are the

same or the difference is withinsame or the difference is within

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same or the difference is withinsame or the difference is within

acceptable limits.acceptable limits.

No, there is a major discrepancy betweenNo, there is a major discrepancy between

raw data and FMGS positions.raw data and FMGS positions.

No, the accuracy is displayed LOW on theNo, the accuracy is displayed LOW on the

MCDU PROG page.MCDU PROG page.

One of the IR has an attitude problem. Pleaseperform the correct action.

One of the IR has an attitude problem. PleaseOne of the IR has an attitude problem. Please

perform the correct action.perform the correct action.

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On the GNADIRS control panel, what is the position

for the DATA selector to see the remaining time for

alignment?

On the GNADIRS control panel, what is the positionOn the GNADIRS control panel, what is the position

for the DATA selector to see the remaining time forfor the DATA selector to see the remaining time for

alignment?alignment?

PPOSPPOS

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PPOS.PPOS.

HDG.HDG.

STS.STS.

TEST.TEST.

ALIGN ALIGN ALIGN

What does the indication TTN 10 on the GNADIRSpanel mean?

What does the indication TTN 10 on the GNADIRSWhat does the indication TTN 10 on the GNADIRS

panel mean?panel mean?

It is an indication that IR3 has calculated aIt is an indication that IR3 has calculated a

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heading of 10 degrees to True North.heading of 10 degrees to True North.

It is an indication that it will take 10It is an indication that it will take 10

minutes to complete the alignment.minutes to complete the alignment.

It is an indication that the headingIt is an indication that the heading

calculated by IR3 differs by 10 degreescalculated by IR3 differs by 10 degrees

from the average.from the average.

It is an indication that the time to the nextIt is an indication that the time to the next

waypoint is 10 minutes.waypoint is 10 minutes.

ALIGN ALIGN ALIGN

An ILS approach is selected. Please indicate thedisplays with information about ILS 2.

An ILS approach is selected. Please indicate theAn ILS approach is selected. Please indicate the

displays with information about ILS 2.displays with information about ILS 2.

PFD 1 and ND 1PFD 1 and ND 1.

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PFD 1 and ND 1.PFD 1 and ND 1.




Is it possible to get information about ILS 2 on theCAPT side?

Is it possible to get information about ILS 2 on theIs it possible to get information about ILS 2 on the

CAPT side?CAPT side?

Yes, on the PFD 1.Yes, on the PFD 1.

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Yes, on the PFD 1. Yes, on the PFD 1.

Yes, on the ND 1. Yes, on the ND 1.

No, it is not possible.No, it is not possible.

Which Nav-aids are displayed on the DDRMI?

Which NavWhich Nav--aids are displayed on the DDRMI?aids are displayed on the DDRMI?

VOR 1 and VOR 2.VOR 1 and VOR 2.

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VOR 1 and VOR 2.VOR 1 and VOR 2.

ADF 1 and ADF 2.ADF 1 and ADF 2.

VOR 1 and ADF 2.VOR 1 and ADF 2.

VOR 2 and ADF 1.VOR 2 and ADF 1.

Please indicate the location of the GPWS panel.

Please indicate the location of the GPWS panel.Please indicate the location of the GPWS panel.

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Please indicate the location of the ATC and TCASpanel.

Please indicate the location of the ATC and TCASPlease indicate the location of the ATC and TCAS

panel.panel.

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Which situation corresponds to the WX RADARsettings?

Which situation corresponds to the WX RADARWhich situation corresponds to the WX RADAR

settings?settings?

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What is the appropriate ECAM page to getinformation about the oxygen system?

What is the appropriate ECAM page to getWhat is the appropriate ECAM page to get

information about the oxygen system?information about the oxygen system?

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In case of an ECAM procedure calling for a Manual

deployment of the masks, indicate which control pb

has to be pressed.

In case of an ECAM procedure calling for a ManualIn case of an ECAM procedure calling for a Manual

deployment of the masks, indicate which controldeployment of the masks, indicate which control pbpb

has to be pressed.has to be pressed.

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On the passenger OXYGEN control panel, whichindication confirms the deployment of the masks?

On the passenger OXYGEN control panel, whichOn the passenger OXYGEN control panel, which

indication confirms the deployment of the masks?indication confirms the deployment of the masks?

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On the crew OXYGEN MASK Regulator Panel, which

statement best reflects the function of the N/100%

supply selector?

On the crew OXYGEN MASK Regulator Panel, whichOn the crew OXYGEN MASK Regulator Panel, which

statement best reflects the function of the N/100%statement best reflects the function of the N/100%

supply selector?supply selector?

The 100% position provides the maximumThe 100% position provides the maximum

pressure, N provides the normal pressure,pressure, N provides the normal pressure,

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N position cuts the oxygen supply, 100%N position cuts the oxygen supply, 100%

position enables normal oxygen supply.position enables normal oxygen supply.

The N/100% selector is to be used duringThe N/100% selector is to be used during

the preflight check to check the oxygenthe preflight check to check the oxygen

supply to the mask.supply to the mask.

which is lower.which is lower.

The N position provides an air/oxygenThe N position provides an air/oxygen

mixture, 100% delivers pure oxygen.mixture, 100% delivers pure oxygen.

The cockpit CREW OXYGEN being operative,

which pb has to be pressed to switch the system

OFF?

The cockpit CREW OXYGEN being operative,The cockpit CREW OXYGEN being operative,

whichwhich pbpb has to be pressed to switch the systemhas to be pressed to switch the system

OFF?OFF?

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After switching the cockpit CREW OXYGEN OFF,which ECAM indication would you see?

After switching the cockpit CREW OXYGEN OFF,After switching the cockpit CREW OXYGEN OFF,

which ECAM indication would you see?which ECAM indication would you see?

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On the ECAM control panel, please select the

appropriate ECAM page to get information about

the PNEUMATIC system.

On the ECAM control panel, please select theOn the ECAM control panel, please select the

appropriate ECAM page to get information aboutappropriate ECAM page to get information about

the PNEUMATIC system.the PNEUMATIC system.

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Both engines are running and APU BLEED has

been switched OFF. Is the ECAM BLEED page

display correct ?

Both engines are running and APU BLEED hasBoth engines are running and APU BLEED has

been switched OFF. Is the ECAM BLEED pagebeen switched OFF. Is the ECAM BLEED page

display correct ?display correct ?

No, APU bleed closed, but X bleed valveNo, APU bleed closed, but X bleed valve

has to stay open.has to stay open.

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y py p

No, the crew should select X bleed valveNo, the crew should select X bleed valve

selector to (shut) position to close theselector to (shut) position to close the

valve manually after one engine is started.valve manually after one engine is started.

No, IP HP valves should be closed.No, IP HP valves should be closed.

Yes, all the indications are correct, HP Yes, all the indications are correct, HPvalves open because of high air demandvalves open because of high air demand

with engine at low RPM.with engine at low RPM.

An ENG 1 BLEED fault has occurred and is

indicated by the related ECAM E/WD failure

message.

An ENG 1 BLEED fault has occurred and isAn ENG 1 BLEED fault has occurred and is

indicated by the related ECAM E/WD failureindicated by the related ECAM E/WD failure

message.message.

The ENG 1 BLEED valve has beenThe ENG 1 BLEED valve has been

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The left hand Bleed canThe left hand Bleed can’’t be recovered.t be recovered.

APU bleed can never supply the left side.APU bleed can never supply the left side.

automatically closed.automatically closed.

On ground, on the ECAM SD “BLEED” page theGND symbol is always displayed.

On ground, on the ECAM SDOn ground, on the ECAM SD ““BLEEDBLEED”” page thepage the

GND symbol is always displayed.GND symbol is always displayed.

True.True.

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False.False.

According to the ECAM BLEED page message and“AIR COND” control panel indications.

According to the ECAM BLEED page message andAccording to the ECAM BLEED page message and

““AIR CONDAIR COND”” control panel indications.control panel indications.

The engines are running and supplyingThe engines are running and supplying

bleed air.bleed air.

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The engines are not running, the APU isThe engines are not running, the APU is

supplying bleed air.supplying bleed air.

The engines are running, the APU isThe engines are running, the APU is

supplying bleed air.supplying bleed air.

The engines are not running, a GND HPThe engines are not running, a GND HP

air unit is supplying bleed air.air unit is supplying bleed air.

After starting both engines and according to those

AIR COND panel and ECAM BLEED page

indications, which source(s) provide the bleed air?

After starting both engines and according to thoseAfter starting both engines and according to those

AIR COND panel and ECAM BLEED pageAIR COND panel and ECAM BLEED page

indications, which source(s) provide the bleed air?indications, which source(s) provide the bleed air?

The engines.The engines.

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The APU.The APU.

The engines and the APU together.The engines and the APU together.

What is the engine power according to this ECAMindication?

What is the engine power according to this ECAMWhat is the engine power according to this ECAM

indication?indication?

At or close to takeAt or close to take--off power.off power.

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The engines are not running.The engines are not running.

At or slightly above idle power.At or slightly above idle power.

According to the present AIR COND control panel

switch positions and ECAM BLEED pageindications, which source(s) will supply bleed air

when the APU BLEED pb is pressed.

According to the present AIR COND control panelAccording to the present AIR COND control panel

switch positions and ECAM BLEED pageswitch positions and ECAM BLEED page

indications, which source(s) will supply bleed airindications, which source(s) will supply bleed air

when the APU BLEEDwhen the APU BLEED pbpb is pressed.is pressed.

The APU supplies both sides of theThe APU supplies both sides of the

system.system.

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The APU supplies the left side of theThe APU supplies the left side of the

system only.system only.

The APU supplies left side and engine 2The APU supplies left side and engine 2

the right side of the system.the right side of the system.

There will be no bleed air supplied.There will be no bleed air supplied.

The APU BLEED pb has just been switched ON.

On the ECAM BLEED page what do the related

indications mean?

The APU BLEEDThe APU BLEED pbpb has just been switched ON.has just been switched ON.

On the ECAM BLEED page what do the relatedOn the ECAM BLEED page what do the related

indications mean?indications mean?

The X BLEED valve has failed to open.The X BLEED valve has failed to open.

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The X BLEED valve has failed to close.The X BLEED valve has failed to close.

The X BLEED valve is in transit.The X BLEED valve is in transit.

The X BLEED valve is open.The X BLEED valve is open.

Following an ENG 1 BLEED fault, the ECAM E/WD

procedure has been applied; on the ECAM statuspage how do we interpret the STATUS information

message in green?

Following an ENG 1 BLEED fault, the ECAM E/WDFollowing an ENG 1 BLEED fault, the ECAM E/WD

procedure has been applied; on the ECAM statusprocedure has been applied; on the ECAM status

page how do we interpret the STATUS informationpage how do we interpret the STATUS information

message in green?message in green?

One pack has been automaticallyOne pack has been automatically

switched off because one ENG BLEEDswitched off because one ENG BLEED

system cannot supply WAI and 2 packs.system cannot supply WAI and 2 packs.

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system cannot supply WAI and 2 packs.y pp y p

One pack has to be switched OFF if WINGOne pack has to be switched OFF if WING

ANTI ICE (WAI) is used because one ENGANTI ICE (WAI) is used because one ENG

BLEED system cannot supply WAI and 2BLEED system cannot supply WAI and 2

packs together.packs together.

If WAI, has to be used, the X BLEED valveIf WAI, has to be used, the X BLEED valve

is automatically closed. Therefore, pack 1is automatically closed. Therefore, pack 1

will no longer be supplied.will no longer be supplied.

What is the normal APU Fire extinguisher

overpressure indication, and how do you interpret

it?

What is the normal APU Fire extinguisherWhat is the normal APU Fire extinguisher

overpressure indication, and how do you interpretoverpressure indication, and how do you interpret

it?it?

A red disc, which means the APU FIREA red disc, which means the APU FIRE

EXTING BOTTLE has been dischargedEXTING BOTTLE has been discharged

due to an APU fire.due to an APU fire.

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A green disc, which means the bottleA green disc, which means the bottle

pressure is normal.pressure is normal.

A red disc, which means the APU FIREA red disc, which means the APU FIREEXTING BOTTLE has not been dischargedEXTING BOTTLE has not been discharged

overboard.overboard.

A pressure gage visible from outsideA pressure gage visible from outside

which indicates the bottle pressure.which indicates the bottle pressure.

To use the APU bleed system, the crew will select:

To use the APU bleed system, the crew will select:To use the APU bleed system, the crew will select:

The APU BLEEDThe APU BLEED pbpb on AIR CONDon AIR COND


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The ENG1 and ENG2 BLEEDThe ENG1 and ENG2 BLEED pbspbs..

This is an automatic sequence initiatedThis is an automatic sequence initiated

when second or Eng starting is selected.when second or Eng starting is selected.

The bleed rotary selector on AIR CONDThe bleed rotary selector on AIR COND


On ground and in flight, electric power forOn ground and in flight, electric power for

the aircraft electric system and bleed airthe aircraft electric system and bleed air

for engine start.for engine start.

The APU provides:

The APU provides:The APU provides:

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Bleed air for engine start on ground andBleed air for engine start on ground and

air conditioning in flight only.air conditioning in flight only.

Electric Power only for electric system onElectric Power only for electric system on

ground and in flight.ground and in flight.

-- On ground: bleed air for engine startOn ground: bleed air for engine start-- On ground and in flight: electric powerOn ground and in flight: electric power

and bleed air for air conditioning.and bleed air for air conditioning.

g

The Electric Power supplied from the APUgenerator is

The Electric Power supplied from the APUThe Electric Power supplied from the APU

generator isgenerator is

Available as soon as APU is running, evenAvailable as soon as APU is running, even

if APU GEN is not selected ON.if APU GEN is not selected ON.

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Only available if the ground ExternalOnly available if the ground External

Power is already connected to the a/cPower is already connected to the a/c

Electric network .Electric network .

Available as soon as engines are shutAvailable as soon as engines are shut

down.down.

Available when APU is running, APU GENAvailable when APU is running, APU GEN

is ON and EXT PWR is not ON.is ON and EXT PWR is not ON.

You have just set the APU MASTER SW to OFF.

You notice you still have APU AVAIL indications.

What is the reason for that ?

You have just set the APU MASTER SW to OFF. You have just set the APU MASTER SW to OFF.

You notice you still have APU AVAIL indications. You notice you still have APU AVAIL indications.

What is the reason for that ?What is the reason for that ?

The APU has shut down but the AIRThe APU has shut down but the AIR

INLET FLAP is not fully closed yet.INLET FLAP is not fully closed yet.

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The APU is still running because it alwaysThe APU is still running because it always

needs a cool down period after the APUneeds a cool down period after the APU

MASTER SW has been switched off.MASTER SW has been switched off.

The APU is still running. It is in the coolThe APU is still running. It is in the cool

down period because you have used APUdown period because you have used APU

bleed before.bleed before.

The APU is still running. You have toThe APU is still running. You have topush the START SW to initiate the shutpush the START SW to initiate the shut

down sequence.down sequence.

After the engines have been switched off, you

realize that there is no external power available.According to the indications can you still interrupt

the APU shut down sequence?

After the engines have been switched off, youAfter the engines have been switched off, you

realize that there is no external power available.realize that there is no external power available.

According to the indications can you still interruptAccording to the indications can you still interrupt

the APU shut down sequence?the APU shut down sequence?

No, I have to wait until the APU AIR INLETNo, I have to wait until the APU AIR INLET

FLAP is fully closed and then start theFLAP is fully closed and then start the

APU again.APU again.

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Yes, I simply push the APU START Yes, I simply push the APU START

switch to ON.switch to ON.

No, I have to wait until the AVAILNo, I have to wait until the AVAILindications disappear and then start theindications disappear and then start the

APU again.APU again.

Yes, I simply push the APU MASTER SW Yes, I simply push the APU MASTER SW

back to ON.back to ON.

Which ECAM APU page corresponds to theseindications on the overhead panel ?

Which ECAM APU page corresponds to theseWhich ECAM APU page corresponds to these

indications on the overhead panel ?indications on the overhead panel ?

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You are attempting to start the APU.

After 20 seconds you get the following indicationsthat you didn’t get during the last APU start.

Can you continue the APU start?

You are attempting to start the APU. You are attempting to start the APU.

After 20 seconds you get the following indicationsAfter 20 seconds you get the following indications

that you didnthat you didn’’t get during the last APU start.t get during the last APU start.

Can you continue the APU start?Can you continue the APU start?

No. A low oil level has been detected andNo. A low oil level has been detected and

any start attempt will damage the APU.any start attempt will damage the APU.

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Any start attempt with a detected LOWAny start attempt with a detected LOW

OIL LEVEL will lead to an AUTOOIL LEVEL will lead to an AUTO

SHUTDOWN to prevent the APU to beSHUTDOWN to prevent the APU to be

damaged.damaged.

Yes. The APU will run for another 60 Yes. The APU will run for another 60hours after the LOW OIL LEVEL has beenhours after the LOW OIL LEVEL has been

detected.detected.

Yes, you simple have to wait 20 sec until Yes, you simple have to wait 20 sec until

the LOW OIL LEVEL advisory disappearsthe LOW OIL LEVEL advisory disappears

and then go ahead with the APU start.and then go ahead with the APU start.

The APU will keep on running to coolThe APU will keep on running to cool

down and then shutdown.down and then shutdown.

After engine shut down, APU running but APU

bleed has not been used, when you select APU

MASTER SW pb off.

After engine shut down, APU running but APUAfter engine shut down, APU running but APU

bleed has not been used, when you select APUbleed has not been used, when you select APU

MASTER SW pb off.MASTER SW pb off.

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APU will shutdown only if external powerAPU will shutdown only if external power

is connected.is connected.

Nothing happen because air conditioningNothing happen because air conditioning

is selected on.is selected on.

The APU will shutdown right away.The APU will shutdown right away.

15 000 ft15 000 ft

In flight APU starting limitation is

In flight APU starting limitation isIn flight APU starting limitation is

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39 000 ft39 000 ft

20 000 ft20 000 ft

What is the maximum altitude the APU may be usedfor bleed air supply with 1 pack operating ?

What is the maximum altitude the APU may be usedWhat is the maximum altitude the APU may be used

for bleed air supply with 1 pack operating ?for bleed air supply with 1 pack operating ?

15 000 ft15 000 ft

ALTITUDE (Ft)ALTITUDE (Ft)

20 00020 000

39 00039 000

15 00015 000

25 00025 000

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25 000 ft25 000 ft

39 000 ft39 000 ft

20 000 ft20 000 ft

According to the ECAM APU page indications :

According to the ECAM APU page indications :According to the ECAM APU page indications :

The APU is running and available. It isThe APU is running and available. It is

providing bleed air and electrical power.providing bleed air and electrical power.

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providing bleed air only.providing bleed air only.


providing electrical power only.providing electrical power only.

The APU is running and available . It isThe APU is running and available . It isproviding neither electrical power norproviding neither electrical power nor

bleed air.bleed air.

On the ground, during APU start, the master

caution and single chime come ON and you noticeon the ECAM, that the APU won’t exceed 53% N1.

Which statement is true?

On the ground, during APU start, the masterOn the ground, during APU start, the master

caution and single chime come ON and you noticecaution and single chime come ON and you notice

on the ECAM, that the APU wonon the ECAM, that the APU won’’t exceed 53% N1.t exceed 53% N1.

Which statement is true?Which statement is true?

An APU AUTO SHUT DOWN will occurAn APU AUTO SHUT DOWN will occur

because of APU failure to reach 90% N1.because of APU failure to reach 90% N1.

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You have to abort the start by pushing the You have to abort the start by pushing the

APU MASTER SW to off.APU MASTER SW to off.

An APU EMER SHUT DOWN will occurAn APU EMER SHUT DOWN will occur

because APU EGT overheating may causebecause APU EGT overheating may cause

an APU fire.an APU fire.

The FLAP will remain open after APUThe FLAP will remain open after APU

shutdown to vent the APU compartment.shutdown to vent the APU compartment.

You are performing the walk around with the APU

running and nobody is in the cockpit.

What will happen in case of an APU FIRE?

You are performing the walk around with the APU You are performing the walk around with the APU

running and nobody is in the cockpit.running and nobody is in the cockpit.

What will happen in case of an APU FIRE?What will happen in case of an APU FIRE?

An APU EMER shut down will occur andAn APU EMER shut down will occur and

the APU fire bottle will be dischargedthe APU fire bottle will be discharged

automatically.automatically.

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An APU AUTO shut down will occur butAn APU AUTO shut down will occur but

you have to discharge the APU fire bottleyou have to discharge the APU fire bottle

from the cockpit manually.from the cockpit manually.

An EMER AUTO shut down will occur butAn EMER AUTO shut down will occur but

you have to discharge the APU fire bottleyou have to discharge the APU fire bottle

manually either from the cockpit or bymanually either from the cockpit or by

pushing the APU SHUT DOWN switch onpushing the APU SHUT DOWN switch on

the external power panel.the external power panel.

You have to perform the ECAM actions to You have to perform the ECAM actions to

shut down the APU and extinguish the fireshut down the APU and extinguish the fire

from the cockpit.from the cockpit.

Please indicate the stowing place

for the escape ropes.

Please indicate the stowing placePlease indicate the stowing place

for the escape ropes.for the escape ropes.

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On the ECAM DOOR/OXY page, what does anamber door indication mean?

On the ECAM DOOR/OXY page, what does anOn the ECAM DOOR/OXY page, what does an

amber door indication mean?amber door indication mean?

The door is fully open.The door is fully open.

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The door is unlocked.The door is unlocked.

The door is inoperative.The door is inoperative.

The door is fully closed.The door is fully closed.

According to this indication, the Cargo door isinoperative.

According to this indication, the Cargo door isAccording to this indication, the Cargo door is

inoperative.inoperative.

True.True.

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False.False.

You have reached the gate. Somebody is about to

open the left forward door from the outside. What

will happen in this case?

You have reached the gate. Somebody is about to You have reached the gate. Somebody is about to

open the left forward door from the outside. Whatopen the left forward door from the outside. What

will happen in this case?will happen in this case?

The slide will be deployed.The slide will be deployed.

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Nothing. Opening from outside disarmsNothing. Opening from outside disarms

the slide.the slide.

Nothing. The door can't be open fromNothing. The door can't be open from

outside as long as theoutside as long as the slideslide is armed.is armed.

On the ECAM SD DOOR/OXY page this indicationmeans.

On the ECAM SD DOOR/OXY page this indicationOn the ECAM SD DOOR/OXY page this indication

means.means.

OverwingOverwing exits and right rear door slidesexits and right rear door slidesare armed, left forward cabin door andare armed, left forward cabin door and

forward cargo door indicate aforward cargo door indicate a

malfunction.malfunction.

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The left forward cabin door and theThe left forward cabin door and the

forward cargo door are unlocked, theforward cargo door are unlocked, the

overwingoverwing exits and the rightexits and the right rear rear door door

slides are not armed.slides are not armed.

OverwingOverwing exits and right rear door slidesexits and right rear door slides

are not armed, left forward cabin door andare not armed, left forward cabin door and

forward cargo door indicating aforward cargo door indicating a

malfunction.malfunction.

The left forward cabin door and theThe left forward cabin door and the

forward cargo door are unlocked, theforward cargo door are unlocked, the

overwingoverwing exits and the right rear door exits and the right rear door

slides are armed.slides are armed.

You are at the gate, according to this DOOR/OXYECAM page, the EMERGENCY EXITs are disarmed.

You are at the gate, according to this DOOR/OXY You are at the gate, according to this DOOR/OXY

ECAM page, the EMERGENCYECAM page, the EMERGENCY EXITsEXITs are disarmed.are disarmed.

True.True.

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False.False.

Regarding engine THRUST LEVERS position, whichdetent(s) can be used for take-off?

Regarding engine THRUST LEVERS position, whichRegarding engine THRUST LEVERS position, which

detent(sdetent(s) can be used for take) can be used for take--off?off?

FULL.FULL.

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CLIMB and TO/GA.CLIMB and TO/GA.

FLEX/MCT and TO/GA.FLEX/MCT and TO/GA.

CLIMB and FLEX/MCT.CLIMB and FLEX/MCT.

What is the meaning of an amber FAULT light onthe ENG panel?

What is the meaning of an amber FAULT light onWhat is the meaning of an amber FAULT light on

the ENG panel?the ENG panel?

It indicates a failure in the automatic startIt indicates a failure in the automatic start

sequence.sequence.

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It indicates a failure in the engine fireIt indicates a failure in the engine fire

extinguishing system.extinguishing system.

It indicates an engine failure.It indicates an engine failure.

On the ECAM E/WD page, what is the meaning ofthe amber CHK indication?

On the ECAM E/WD page, what is the meaning ofOn the ECAM E/WD page, what is the meaning of

the amber CHK indication?the amber CHK indication?

It is an indication that the EGT of ENG 1 isIt is an indication that the EGT of ENG 1 is

out of the normal range.out of the normal range.

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It is an indication of a discrepancyIt is an indication of a discrepancy

between the digital EGT indication andbetween the digital EGT indication and

the value indicated by the needle.the value indicated by the needle.

It is an indication of a discrepancyIt is an indication of a discrepancybetween the value shown on the ECAMbetween the value shown on the ECAM

and the real value.and the real value.


between EGT of ENG1 and ENG2.between EGT of ENG1 and ENG2.

C

H

K

ENG 1 EGT DISCREPANCY

On the ECAM E/WD page, what is the meaning ofthe amber CHK indication?

On the ECAM E/WD page, what is the meaning ofOn the ECAM E/WD page, what is the meaning of

the amber CHK indication?the amber CHK indication?

It is an indication that the EGT of ENG 1 isIt is an indication that the EGT of ENG 1 is

out of the normal range.out of the normal range.

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between the digital EGT indication andbetween the digital EGT indication and

the value indicated by the needle.the value indicated by the needle.

It is an indication of a discrepancyIt is an indication of a discrepancybetween the value shown on the ECAMbetween the value shown on the ECAM

and the real value.and the real value.


between EGT of ENG1 and ENG2.between EGT of ENG1 and ENG2.

ENG 1 EGT DISCREPANCY

You are in the middle of the engine start procedure.Is this an automatic start or a manual start?

You are in the middle of the engine start procedure. You are in the middle of the engine start procedure.

Is this an automatic start or a manual start?Is this an automatic start or a manual start?

Automatic.Automatic.

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Manual.Manual.

You are in the middle of the engine start procedure.Is this an automatic start or a manual start?

You are in the middle of the engine start procedure. You are in the middle of the engine start procedure.

Is this an automatic start or a manual start?Is this an automatic start or a manual start?

Automatic.Automatic.

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Manual.Manual.

During a manual start, what is the role of theFADEC?

During a manual start, what is the role of theDuring a manual start, what is the role of the

FADEC?FADEC?

It has a passive monitoring role, the crewIt has a passive monitoring role, the crewhas to monitor the start carefully to takehas to monitor the start carefully to take

corrective actions in case ofcorrective actions in case of

malfunctions.malfunctions.

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FADEC does not monitor the manualFADEC does not monitor the manual

start at all. All steps and possiblestart at all. All steps and possible

corrective actions have to be performedcorrective actions have to be performed

by the pilots.by the pilots.

There is no difference betweenThere is no difference between

automatic and normal start, FADECautomatic and normal start, FADEC

monitors and reacts to possible failuresmonitors and reacts to possible failures

during the start sequence.during the start sequence.

During a manual start, what is the role of theFADEC?

During a manual start, what is the role of theDuring a manual start, what is the role of the

FADEC?FADEC?

It has a passive monitoring role, the crewIt has a passive monitoring role, the crewhas to monitor the start carefully to takehas to monitor the start carefully to take

corrective actions in case ofcorrective actions in case of

malfunctions.malfunctions.

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FADEC does not monitor the manualFADEC does not monitor the manual

start at all. All steps and possiblestart at all. All steps and possible

corrective actions have to be performedcorrective actions have to be performed

by the pilots.by the pilots.

There is no difference betweenThere is no difference between

automatic and normal start, FADECautomatic and normal start, FADEC

monitors and reacts to possible failuresmonitors and reacts to possible failures

during the start sequence.during the start sequence.

Which step of a manual start is taken over by theFADEC?

Which step of a manual start is taken over by theWhich step of a manual start is taken over by the

FADEC?FADEC?

Ignition start.Ignition start.

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Fuel flow start.Fuel flow start.

Starter engagement.Starter engagement.

Ignition cutIgnition cut--out.out.

Which step of a manual start is taken over by theFADEC?

Which step of a manual start is taken over by theWhich step of a manual start is taken over by the

FADEC?FADEC?


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Starter engagement.Starter engagement.

Ignition cutIgnition cut--out.out.

From ECAM E/WD and SD engine pages

determinate which step of a manual start is taken

over by the FADEC?

From ECAM E/WD and SD engine pagesFrom ECAM E/WD and SD engine pages

determinate which step of a manual start is takendeterminate which step of a manual start is taken

over by the FADEC?over by the FADEC?

Starter valve closure.Starter valve closure.

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Starter valve engagement.Starter valve engagement.

From ECAM E/WD and SD engine page determinate

which step of a manual start is taken over by the

FADEC.

From ECAM E/WD and SD engine page determinateFrom ECAM E/WD and SD engine page determinate

which step of a manual start is taken over by thewhich step of a manual start is taken over by the

FADEC.FADEC.

Starter valve closure.Starter valve closure.

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Starter valve engagement.Starter valve engagement.

You are about to perform a take-off. You don’t have

inserted a FLEX temperature.

Which thrust lever detent shall be used for take-off?

You are about to perform a take You are about to perform a take--off. You donoff. You don’’t havet have

inserted a FLEX temperature.inserted a FLEX temperature.

Which thrust lever detent shall be used for takeWhich thrust lever detent shall be used for take--off?off?

FULL.FULL.

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FLEX/MCT.FLEX/MCT.

TO/GA.TO/GA.

CLIMB.CLIMB.

During the automatic start sequence of ENG 2, you

notice that only igniter B is powered.

Is this normal?

During the automatic start sequence of ENG 2, youDuring the automatic start sequence of ENG 2, you

notice that only igniter B is powered.notice that only igniter B is powered.

Is this normal?Is this normal?

No, normally igniter A is used for theNo, normally igniter A is used for the

engine start.engine start.

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Yes, igniter B is always used for the Yes, igniter B is always used for the


Yes, igniters are used alternatively for Yes, igniters are used alternatively forengine start, in this case B.engine start, in this case B.

No, normally both igniters are used forNo, normally both igniters are used for


During the automatic start sequence of ENG 2, you

notice that only igniter B is powered.

Is this normal?

During the automatic start sequence of ENG 2, youDuring the automatic start sequence of ENG 2, you

notice that only igniter B is powered.notice that only igniter B is powered.




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Yes, igniter B is always used for the Yes, igniter B is always used for the


Yes, igniters are used alternatively for Yes, igniters are used alternatively forengine start, in this case B.engine start, in this case B.

No, normally both igniters are used forNo, normally both igniters are used for


You are performing a take-off with the thrust leversin the FLEX position. Is A/THR now active?

You are performing a take You are performing a take--off with the thrust leversoff with the thrust levers

in the FLEX position. Is A/THR now active?in the FLEX position. Is A/THR now active?

Yes. Yes.

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No.No.

You are performing a take-off with the thrust leversin the FLEX position. Is A/THR now active?

You are performing a take You are performing a take--off with the thrust leversoff with the thrust levers

in the FLEX position. Is A/THR now active?in the FLEX position. Is A/THR now active?

Yes. Yes.

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No.No.

You are performing a take off with thrust levers inFLEX position. When does A/THR become active?

You are performing a take off with thrust levers in You are performing a take off with thrust levers in

FLEX position. When does A/THR become active?FLEX position. When does A/THR become active?

As soon as the thrust levers are pulledAs soon as the thrust levers are pulled

back into the CLIMB position.back into the CLIMB position.

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As soon as you engage the autopilot.As soon as you engage the autopilot.

As soon as you push the A/THRAs soon as you push the A/THR pbpbmanually on.manually on.

As soon as you pass the thrust reductionAs soon as you pass the thrust reduction

altitude.altitude.

You are performing a take off with thrust levers inFLEX position. When does A/THR become active?

You are performing a take off with thrust levers in You are performing a take off with thrust levers in

FLEX position. When does A/THR become active?FLEX position. When does A/THR become active?


back into the CLIMB position.back into the CLIMB position.

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As soon as you push the A/THRAs soon as you push the A/THR pbpbmanually on.manually on.

As soon as you pass the thrust reductionAs soon as you pass the thrust reduction

altitude.altitude.

You are performing a take-off with TOGA power.When does the A/THR become active?

You are performing a take You are performing a take--off with TOGA power.off with TOGA power.

When does the A/THR become active?When does the A/THR become active?


back into the FLEX position.back into the FLEX position.

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As soon as the thrust levers are pulledAs soon as the thrust levers are pulledback into the CLIMB position.back into the CLIMB position.

As soon as you push the A/THRAs soon as you push the A/THR pbpb

manually on.manually on.

You are performing a take-off with TOGA power.When does the A/THR become active?

You are performing a take You are performing a take--off with TOGA power.off with TOGA power.

When does the A/THR become active?When does the A/THR become active?


back into the FLEX position.back into the FLEX position.

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As soon as the thrust levers are pulledAs soon as the thrust levers are pulledback into the CLIMB position.back into the CLIMB position.

As soon as you push the A/THRAs soon as you push the A/THR pbpb

manually on.manually on.

What does an amber REV indication mean?

What does an amber REV indication mean?What does an amber REV indication mean?

The reversers are faulty.The reversers are faulty.

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The reversers are stuck.The reversers are stuck.

The reversers are unlocked.The reversers are unlocked.

The reversers are fully deployed.The reversers are fully deployed.

What does an amber REV indication mean?

What does an amber REV indication mean?What does an amber REV indication mean?


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On the ECAM E/WD, with thrust levers reverser to

reverse position. What does a green REV indication

mean?

On the ECAM E/WD, with thrust levers reverser toOn the ECAM E/WD, with thrust levers reverser to

reverse position. What does a green REV indicationreverse position. What does a green REV indication

mean?mean?


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On the ECAM E/WD, with thrust levers reverser to

reverse position. What does a green REV indication

mean?

On the ECAM E/WD, with thrust levers reverser toOn the ECAM E/WD, with thrust levers reverser to

reverse position. What does a green REV indicationreverse position. What does a green REV indication

mean?mean?


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Before engine starting the Eng FADEC should be

energized: which control do you activate in order to

energize the FADEC prior to engine start?

Before engine starting the Eng FADEC should beBefore engine starting the Eng FADEC should be

energized: which control do you activate in order toenergized: which control do you activate in order to

energize the FADEC prior to engine start?energize the FADEC prior to engine start?

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Before engine starting the Eng FADEC should be

energized: which control do you activate in order to

energize the FADEC prior to engine start?

Before engine starting the Eng FADEC should beBefore engine starting the Eng FADEC should be

energized: which control do you activate in order toenergized: which control do you activate in order to

energize the FADEC prior to engine start?energize the FADEC prior to engine start?

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During the manual start sequence of ENG 2, you

notice that both igniters are powered.

Is this normal?

During the manual start sequence of ENG 2, youDuring the manual start sequence of ENG 2, you

notice that both igniters are powered.notice that both igniters are powered.




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No, normally igniter B is used for theNo, normally igniter B is used for the


Yes, both igniters are used for every start. Yes, both igniters are used for every start.

Yes, for manual start both igniters are Yes, for manual start both igniters are

always used.always used.

During the manual start sequence of ENG 2, you

notice that both igniters are powered.

Is this normal?

During the manual start sequence of ENG 2, youDuring the manual start sequence of ENG 2, you

notice that both igniters are powered.notice that both igniters are powered.




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Yes, for manual start both igniters are Yes, for manual start both igniters are

always used.always used.

Documents

54806217 Airbus CBTquiz1