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

To decrease the HOT AIR demand from To 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, the With 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 from To 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 from To decrease the BLEED AIR demand from the APU.the APU.

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 ECAM Have a look at the ECAM ““CONDCOND”” page : page : ““ALTN ALTN MODEMODE”” is displayed.is displayed.What happened?What happened?

Channel 1 of ZONE CONTROLLER has Channel 1 of ZONE CONTROLLER has failed and the pilot has closed the HOT failed and the pilot has closed the HOT AIR and TRIM AIR valves. AIR and TRIM AIR valves.

Channel 1 of ZONE CONTROLLER has Channel 1 of ZONE CONTROLLER has failed and channel 2 has taken over, thus failed and channel 2 has taken over, thus the HOT AIR and TRIM AIR valves have the HOT AIR and TRIM AIR valves have closed automatically.closed automatically.

Looking at the ECAM BLEED page and AIR COND overhead panel, what can be concluded? Looking at the ECAM BLEED page and AIR COND Looking 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 valve On 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 the Aircraft is depressurized, but after the RAM AIR valve opens at least one pack RAM AIR valve opens at least one pack should be pressurized again.should be pressurized again.

Aircraft is depressurized, but the X Aircraft is depressurized, but the X BLEED valve should be open since both BLEED valve should be open since both engines are running.engines are running.

To HI, in order to help reduce the cabin To HI, in order to help reduce the cabin temperature.temperature.

To HI and cockpit TEMP SELECTOR to To HI and cockpit TEMP SELECTOR to HOT in order to have maximum cooling HOT 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 a During taxi, with a full load of passengers and in a high temperature area, how should the pack flow high temperature area, how should the pack flow be set?be set?

To LO, in order to minimize the amount of To 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 automatic To NORM, as the system is fully automatic apart from temperature settings.apart from temperature settings.

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

To regulate the pack outlet pressure to To regulate the pack outlet pressure to each zone.each zone.

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

To optimize the zone temperature by To optimize the zone temperature by adding cold air.adding cold air.

To optimize the zone temperature by To optimize the zone temperature by adding hot air.adding hot air.

For the Normal Operation of the CARGO COND SYSTEM :For the Normal Operation of the CARGO COND For the Normal Operation of the CARGO COND SYSTEM :SYSTEM :

The pilot ensures that there are no lights The pilot ensures that there are no lights illuminated on the illuminated on the pbpb swsw and that the and that the temperature is set as required.temperature is set as required.

The system display will be found on the The system display will be found on the ECAM BLEED page.ECAM BLEED page.

The pilot has no control of the system The pilot has no control of the system temperature.temperature.

The system display will be found on the The system display will be found on the ECAM PRESS page.ECAM PRESS page.

AftCargo

Ventilation Controller

ForwardCargo

Ventilation Controller

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 just Crew should SWITCH OFF both packs just before engines start.before engines start.

Crew should SWITCH OFF both engine Crew should SWITCH OFF both engine bleed valves just before engine start.bleed valves just before engine start.

During engine start, all the current During engine start, all the current indications on ECAM BLEED page and indications on ECAM BLEED page and COND overhead panel are correct.COND overhead panel are correct.

Crew should select X bleed valve selector Crew should select X bleed valve selector to SHUT position to pressurize the left to SHUT position to pressurize the left side first.side first.

The X BLEED should have remained The X BLEED should have remained open.open.

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

The crew should set X BLEED valve The crew should set X BLEED valve selector to SHUT position.selector to SHUT position.

The ENGINE H.P valve must be closed The 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 has Both engines are running and the APU bleed has been switched OFF.been switched OFF.Which statement is correct?Which statement is correct?

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, what If the PACK FLOW CONTROL valves close, what will be the subsequent position of the TRIM AIR will 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 AirValve

Hot AirValve

HotBleed Air

HOT AIR

Mixing Unit

Pack 1

Pack 2

The lower value is the temperature of the The lower value is the temperature of the air entering a zone (DUCT INLET air entering a zone (DUCT INLET temperature). The upper value is the temperature). The upper value is the actual zone temperature monitored by the actual zone temperature monitored by the zone 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 ECAM Have a look at the ECAM ““CONDCOND”” page. Why are page. Why are two different temperature values displayed for each two different temperature values displayed for each zone of the aircraft?zone of the aircraft?

The lower value is the pack outlet The lower value is the pack outlet temperature. The upper value is the actual temperature. The upper value is the actual zone temperature monitored by the zone zone temperature monitored by the zone control temperature.control temperature.

The lower value is the temperature of the The lower value is the temperature of the air controlled by the HOT AIR valve. The air controlled by the HOT AIR valve. The upper value is the pack outlet air upper value is the pack outlet air temperature.temperature.

The lower value is the actual zone The lower value is the actual zone temperature. The upper value is the temperature. The upper value is the selected zone temperature.selected zone temperature.

Accelerating the cabin zones Accelerating 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 and Reducing the BLEED AIR requirement and therefore saving fuel.therefore saving fuel.

HOT AIR

Mixing Unit

Pack 1

Pack 2

CabinFan

CabinFan

CabinFan

CabinFan

To provide backup pressure if the cabin To provide backup pressure if the cabin pressure controllers should fail.pressure controllers should fail.

In the CABIN PRESSURIZATION system, the function of the safety valves is...In the CABIN PRESSURIZATION system, the In 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 differential Protect against excessive differential pressure.pressure.

Yes, SYS1 is still controlling the cabin Yes, SYS1 is still controlling the cabin altitude through the safety altitude through the safety valvevalve. .

No, in this case the cabin altitude has to No, in this case the cabin altitude has to be controlled through be controlled through the LDG ELEV the 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 set On the CABIN PRESS panel with a LDG ELEV set manually, is there still an automatic control of the manually, is there still an automatic control of the cabin altitude? cabin altitude?

No, in this case the cabin altitude has to No, 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 the altitude through the outflowoutflow valve.valve.

7.6 7.6 psipsi

8.6 8.6 psipsi

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

5.3 5.3 psipsi

6.9 6.9 psipsi??

1.0 1.0 psipsi

8.6 8.6 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 the what should the differential pressure be on the ground, while at the gate? ground, while at the gate?

0 0 psipsi

0.5 0.5 psipsi

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

Can not be controlled manually and are Can not be controlled manually and are fully automatic.fully automatic.

On the CABIN PRESSURIZATION system, the safety valves….On the CABIN PRESSURIZATION system, the On 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 SEL Are controlled with the MODE SEL pbpb..

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 has On 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.

The air outlet valve.The air outlet valve.

The safety valve.The safety valve.

On the CABIN PRESS panel, pushing on the MODE SEL pb sw gives control overOn the CABIN PRESS panel, pushing on the MODE On the CABIN PRESS panel, pushing on the MODE SEL SEL pbpb swsw gives control overgives control over

The outflow valve.The outflow valve.

The air intake valve.The air intake valve.

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 cabin On the ECAM STATUS page, as you can see cabin pressure control is manual. You want descend from pressure 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.

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 set On the CABIN PRESS panel, with the MODE SEL set to MAN and the MAN V/S CTL held in the DN to 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.

What ventilation configuration is displayed on the CAB PRESS page?What ventilation configuration is displayed on the What 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).

What ventilation configuration is displayed on the CAB PRESS page?What ventilation configuration is displayed on the What 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).

Please indicate the position of the VENTILATION panel.Please indicate the position of the VENTILATION Please indicate the position of the VENTILATION panel.panel.

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

It is an indication that the aircraft has not It 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 system It is an indication that at least one system requires crew attention.requires crew attention.

It is an indication that there is at least one It 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 system It 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 engine On 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?

Press and hold the corresponding button Press 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 the Switch the SD to one of the PFDPFD’’ss..

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

The E/WD is automatically transferred to The E/WD is automatically transferred to one of the NDone of the ND’’s.s.

The E/WD is automatically transferred to The E/WD is automatically transferred to one of the one of the PFDPFD’’ss..

To get E/WD information, it must be To 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 be To get E/WD information, it must be manually transferred to one of the manually transferred to one of the PFDPFD’’ss..

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

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

ECAM cautions and warnings and auralECAM cautions and warnings and auralwarnings are lost.warnings are lost.

MASTER CAUTION light, MASTER MASTER CAUTION light, MASTER WARNING light and aural warnings are WARNING light and aural warnings are lost.lost.

MASTER CAUTION light, MASTER MASTER CAUTION light, MASTER WARNING light, aural warnings andWARNING light, aural warnings andECAM cautions and warnings are lost.ECAM cautions and warnings are lost.

On the ECAM SYSTEM in case of a double FWC failure...On the ECAM SYSTEM in case of a double FWC On the ECAM SYSTEM in case of a double FWC failure...failure...

The failure message has been previously The failure message has been previously cancelled with the EMER CANC cancelled with the EMER CANC pbpb..

The failure message had occurred during The failure message had occurred during the previous flight.the previous flight.

The FWC is working in a degraded mode The FWC is working in a degraded mode and is not able anymore to detect this and 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 a CANCELLED CAUTION mean?On the ECAM STATUS page , what does a On the ECAM STATUS page , what does a CANCELLED CAUTION mean?CANCELLED CAUTION mean?

By resetting the appropriate circuit By resetting the appropriate circuit breaker.breaker.

By pressing and holding any CLR By pressing and holding any CLR pbpb forformore than 3 seconds.more than 3 seconds.

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

By pressing and holding the RCL By pressing and holding the RCL pbpb for for more than 3 seconds.more than 3 seconds.

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

The location of the DFDR (Digital Flight Data Recorder) is :The location of the DFDR (Digital Flight Data The 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 tape and 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 protection In the passenger Cabin for protection reason.reason.

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 the The DFDR will be only energized after the first engine start.first engine start.

The DFDR is energized during 5 minutes The 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.

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 pb When 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.

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

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 on A fault light illuminating amber on overhead panel.overhead panel.

An ECAM caution message.An ECAM caution message.

A low frequency signal sounds through A low frequency signal sounds through the cockpit loud speaker.the cockpit loud speaker.

A MAINTENANCE message in the status A MAINTENANCE message in the status page.page.

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

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

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

Red.Red.

Amber.Amber.

Green.Green.

White.White.

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

Red.Red.

Amber.Amber.

Green.Green.

White.White.

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

Red.Red.

Amber.Amber.

Green.Green.

White.White.

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

On the ECAM SD page, what does an advisory message mean?On the ECAM SD page, what does an advisory On 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 of The parameter is out of limitslimits..

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

1.1 5.1

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 the E/WD page, what does the green arrow at the bottom of the page mean?bottom of the page mean?

It indicates that there is a It indicates that there is a STSSTS page page behind.behind.

It indicates that there is a system page It indicates that there is a system page behind.behind.

It means that there is more information It means that there is more information to be seen.to be seen.

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 observe On the ECAM ENGINE system page, you observe the VIB (N2) indication. What is the name of such an the 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

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

150 150 ktkt..

160 160 ktkt..

169 169 ktkt..

185 185 ktkt..

140

160

180

200

F

120

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

The present speed is 250 The present speed is 250 ktskts selected by selected by the crew and the MAX speed for lowering the crew and the MAX speed for lowering landing gear is VLE 230 landing gear is VLE 230 ktskts..

The aircraftThe aircraft’’s speed is 250 s speed is 250 ktskts which is a which is a managed speed. The symbol at 230 managed speed. The symbol at 230 ktsktsrepresents the VFE corresponding to the represents the VFE corresponding to the next flap lever position.next flap lever position.

The present speed of 250 The present speed of 250 ktskts is selected is selected by the crew. The circle at the bottom of by the crew. The circle at the bottom of the scale represents green dot speed the scale represents green dot speed which is the engine out operating speed which is the engine out operating speed in clean configuration. in clean configuration.

The = symbol at 230 The = symbol at 230 ktskts represents a represents a speed constraint. The circle on the speed constraint. The circle on the bottom represents green dot speed which bottom represents green dot speed which is the holding speed.is the holding speed.

220

240

260

280

=

o

On the PFD, the magenta symbols on the speed scale represent:On the PFD, the magenta symbols on the speed On the PFD, the magenta symbols on the speed scale represent:scale represent:

The ECON speed range during managed The ECON speed range during managed descent.descent.

The managed speed by the FMGS during The managed speed by the FMGS during managed climb.managed climb.

The upper magenta for high speed The upper magenta for high speed protection, the lower for turbulence protection, the lower for turbulence operating speed.operating speed.

The lower magenta symbol represents The lower magenta symbol represents VLS.VLS. .636

300

320

340

360

Is it possible to change the baro reference display from Hecto Pascals to inches of mercury and vice versa?

Is it possible to change the Is it possible to change the barobaro reference display reference display from from HectoHecto PascalsPascals to inches of mercury and vice to inches of mercury and vice versa?versa?

No, it is not possible because each airline No, 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 barobaroreference selector on the EFIS panel. reference selector on the EFIS panel.

No, the crew should refer to a conversion No, 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

On the PFD altimeter scale, which statement is correct ?On the PFD altimeter scale, which statement is On the PFD altimeter scale, which statement is correct ?correct ?

The crew is pushing the The crew is pushing the barobaro reference reference selector to change from STD setting to selector to change from STD setting to local QNH.local QNH.

Crew is pushing the Crew is pushing the barobaro reference reference selector to change from local QNH to the selector 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

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

180 180 ktkt..

191 191 ktkt..

215 215 ktkt..

250 250 ktkt..

140

160

180

250

220

S200

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

140 140 ktkt..

155 155 ktkt..

175 175 ktkt..

185 185 ktkt..

140

160

180

200

=

F

120

On the PFD, what is the meaning of the blue ribbon on the altitude scale?On the PFD, what is the meaning of the blue ribbon On 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 the It marks the preselectedpreselected altitude.altitude.

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

STD

FL 70

30.08QNH

7000

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

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.

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.

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.

On the PFD, which of the following statements is true?On the PFD, which of the following statements is On the PFD, which of the following statements is true?true?

The aircraft is in a climb, drifting to the The aircraft is in a climb, drifting to the left.left.

The aircraft is in a climb, drifting to the The aircraft is in a climb, drifting to the right.right.

The aircraft is in a descent, drifting to the The aircraft is in a descent, drifting to the left.left.

The aircraft is in a descent, drifting to the The aircraft is in a descent, drifting to the right.right.

On the ND, which of the following statements is true?On the ND, which of the following statements is On the ND, which of the following statements is true?true?

The heading to the next waypoint PAS isThe heading to the next waypoint PAS is108, it is at 28 NM, time left to the 108, 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 is108, it is at 28 NM, time to the destination108, it is at 28 NM, time to the destinationis 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 is108, it is at 28 NM, elapsed time of this 108, 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 is108, it is at 28 NM, it will be 108, it is at 28 NM, it will be overflownoverflown at at 9:08.9:08.

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 new ATC cleared you to FL 150. The PF sets the new altitude on the FCU. What will happen if he pulls the altitude on the FCU. What will happen if he pulls the ALT selection knob?ALT selection knob?

The aircraft will stop the climb at FL 60 The aircraft will stop the climb at FL 60 until passing the constraint then continue until passing the constraint then continue climb to FL 150.climb to FL 150.

The aircraft will disregard the The aircraft will disregard the constraintconstraintand climb to FL 150.and climb to FL 150.

As soon as the aircraft passes FL 60, the As soon as the aircraft passes FL 60, the target altitude on the PFD will change to target 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 PF The aircraft will level off at FL 60. The PF must pull the ALT selection knob a must pull the ALT selection knob a second time to climb to FL 150.second time to climb to FL 150.

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 climbing The 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 ALT What 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 PF The aircraft will level off at FL 60. The PF must push or pull the ALT selection knob must 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 the The aircraft will disregard the constraintconstraintand climb to FL 150.and climb to FL 150.

As soon as the aircraft passes FL 60, the As soon as the aircraft passes FL 60, the target on the PFD will change to FL 150 target 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 climb No change, the aircraft will stop the climb at FL 60 until passing the constraint then at FL 60 until passing the constraint then continue climb to FL 150.continue climb to FL 150.

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 climbing The 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/TRK What will happen if the PF pulls the HDG/TRK selection knob now?selection knob now?

The aircraft will continue on the present The 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 present The aircraft will stay on the present heading, disregard the constraint and heading, 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 the PLN, stop the climb at FL 60 until passing the constraint climb 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 to disregard the constraint and climb to FL 150.FL 150.

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 have On the MCDU, you notice that some waypoints have a small triangle behind the name. What does it a small triangle behind the name. What does it stand for?stand for?

It means these waypoints will be It means these waypoints will be overflownoverflown..

It means these waypoints are compulsory It means these waypoints are compulsory reporting points.reporting points.

It indicates altitude constraints at these It indicates altitude constraints at these waypoints.waypoints.

It indicates speed constraints at these It indicates speed constraints at these waypoints.waypoints.

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. What does it mean?What does it mean?

The FMGC warns you about a possible The FMGC warns you about a possible overspeedoverspeed..

TCAS discovered a possible traffic TCAS discovered a possible traffic conflict and warns you to decelerate to conflict and warns you to decelerate to keep your separation.keep your separation.

Due to some environmental Due to some environmental circumstances, the aircraft missed a circumstances, 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 to loose energy so that you will be able to intercept the descent path.intercept the descent path.

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, an The 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 automatically No procedure, the a/c will automatically resume the climb after having sequenced resume the climb after having sequenced the constrained waypoint. the constrained waypoint.

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

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 AP It is the FMGC corresponding to the AP engaged or FMGC1 when both AP engaged or FMGC1 when both AP engaged.engaged.

Randomly at power up.Randomly at power up.

It is the FMGC corresponding to the Pilot It is the FMGC corresponding to the Pilot Flying side.Flying side.

It is always FMGC1.It is always FMGC1.

The autothrust system has two channels. Which FMGC controls the A/THR (both FMGCs being operative)?

The The autothrustautothrust system has two channels. Which system has two channels. Which FMGC controls the A/THR (both FMGC controls the A/THR (both FMGCsFMGCs being being operative)?operative)?

The FMGC1.The FMGC1.

The FMGC2.The FMGC2.

The randomly chosen FMGC.The randomly chosen FMGC.

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 the Setting 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 the On the FMA, in the AutothrustAutothrust mode mode column.column.

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

Dashes in the FCU window indicate the system has enough information to manage the settings of the targets.Why is the altitude window not dashed?

Dashes in the FCU window indicate the system has Dashes in the FCU window indicate the system has enough information to manage the settings of the enough 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 the The altitude window shows digits as the target altitude is always set manually by target altitude is always set manually by the pilot.the pilot.

The altitude selector knob has not been The altitude selector knob has not been pushed. pushed.

The altitude selector knob has not been The altitude selector knob has not been pulled. pulled.

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

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

The target speed is managed by the The target speed is managed by the FMGC.FMGC.

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

The pilot has pulled the speed selector The pilot has pulled the speed selector knob.knob.

The The autothrustautothrust mode is speed.mode is speed.

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 appear speed selector knob, which speed value will appear on the FCU window ?on the FCU window ?

The max limit speed according to the The max limit speed according to the aircraft configuration.aircraft configuration.

VLS + 20 VLS + 20 ktkt..

The current speed.The current speed.

VMO or MMO.VMO or MMO.

When can you engage autopilots 1+2 at the same time?When can you engage autopilots 1+2 at the same When 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 for As soon as the APPR mode is armed for an ILS approach.an ILS approach.

As soon as the APPR mode is armed for a As soon as the APPR mode is armed for a non precision approach on managed non precision approach on managed mode.mode.

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.What does it mean?What does it mean?

ALT is armed and an altitude constraint ALT 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 target The aircraft is on descent and the target altitude is higher than the current aircraft altitude is higher than the current aircraft altitude.altitude.

The target altitude is above the glide The target altitude is above the glide slope altitude capture.slope altitude capture.

ALT is armed, the target altitude is given ALT is armed, the target altitude is given by the ALT window in the FCU.by the ALT window in the FCU.

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.

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 the PLN page. Notice the small white arrow shown on the right top. It small 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 displayed Another 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 be Another page is available and can be displayed by selecting the NEXT PAGE displayed by selecting the NEXT PAGE key.key.

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

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.

The standard instrument departure is shown on the navigation display, however an amber line can be seen:

The standard instrument departure is shown on the The standard instrument departure is shown on the navigation display, however an amber line can be navigation 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 instrument It is the engine out standard instrument departure.departure.

It is the standard departure for light It is the standard departure for light airplanes. airplanes.

Have a look at the MCDU, the ILS 23R is a currently selected approach, the green color means:Have a look at the MCDU, the ILS 23R is a currently Have 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 active This approach is inserted into the active FF--PLN.PLN.

This approach is displayed in green This 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.

The ILS 23L has been selected. On the MCDU, what is the meaning of the yellow font?The ILS 23L has been selected. On the MCDU, what The 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 the The selection has been made on the secondary FPLN.secondary FPLN.

This selection is definitely done and This selection is definitely done and cannot be erased.cannot be erased.

The selection is temporary (not yet The selection is temporary (not yet inserted).inserted).

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

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 waypoint shows VIA/GO TO data field, it is used:The lateral revision page from a FThe lateral revision page from a F--PLN waypoint PLN 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 by PLN waypoint by waypoint.waypoint.

After engines start, which page shall be used to enter any weight modification?After engines start, which page shall be used to After 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.

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

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 is The lateral guidance during takeoff roll is linked to the ILS localizer signal.linked to the ILS localizer signal.

The aircraft is automatically guided to The aircraft is automatically guided to maintain the runway center line.maintain the runway center line.

The runway used for takeoff is confirmed The runway used for takeoff is confirmed by ATC.by ATC.

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 is The 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.

Have a look at the ND. What is the meaning of the highlighted magenta symbol?Have a look at the ND. What is the meaning of the Have 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 be The altitude constraint cannot be satisfied.satisfied.

The aircraft will level off at that point to The aircraft will level off at that point to satisfy the altitude constraint.satisfy the altitude constraint.

The aircraft will resume the climb at that The aircraft will resume the climb at that point.point.

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 SRS On 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.

In this situation, what will happen if you push the HDG knob?In this situation, what will happen if you push the In 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 theFROM WPT and as such, the active legFROM WPT and as such, the active legcannot 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 tointercept the active leg.intercept the active leg.

The aircraft will follow the selected HDGThe aircraft will follow the selected HDGwhatever the action on the FCU is.whatever the action on the FCU is.

The selected target will change from a The selected target will change from a HDG to a TRK.HDG to a TRK.

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

The aircraft is guided by the The aircraft is guided by the autoflightautoflightsystem along the programmed missed system along the programmed missed approach navigation. approach navigation.

The aircraft is guided along a new route The aircraft is guided along a new route as the navigation accuracy level reverted as the navigation accuracy level reverted to to ““lowlow”” at the time of go around. at the time of go around.

The aircraft maintains the track followed The aircraft maintains the track followed at mode engagement.at mode engagement.

The aircraft proceeds on the fastest way The aircraft proceeds on the fastest way to come back for a new approach.to come back for a new approach.

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 the TOGA 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 full Only 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.

Why must the pilot press the take over pushbutton on the side stick twice to disconnect the autopilot?Why must the pilot press the take over pushbutton Why 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 autopilot A first time to disconnect the autopilot and a second time to confirm the and a second time to confirm the disconnection.disconnection.

A the first time to disconnect the autopilot A the first time to disconnect the autopilot and a second time to get a definite priority and a second time to get a definite priority on his side.on his side.

A first time to disconnect the autopilot A first time to disconnect the autopilot and a second time to reset all the related and a second time to reset all the related warnings.warnings.

A first time to disconnect the autopilot A first time to disconnect the autopilot and a second time to reset the master and a second time to reset the master FMGC.FMGC.

The The autothrustautothrust is active but the thrust is is active but the thrust is limited by the thrust levers position. limited by the thrust levers position.

The The autothrustautothrust is still active but can is still active but can control the thrust to IDLE only.control the thrust to IDLE only.

What does the “AUTOFLT A/THR LIMITED” message mean? What does the What does the ““AUTOFLTAUTOFLT A/THR LIMITEDA/THR LIMITED”” message message mean? mean?

The The autothrustautothrust is active but only one is active but only one channel is operative.channel is operative.

The maximum engine thrust has been The maximum engine thrust has been automatically reduced by the automatically reduced by the FADECsFADECs..

Both autopilots are engaged which FMGC is master?Both autopilots are engaged which FMGC is Both 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 two None as the two FMGCFMGC’’ss are acting are acting independently.independently.

FMGC 2FMGC 1

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

The switching occurs at every FMGC The switching occurs at every FMGC power up.power up.

It depends on which ATHR channel is It depends on which ATHR channel is engaged.engaged.

FMGC2.FMGC2.

FMGC1.FMGC1.

FMGC 2FMGC 1

In independent operation mode which FMGC is master?In independent operation mode which FMGC is In independent operation mode which FMGC is master?master?

FMGC1.FMGC1.

FMGC2.FMGC2.

None, the two None, the two FMGCFMGC’’ss are acting are acting independently.independently.

It depends on which FMGC was the It 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

What is the meaning of “OPP FMGC IN PROCESS”, the message displayed here in the scratchpad of MCDU1?

What is the meaning of What is the meaning of ““OPP FMGC IN PROCESSOPP FMGC IN PROCESS””, , the message displayed here in the scratchpad of the 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 better The FMGC2 performance became better than the FMGC1.than the FMGC1.

What is the meaning of “SET OFFSIDE RNG/MODE”which appears on ND1?What is the meaning of What 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 mode The selection of the offside range mode will allow the display of the navigation will allow the display of the navigation map on this side.map on this side.

The selection of the offside range mode The selection of the offside range mode will make the FMGCwill make the FMGC’’s resynchronization s resynchronization shorter. shorter.

The selection of the offside range mode The selection of the offside range mode will make the return on FMGC dual mode will make the return on FMGC dual mode easier.easier.

The selection of the offside range mode The selection of the offside range mode will reduce the FMGC1 reset duration at will reduce the FMGC1 reset duration at one minute.one minute.

FCU 1 failure has no consequences on the FCU 1 failure has no consequences on the FCU utilization, as the second channel FCU 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 the Only the lateral modes can be set from the FCU panel.FCU panel.

Some FCU functions LOC and APP Some 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?

The FCU 1 and 2 have failed, how the pilot can control the vertical and lateral modes?The FCU 1 and 2 have failed, how the pilot can The 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 controls s 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 be The vertical and lateral modes cannot be controlled from the FCU. Only the manual controlled from the FCU. Only the manual flight on raw data is possible. flight on raw data is possible.

The pilot can control the lateral and The pilot can control the lateral and vertical modes using the MCDU.vertical modes using the MCDU.

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

The pilot can engage both AP in all The pilot can engage both AP in all phases of flight.phases of flight.

The cross talk function is lost, each The cross talk function is lost, each FMGC will work independently, the same FMGC will work independently, the same entry has to be made on both entry has to be made on both MCDUsMCDUs..

There is no more radio updating of the There is no more radio updating of the FMGC position and only the mix IRS FMGC position and only the mix IRS coordinates are provided for the coordinates are provided for the navigation.navigation.

The FMGC1 failed and “OPP FMGC IN PROCESS” is displayed on the MCDU1. The FMGC2 has taken over automatically :

The FMGC1 failed and The FMGC1 failed and ““OPP FMGC IN PROCESSOPP FMGC IN PROCESS”” is is displayed on the MCDU1. The FMGC2 has taken displayed 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

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 1 modes 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, engage As the autopilot 1 disengages, engage autopilot 2.autopilot 2.

The PFD barometric reference is now only The PFD barometric reference is now only available on standard and the pilot must available on standard and the pilot must set the current set the current barobaro setting on the setting on the standby altimeter.standby altimeter.

The FCU2 has taken over automatically The FCU2 has taken over automatically and the and the barobaro reference must be cross reference must be cross checked.checked.

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 indefinitely Nothing, the aircraft follows indefinitely the selected HDG/TRK.the selected HDG/TRK.

The aircraft continues to follow The aircraft continues to follow the current HDG until Fthe current HDG until F--PLN interception.PLN interception.

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 until The aircraft follows the selected HDG until intercepting the lateral Fintercepting the lateral F--PLN.PLN.

Nothing, the aircraft continues on HDG Nothing, the aircraft continues on HDG 140 indefinitely.140 indefinitely.

Please indicate the position of the two FLIGHT DIRECTOR (FD) controls.Please indicate the position of the two FLIGHT Please indicate the position of the two FLIGHT DIRECTOR (FD) controls.DIRECTOR (FD) controls.

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

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 a The active lateral mode which is a constraint.constraint.

The armed lateral mode.The armed lateral mode.

The armed lateral mode which is a The armed lateral mode which is a constraint.constraint.

The active lateral mode.The active lateral mode.

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 a The active lateral mode which is a constraint.constraint.

The armed lateral mode.The armed lateral mode.

The armed lateral mode which is a The armed lateral mode which is a constraint.constraint.

The active lateral mode.The active lateral mode.

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.

The yaw bar, when displayed on the PFD instead of the flight director roll bar, is used to :The yaw bar, when displayed on the PFD instead of The 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 is Provide 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 1000 off up to 1000 feat AGL to maintain the runway center feat AGL to maintain the runway center line.line.

Confirm that the aircraft is well Confirm that the aircraft is well established in the glide slope on ILS final established in the glide slope on ILS final approach.approach.

Change over automatically in case of Change over automatically in case of localizer failure on ILS final approach.localizer failure on ILS final approach.

What does MAN TOGA indicate on the FMA column?What does MAN TOGA indicate on the FMA What does MAN TOGA indicate on the FMA column?column?

The thrust has been manually set to The thrust has been manually set to TOGA.TOGA.

The The autothrustautothrust system is inoperative.system is inoperative.

The FMGC guidance The FMGC guidance autothrustautothrust command command is unserviceable. is unserviceable.

The pilot has disconnected the The pilot has disconnected the autothrustautothrustsystem.system.

The The autothrustautothrust will be automatically will be automatically activated by the FMGC without any pilot activated by the FMGC without any pilot action when crossing the thrust reduction action when crossing the thrust reduction altitude.altitude.

The The autothrustautothrust will become active when will become active when the pilot sets the thrust levers in the climb the pilot sets the thrust levers in the climb detent.detent.

The thrust levers must be set to idle and The thrust levers must be set to idle and then in the climb detent to activate the then in the climb detent to activate the autothrustautothrust..

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

“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 reduction We have crossed the thrust reduction altitude.altitude.

The The autothrustautothrust levers are stuck and can levers 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 FLEX The pilot has forgotten to enter the FLEX temperature on the MCDU taketemperature on the MCDU take--off page off page before taking off.before taking off.

The thrust levers will automatically move The thrust levers will automatically move to the climb detent.to the climb detent.

The constant rate of climb is maintained The constant rate of climb is maintained by the autopilot.by the autopilot.

You are established in climb, THR CLB mode is active: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 and The 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 AP A/THR commands CLB thrust and AP maintains the target speed by using pitch maintains the target speed by using pitch adjustments.adjustments.

The speed and the rate of climb are The speed and the rate of climb are controlled by the thrust.controlled by the thrust.

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 is The aircraft has leveled off at 13000 feet, ALT is green on the FMA and the green on the FMA and the autothrustautothrust is in SPEED is in SPEED mode:mode:

The target speed and the altitude are The target speed and the altitude are maintained by the autopilot. maintained by the autopilot.

The target speed is maintained by the The target speed is maintained by the autopilot and the altitude is controlled by autopilot and the altitude is controlled by the the autothrustautothrust. .

The The autothrustautothrust system controls the thrust system controls the thrust to maintain the target speed and the to maintain the target speed and the autopilot maintain the altitude by autopilot maintain the altitude by adjusting the pitch.adjusting the pitch.

The altitude and speed are maintained by The altitude and speed are maintained by the A/THR. the A/THR.

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

Why do you set the thrust levers to IDLE for landing?Why do you set the thrust levers to IDLE for Why do you set the thrust levers to IDLE for landing?landing?

To engage the manual mode of the To 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.

According to these indications, what is the correct statement?According to these indications, what is the correct According 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.

ALT mode is engaged, MCDU PERF page indicates CLB. Why?ALT mode is engaged, MCDU PERF page indicates ALT 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 below FL290 is the FCU selection, and is below the CRZ FL.the CRZ FL.

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 page ALT mode is engaged at FL290, MCDU PERF page indicates CLB. How do you obtain ALT CRZ on the indicates 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 on Set 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 to Push the altitude selector knob to continue the climb as programmed continue the climb as programmed before.before.

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 :

The The autothrustautothrust maintain the thrust at idle maintain the thrust at idle and the auto pilot adjust the pitch to and the auto pilot adjust the pitch to maintain the target speed.maintain the target speed.

The The autothrustautothrust adjust the thrust to adjust the thrust to maintain the target speed and the maintain the target speed and the autopilot control the descent flight path.autopilot control the descent flight path.

The The autothrustautothrust maintain the thrust at idle maintain the thrust at idle and the autopilot control the vertical and the autopilot control the vertical speed.speed.

The The autothrustautothrust control the target speed control the target speed and the rate of descent.and the rate of descent.

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 the Automatically when the aircraft overfly the deceleration point or manually by the pilot deceleration point or manually by the pilot on the PERF pageon the PERF page

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

Only automatically at the deceleration Only automatically at the deceleration point.point.

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

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

By pressing the approach mode By pressing the approach mode pushbutton.pushbutton.

By setting TOGA to engage the go around By setting TOGA to engage the go around mode.mode.

What is the meaning of the small magenta dot displayed by the altitude scale?What is the meaning of the small magenta dot What 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 wrong It 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 be It warns the pilot that the speed must be reduced to regain the computed descent reduced to regain the computed descent profile.profile.

It indicates that the expedite mode must It indicates that the expedite mode must be engaged.be engaged.

It highlights any vertical deviation of the It highlights any vertical deviation of the aircraft from the computed descent aircraft from the computed descent profile.profile.

I use the MECH pb I 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 keyon 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 see t see him. How do you get his attention?him. How do you get his attention?

I open the side window and try to I open the side window and try to get his attention.get his attention.

On the RCDR control panel, press the On the RCDR control panel, press the GND CTL pb to switch the CVR ON, then GND CTL pb to switch the CVR ON, then press the CVR TEST pb.press the CVR TEST pb.

The CVR TEST can only be performed The CVR TEST can only be performed after one engine is started then after one engine is started then ““BB””answer is applied.answer is applied.

Be sure the PARKING BRK is ON then Be sure the PARKING BRK is ON then repeat repeat ““BB”” answer.answer.

During Preflight, check of the CVR operation is performed as follow.During Preflight, check of the CVR operation is During Preflight, check of the CVR operation is performed as follow.performed as follow.

The system being operative as soon as The system being operative as soon as aircraft aircraft ElecElec Power network is powered, Power network is powered, on the RCDR Control panel, press the on the RCDR Control panel, press the CVR TEST pb, you get an audio signal for CVR TEST pb, you get an audio signal for correct operation.correct operation.

The aircraft must be on the ground with The aircraft must be on the ground with at 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 at The 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 with The aircraft must be on the ground with the parking brake set.the parking brake set.

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

It indicates that RMP1 is configured to It indicates that RMP1 is configured to tune VFH2.tune VFH2.

It indicates that RMP2 is configured to It indicates that RMP2 is configured to tune VHF2.tune VHF2.

On the RMP control panel, what does the white SEL light mean?On the RMP control panel, what does the white SEL On 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

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

False.False.

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

True.True.

False.False.

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

False.False.

On the communication control panel, the amber CALL light indicates that somebody is trying to reach you via VHF 3.

On the communication control panel, the amber On the communication control panel, the amber CALL light indicates that somebody is trying to CALL 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 notice the red FAULT light on the RAT & EMER GEN pushbutton.How do you interpret this indication ?

You are in an ELECTRICAL EMERGENCY You are in an ELECTRICAL EMERGENCY CONFIGURATION, shortly after the fault occurred, CONFIGURATION, shortly after the fault occurred, you notice the red FAULT light on the RAT & EMER you 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 thesystem.system.

The fault light on the RAT & EMER GEN The fault light on the RAT & EMER GEN pbpb will extinguish by depressing it.will extinguish by depressing it.

The FAULT light is always on when youThe FAULT light is always on when youare in ELEC EMER CONFIG.are in ELEC EMER CONFIG.

You are in an ELECTRICAL EMERGENCY CONFIGURATION, on ELEC panel you have 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 ?

You are in an ELECTRICAL EMERGENCY You are in an ELECTRICAL EMERGENCY CONFIGURATION, on ELEC panel you have CONFIGURATION, on ELEC panel you have depressed the GEN 1 and GEN 2 depressed 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 TIE Why must you push the BUS TIE pbpb swsw to OFF ?to OFF ?

To separate both sides of the electricalTo separate both sides of the electricalsystem.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 electricalsystem.system.

To switch both generators to the oppositeTo switch both generators to the oppositeside AC BUS.side AC BUS.

In an ELECTRICAL EMERGENCY CONFIGURATION, after performing the initial ECAM procedure, you have separated both sides of the electrical system.Why do you have to try another generator reset ?

In an ELECTRICAL EMERGENCY CONFIGURATION, In an ELECTRICAL EMERGENCY CONFIGURATION, after performing the initial ECAM procedure, you after 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 mightrecover 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 besuccessful.successful.

You should always try two resets if youYou should always try two resets if youhave a generator failure.have a generator failure.

Reconnect the generator to its drive Reconnect the generator to its drive mechanism.mechanism.

Disconnect the corresponding generator Disconnect 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 supply Cut the corresponding generator supply to AC bus 1 or 2.to AC bus 1 or 2.

Cut the corresponding generator supply Cut the corresponding generator supply to the ESS AC bus.to the ESS AC bus.

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

At the engine RPM trough their gearbox At the engine RPM trough their gearbox connection.connection.

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

At a intermediate speed controlled by an At a intermediate speed controlled by an electronic computer.electronic computer.

No necessity to control the generator No necessity to control the generator speed because the AC network operates speed 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 BUS and DC ESS BUS.In normal configuration :

The Electrical System includes two buses: AC ESS The Electrical System includes two buses: AC ESS 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 the To balance the ElecElec load GEN 1 is directly load GEN 1 is directly supplying the AC ESS BUS.supplying the AC ESS BUS.

To balance the To balance the ElecElec load GEN 2 is directly load 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 pilot to switchover the supply of AC ESS bus.The purpose of AC ESS FEED pb The purpose of AC ESS FEED pb swsw is to enable is 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.

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

The emergency electrical generator used as a back up is hydraulically driven by the RAT which automatically extends when both AC BUS 1 and AC BUS 2 are lost and the aircraft speed is above 100kts.

The emergency electrical generator used as a back The emergency electrical generator used as a back up is hydraulically driven by the RAT which up is hydraulically driven by the RAT which automatically extends when both AC BUS 1 and AC automatically extends when both AC BUS 1 and AC BUS 2 are lost and the aircraft speed is above BUS 2 are lost and the aircraft speed is above 100kts.100kts.

True.True.

False.False.

From ECAM ELEC page, the APU GEN box information indicates that:From ECAM ELEC page, the APU GEN box From ECAM ELEC page, the APU GEN box information indicates that:information indicates that:

The APU GEN does not have priority over The APU GEN does not have priority over the external power.the external power.

The APU GEN The APU GEN pbpb SW on overhead panel SW on overhead panel is 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 GEN:Looking at the ECAM ELEC Page, to connect APU Looking at the ECAM ELEC Page, to connect APU GEN:GEN:

Push APU GEN pb Push APU GEN pb swsw located overhead located 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 ?

APU GEN shares 36% of the APU GEN shares 36% of the elecelec network network load, the remaining 64% being taken by load, 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 the The external power is supplying the network.network.

During preliminary procedure to check the battery voltage, the associated BATT pb sw should be:During preliminary procedure to check the battery During preliminary procedure to check the battery voltage, the associated BATT voltage, the associated BATT pbpb swsw should be:should be:

Switched ON.Switched ON.

Switched OFF.Switched OFF.

Any position, the voltage indication being Any position, the voltage indication being all time available.all time available.

The minimum battery voltage for normal operation should be:The minimum battery voltage for normal operation The minimum battery voltage for normal operation should be:should be:

24V.24V.

25,5V.25,5V.

28V.28V.

The EXT PWR AVAIL illuminated green on the overhead panel means that :The EXT PWR AVAIL illuminated green on the The EXT PWR AVAIL illuminated green on the overhead panel means that :overhead panel means that :

The ground cart is supplying the aircraft The ground cart is supplying the aircraft network.network.

The external power is plugged in and The external power is plugged in and delivers bleed air.delivers bleed air.

The connected ground cart voltage and The connected ground cart voltage and frequency are normal. frequency are normal.

On EXT PWR pb sw, the illuminated cyan light means that:On EXT PWR On EXT PWR pbpb swsw, the illuminated cyan light , the illuminated cyan light means that:means that:

The ground cart is supplying the aircraft The ground cart is supplying the aircraft electrical network.electrical network.

External power is plugged in but not External power is plugged in but not supplying the network.supplying the network.

External power is plugged in and delivers External power is plugged in and delivers bleed air only.bleed air only.

After starting engine n°2, is the present ECAM ELEC page a correct configuration?After starting engine nAfter starting engine n°°2, is the present ECAM 2, is the present ECAM ELEC page a correct configuration?ELEC page a correct configuration?

No. ENG GEN nNo. ENG GEN n°°2 should power all 2 should power all aircraft network.aircraft network.

No. The APU GEN should continue No. The APU GEN should continue powering all aircraft network.powering all aircraft network.

Yes. ENG GEN nYes. ENG GEN n°°2 is now powering its 2 is now powering its own side.own side.

You have to switch each battery on by its You have to switch each battery on by its associated associated pbpb swsw to check the voltage.to check the voltage.

As you enter in the dark cockpit you first check the battery voltages. What are the necessary checks before checking the voltages?

As you enter in the dark cockpit you first check the As you enter in the dark cockpit you first check the battery voltages. battery voltages. What are the necessary checks before checking the What 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 voltages immediately. No actions are required.immediately. No actions are required.

In flight, following an AC BUS 1 FAULT, AC ESS FEED pb sw must be depressed in order to:In flight, following an AC BUS 1 FAULT, AC ESS In flight, following an AC BUS 1 FAULT, AC ESS FEED pb FEED 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 DC and AC ESS buses loss:AC BUS 1 FAULT will definitively lead to the DC AC BUS 1 FAULT will definitively lead to the DC 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 be No. DC and AC ESS buses will be recovered by pushing on the AC ESS recovered by pushing on the AC ESS FEED FEED pbpb swsw..

Following an AC BUS 1 fault, pushing the AC ESS FEED pb sw on ELEC overhead panel allows you:Following an AC BUS 1 fault, pushing the AC ESS Following an AC BUS 1 fault, pushing the AC ESS FEED FEED 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 is illuminated.What does it mean?

Following the RAT extension due to ELEC EMER Following the RAT extension due to ELEC EMER CONF, the RAT and EMER GEN FAULT light is CONF, the RAT and EMER GEN FAULT light is illuminated.illuminated.What does it mean?What does it mean?

We had an ELEC EMER configuration, the We had an ELEC EMER configuration, the RAT is extended.RAT is extended.

The fault stays illuminated even after The fault stays illuminated even after emergency generator connection.emergency generator connection.

The emergency generator is not The emergency generator is not connected. connected.

In case of ELEC EMER CONF, LAND ASAP in red is displayed on the E/WD.This message will stay:

In case of ELEC EMER CONF, LAND ASAP in red is In case of ELEC EMER CONF, LAND ASAP in red is displayed on the E/WD.displayed on the E/WD.This message will stay:This message will stay:

As long as the Red warning ELEC EMER As long as the Red warning ELEC EMER CONF persists.CONF persists.

Even after having reset one generator Even after having reset one generator successfully.successfully.

Even if BUS TIE pb Even 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 segregated e.g to isolate a short circuit ?

In case of an ELEC EMER CONFIG situation, how In case of an ELEC EMER CONFIG situation, how can the two sides of the electrical system be can the two sides of the electrical system be segregated e.g to isolate a short circuit ?segregated e.g to isolate a short circuit ?

Push BUS TIE Push BUS TIE pbpb SW located on ELEC SW located on ELEC system overhead panel.system overhead panel.

Reset each AC generator.Reset each AC generator.

Manually lower RAT by pushing its Manually lower RAT by pushing its pbpb SWSW

Nothing has to be done because the Nothing has to be done because the segregation is done automatically.segregation is done automatically.

Being in an EMER ELEC configuration what is happening when A/C speed drops below 140 kts? Being in an EMER ELEC configuration what is Being in an EMER ELEC configuration what is happening when A/C speed drops below 140 happening when A/C speed drops below 140 ktskts? ?

AC generators are less powerful due to AC generators are less powerful due to RAT speed decrease.RAT speed decrease.

Electrical network is automatically Electrical network is automatically transferred to the batteries.transferred to the batteries.

You have to stop AC generator by You have to stop AC generator by pressing the pressing 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.Can you manually call an ECAM system page ?

In ELEC EMER CONF, you are in single display In ELEC EMER CONF, you are in single display mode on the ECAM.mode on the ECAM.Can you manually call an ECAM system page ?Can you manually call an ECAM system page ?

No. The upper ECAM screen is only used No. 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 associated associated pbpb SW on the ECAM control SW on the ECAM control panel.panel.

In EMER ELEC CONF, when the RAT stalls due to A/C speed decreasing, the static inverter will become active in order to supply:

In EMER ELEC CONF, when the RAT stalls due to In EMER ELEC CONF, when the RAT stalls due to A/C speed decreasing, the static inverter will A/C speed decreasing, the static inverter will 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. What will happen?

In case of avionics bay smoke, GEN 1 LINE In case of avionics bay smoke, GEN 1 LINE pbpb is is selected OFF. selected OFF. What will happen?What will happen?

All warnings will be reset.All warnings will be reset.

The smoke in the avionic bay will be The smoke in the avionic bay will be evacuated.evacuated.

GEN1 will be disconnected from the GEN1 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 is true ?According to these indications, which statement is According to these indications, which statement is true ?true ?

Both battery voltages are above the Both battery voltages are above the minimum of 20 V.minimum of 20 V.

Both battery voltages are below the Both battery voltages are below the minimum of 25.5 V.minimum of 25.5 V.

I can only check the battery voltages on I can only check the battery voltages on the ECAM ELEC page.the ECAM ELEC page.

I can only check the battery voltages, with I 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?

External power is available. I only have to External power is available. I only have to switch the batteries to on and they will be switch the batteries to on and they will be charged. charged.

I have to switch the external power and I have to switch the external power and the batteries to on and the batteries will the batteries to on and the batteries will be charged.be charged.

I have to switch the external power to ON I 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 the I have to call a mechanic because the batteries can only be charged by batteries 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 ?

The external power is plugged in and the The external power is plugged in and the voltage and frequency parameters are voltage and frequency parameters are normal.normal.

The external power is plugged in.The external power is plugged in.

The external power panel door has been The external power panel door has been opened.opened.

The AVAIL light always illuminates on The AVAIL light always illuminates on ground.ground.

After having switched the external power to ON, you get the following indications. How do you interpret the amber generator parameters and the generator fault lights ?

After having switched the external power to ON, After having switched the external power to ON, you get the following indications. How do you you get the following indications. How do you interpret the amber generator parameters and the interpret the amber generator parameters and the 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. The A 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 indicationsshould disappear after 30 seconds.should disappear after 30 seconds.

On ground these indications are normal On 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 take ?

Both batteries are now being charged by the Both batteries are now being charged by the external power unit.external power unit.Approximately how long does the charging process Approximately how long does the charging process take ?take ?

10 minutes10 minutes

One hourOne 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 page After 20 minutes you check the ECAM ELEC page again. again. Which statement is true ?Which statement is true ?

Both battery voltages are still below the Both battery voltages are still below the minimum voltage.minimum voltage.

To check the battery voltages I have to To check the battery voltages I have to switch them OFF first.switch them OFF first.

To check the battery voltages I have to To check the battery voltages I have to disconnect external power first.disconnect external power first.

Both battery voltages are now above the Both 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 external power only ?

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 by Why is the electrical system still supplied by 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 the different generators ?

The APU generator is supplying the electrical The APU generator is supplying the electrical system.system.By the way, do you know the order of priority for By the way, do you know the order of priority for 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 red On 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 ?

I push the disconnect button and release I push the disconnect button and release it immediately in order to prevent the it immediately in order to prevent the disconnect mechanism from being disconnect mechanism from being damaged.damaged.

I push the disconnect button until the I push the disconnect button until the GEN FAULT light comes on and then for GEN FAULT light comes on and then for at least 3 more seconds in order to ensureat least 3 more seconds in order to ensurethe disconnection.the disconnection.

I push the disconnect button for at leastI push the disconnect button for at least10 seconds to ensure the disconnection.10 seconds to ensure the disconnection.

I push the disconnect button until the I push the disconnect button until the GEN FAULT light comes on but not more GEN FAULT light comes on but not more than 3 seconds otherwise the disconnect than 3 seconds otherwise the disconnect mechanism may be damaged.mechanism may be damaged.

Is the ELEC ECAM system page in accordance with the both engines running electrical configuration ?Is the ELEC ECAM system page in accordance with Is the ELEC ECAM system page in accordance with the both engines running electrical configuration ?the both engines running electrical configuration ?

Yes.Yes.

No. The APU should continue powering No. The APU should continue powering the 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 this ECAM ELEC page configuration correct ? At the gate, with both engines shut down, is this At the gate, with both engines shut down, is this ECAM ELEC page configuration correct ? ECAM ELEC page configuration correct ?

Yes.Yes.

No.No.

The crew should shut down one engine at The 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 selected What will happen when EXT POWER is selected ON? ON?

The APU GEN will be disconnected and The APU GEN will be disconnected and will stop.will stop.

The EXT POWER will supply the A/C The EXT POWER will supply the A/C network.network.

The APU and ground power will both The APU and ground power will both supply the A/C network .supply the A/C network .

The transfer between APU supply and The transfer between APU supply and ground power will take place only after ground power will take place only after depressing the APU/GEN pb depressing the APU/GEN pb swsw to stop to stop the APU supply. the APU supply.

GEN 1 is now inoperative due to the ECAM procedure application following an IDG OIL LO PR caution.Is the associated AC BUS still available?

GEN 1 is now inoperative due to the ECAM GEN 1 is now inoperative due to the ECAM procedure application following an IDG OIL LO PR procedure application following an IDG OIL LO PR caution.caution.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 AC No. GEN 2 will be disconnected from AC BUS 2 within 10 minutes.BUS 2 within 10 minutes.

No. APU must be started to recover AC No. 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 swpressed for:

When executing ECAM action following an IDG OIL When executing ECAM action following an IDG OIL LO PR, the crew will have to hold IDG pb LO PR, the crew will have to hold IDG pb swswpressed for:pressed for:

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, how do you off load the generator?In case of GEN 2 OVERLOAD ECAM caution, how In case of GEN 2 OVERLOAD ECAM caution, how do you off load the generator?do you off load the generator?

By starting the APU to connect a third By 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 to By transferring load on GEN1 in order to keep the galley operating.keep the galley operating.

Following a GEN 2 OVERLOAD and the shedding of the galley is the ELEC page correct?Following a GEN 2 OVERLOAD and the shedding of Following a GEN 2 OVERLOAD and the shedding of the galley is the ELEC page correct?the galley is the ELEC page correct?

Yes.Yes.

No. The GEN overload should stay amber.No. The GEN overload should stay amber.

No. The GALLEY SHED message should No. The GALLEY SHED message should be removed.be removed.

Which of those area, has NO fire extinguishing system installed?Which of those area, has NO fire extinguishing Which of those area, has NO fire extinguishing system installed?system installed?

Avionic bay.Avionic bay.

Cargo compartments.Cargo compartments.

Engine / APU.Engine / APU.

Cabin.Cabin.

Please identify which of those area has a FIRE and OVERHEAT DETECTION system installed.Please identify which of those area has a FIRE and Please identify which of those area has a FIRE and OVERHEAT DETECTION system installed.OVERHEAT DETECTION system installed.

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 to Before performing the APU fire test, you have to check that...check that...

The APU FIRE The APU FIRE pbpb is in and guarded andis in and guarded andAC power is supplied.AC power is supplied.

The APU FIRE The APU FIRE pbpb is in and guarded andis in and guarded andthe APU is running.the APU is running.

The APU FIRE The APU FIRE pbpb is in with the guard inis in with the guard inthe UP position and the AGENT light isthe UP position and the AGENT light isextinguished.extinguished.

The APU FIRE The APU FIRE pbpb is in and guardedis in and guardedand 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?

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 cockpit In this case, during the preliminary cockpit preparation the APU FIRE test will trigger the preparation the APU FIRE test will trigger the following indications:following indications:

On the FIRE Control Panel, the APU FIRE On the FIRE Control Panel, the APU FIRE light, the SQUIB and DISCH lights will light, the SQUIB and DISCH lights will illuminate. Additionally, APU FIRE illuminate. Additionally, APU FIRE warning will be triggered on ECAM.warning will be triggered on ECAM.

On the FIRE Control Panel, the APU FIRE On 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 be But the APU FIRE warning will not be triggered on ECAM.triggered on ECAM.

No test is possible until AC power is No 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.

True.True.

False.False.

Does the APU fire test on battery trigger the CRC and MASTER WARN?Does the APU fire test on battery trigger the CRC Does the APU fire test on battery trigger the CRC and MASTER WARN?and MASTER WARN?

Yes.Yes.

No.No.

With the following indication on ECAM, what is the FIRE DETECTION status?With the following indication on ECAM, what is the With the following indication on ECAM, what is the FIRE DETECTION status?FIRE DETECTION status?

One fire detection loop has failed.One fire detection loop has failed.Fire detection for both engines is stillFire detection for both engines is stillavailable.available.

Both fire detection loops of engine 1 haveBoth fire detection loops of engine 1 havefailed. 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 hasfailed. Fire detection for engine 1 is stillfailed. Fire detection for engine 1 is stillavailable.available.

One fire detection loop of engine 1 hasOne fire detection loop of engine 1 hasfailed. Fire detection for engine 1 isfailed. Fire detection for engine 1 isinoperative.inoperative.

FDU

According to this ECAM E/WD page, the associated procedure isAccording to this ECAM E/WD page, the associated According to this ECAM E/WD page, the associated procedure isprocedure is

An indication presenting the FWD CARGO An indication presenting the FWD CARGO SMOKE condition only.SMOKE condition only.

To press the illuminated red FWD SMOKE To press the illuminated red FWD SMOKE DISCH pb.DISCH pb.

To lift the red guard and press the DISCH To lift the red guard and press the DISCH pb.pb.

This is an automatic This is an automatic fonctionfonction and you and you have to press FWD SMOKE pb to confirm.have to press FWD SMOKE pb to confirm.

The FWD and AFT fire bottles have bothThe FWD and AFT fire bottles have bothbeen discharged into their associatedbeen discharged into their associatedcompartment.compartment.

Now there is no longer any available Now there is no longer any available agent which can be discharged in either agent 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 bothbeen discharged into the FWD been discharged into the FWD compartcompart--mentment..

On the CARGO SMOKE control PANEL both DISCH lights illuminated mean that:On the CARGO SMOKE control PANEL both DISCH On the CARGO SMOKE control PANEL both DISCH lights illuminated mean that:lights illuminated mean that:

There is only one fire bottle which hasThere is only one fire bottle which hasbeen discharged into both cargobeen discharged into both cargocompartments.compartments.

According to these indications, which flight control law is active ?According to these indications, which flight control According to these indications, which flight control law is active ?law is active ?

Normal LawNormal Law

Alternate LawAlternate Law

Direct LawDirect Law

Mechanical Back UpMechanical Back Up

According to these indications, which flight control law is active ?According to these indications, which flight control According to these indications, which flight control law is active ?law is active ?

Normal LawNormal Law

Alternate LawAlternate Law

Direct LawDirect Law

Mechanical Back UpMechanical Back Up

Observe the PFD.Without any sidestick inputs...Observe the PFD.Observe the PFD.Without any Without any sidesticksidestick inputs...inputs...

The aircraftThe aircraft’’s attitude will s attitude will sstay constant.tay constant.

The pitch will stay constant, theThe pitch will stay constant, thebank angle will slowly decrease.bank angle will slowly decrease.

The bank angle will stay The 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 tendtowards towards ““wings levelwings level”” and and ““pitch 0pitch 0””..

The Alpha Floor protection has been The Alpha Floor protection has been triggered.triggered.

The Load Factor Limitation has been The Load Factor Limitation has been triggered.triggered.

There is no protection triggered yet.There is no protection triggered yet.

The High Angle Of Attack protection has The High Angle Of Attack protection has been triggered.been triggered.

According to the following indications...According to the following indications...According to the following indications...

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 pulled s assume, you have set idle power and pulled the the sidesticksidestick back to maintain altitude. Observe the back to maintain altitude. Observe the PFD. If you release the PFD. If you release the sidesticksidestick now...now...

The aircraft will descend at 150 The aircraft will descend at 150 ktskts..

The aircraft will maintain altitude until The aircraft will maintain altitude until 120 120 ktskts are reached .are reached .

The aircraft will maintain altitude until a The aircraft will maintain altitude until a stall occurs.stall occurs.

The aircraft will descend at 135 The aircraft will descend at 135 ktskts..

According to these indications...According to these indications...According to these indications...

The Alpha Floor protection has been The Alpha Floor protection has been triggered.triggered.

The Load Factor Limitation has been The Load Factor Limitation has been triggered.triggered.

There is no triggered protection.There is no triggered protection.

The High Angle Of Attack protection has The High Angle Of Attack protection has been triggered.been triggered.

According to these indications, if the sidestick is held in the full back position...According to these indications, if the According to these indications, if the sidesticksidestick is is held in the full back position...held in the full back position...

The speed will fall below 120 The speed will fall below 120 ktskts..The airplane might stall.The airplane might stall.

The speed will fall below 120 The 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 willoverride the override the sidesticksidestick input. The pitch willinput. The pitch willbe lowered to maintain 120 be lowered to maintain 120 ktskts..

The speed will fall further.The speed will fall further.At 114 At 114 ktskts the pitch will be lowered tothe pitch will be lowered tomaintain 114 maintain 114 ktskts..

Observe the PFD. Which statement is true ?Observe the PFD. Observe the PFD. Which statement is true ?Which statement is true ?

The Alpha Floor protection has The Alpha Floor protection has automatically set CLB power.automatically set CLB power.

The Alpha Floor protection has The Alpha Floor protection has automatically set TO/GA power.automatically set TO/GA power.

The Alpha Floor protection will override The Alpha Floor protection will override sidesticksidestick inputs. The nose will be inputs. 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...

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 ?

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 20Yes, 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 ?

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 80Yes, bank is limited to 80ºº..

aa

bb

How do you interpret the amber crosses on the PFD ?How do you interpret the amber crosses on the How do you interpret the amber crosses on the PFD ?PFD ?

The The autotrimautotrim is lost. You have to use is lost. You have to use manual pitch trim.manual pitch trim.

The ailerons are controlled directly by the The 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 fully right.Which indications do you expect ?

The The CPTCPT’’ss sidesticksidestick is deflected fully left and the is deflected fully left and the FOFO’’s s sidesticksidestick is simultaneously deflected fully is simultaneously deflected fully right.right.Which indications do you expect ?Which indications do you expect ?

If both pilots deflect their sidesticks fully back...If both pilots deflect their If both pilots deflect their sidestickssidesticks fully back...fully back...

The The ““pitch uppitch up”” order is twice as great as order is twice as great as compared only one stick deflected.compared only one stick deflected.

The The ““pitch uppitch up”” order is 1.5 times greaterorder is 1.5 times greateras 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 controlcomputers unless one pilot presses thecomputers unless one pilot presses thetake over take over pbpb on his stick.on his stick.

The The ““pitch uppitch up”” order is equal to a singleorder is equal to a singlestick fully deflected. stick fully deflected.

If the FO presses the take over pb...If the FO presses the take over If the FO presses the take over pbpb......

The CPT is unable to reThe CPT is unable to re--activate hisactivate hissidesticksidestick..

The The CPTCPT’’ss sidesticksidestick is still active. It will is still active. It will be debe de--activated after 40 activated after 40 secssecs..

The CPT can reThe CPT can re--activate his activate his sidesticksidestick bybypressing the take over pressing the take over pbpb for more thanfor more than40 40 secssecs..

The CPT can reThe CPT can re--activate his activate his sidesticksidestickimmediately by pressing his take over immediately by pressing his take over pbpb..

FOFOCPTCPT

Let’s assume the FO presses his take over pb and releases it after more than 40 secs...LetLet’’s assume the FO presses his take over s assume the FO presses his take over pbpb and and releases it after more than 40 releases it after more than 40 secssecs......

The The CPTCPT’’ss sidesticksidestick is deis de--activated unless activated unless he presses his take over he presses his take over pbpb..

The CPT is unable to reThe CPT is unable to re--activate his activate his sidesticksidestick for the rest of the flight.for the rest of the flight.

Both Both sidestickssidesticks are active.are active.

The The CPTCPT’’ss sidesticksidestick is active as long as is active as long as the FOthe FO’’s s 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 ?

Both Both sidestickssidesticks are locked in neutralare locked in neutralposition. The lock can not be overriddenposition. The lock can not be overridden

Both Both sidestickssidesticks are deare de--activated untilactivated untilthe AP is disengaged.the AP is disengaged.

Both Both sidestickssidesticks are locked in neutralare locked in neutralposition. By applying a certain force, theposition. By applying a certain force, thelock can be overridden but the AP lock can be overridden but the AP remains engaged.remains engaged.

Both Both sidestickssidesticks are locked in neutralare locked in neutralposition. By applying a certain force, theposition. By applying a certain force, thelock can be overridden and the AP islock can be overridden and the AP isdisengaged.disengaged.

What will happen next ?What will happen next ?What will happen next ?

The left SPLR 3 will be retracted, the right The left SPLR 3 will be retracted, the right SPLR 3 will be inhibited to prevent SPLR 3 will be inhibited to prevent asymmetry.asymmetry.

The right SPLR 3 will be extended to The right SPLR 3 will be extended to prevent asymmetry.prevent asymmetry.

Left SPLR 3 remains extended, spoiler Left SPLR 3 remains extended, spoiler operation is not possible anymore.operation is not possible anymore.

After a turn, you have the following message. What happened ?After a turn, you have the following message. What After a turn, you have the following message. What happened ?happened ?

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 VFE Speed (red barber pole)?What will happen just before the speed reaches VFE What will happen just before the speed reaches VFE Speed (red barber pole)?Speed (red barber pole)?

Auto flap retraction at 210 Auto flap retraction at 210 ktskts..

Auto flap and slat retraction at 210 Auto 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, the the autothrustautothrust will reduce thrust.will reduce thrust.

F/CTL FLAPS LOCKED

-WING TIP BRK ON

MAX SPEED . . . . . . . .

The message WING TIP BRK ON appears on the E/WD. What does it mean?The message WING TIP BRK ON appears on the The message WING TIP BRK ON appears on the E/WD. What does it mean?E/WD. What does it mean?

A hydraulic device locks the flaps in theirA hydraulic device locks the flaps in theirpresent position.present position.

To reduce structural stress, the slats To reduce structural stress, the slats movement is being slowed down through movement is being slowed down through the wing tip brakes. the wing tip brakes.

To avoid asymmetry, the outer slats are To avoid asymmetry, the outer slats are locked in their present position. locked in their present position.

Because of the locked flaps, the wing tip Because of the locked flaps, the wing tip brake also lock the slats.brake also lock the slats.

Ailerons and rudder.Ailerons and rudder.

Which control surfaces are used for the mechanical backup?Which control surfaces are used for the mechanical Which control surfaces are used for the mechanical backup?backup?

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 the How many actuators are provided to control the ailerons and how many hydraulic sources supply ailerons and how many hydraulic sources supply these actuators?these actuators?

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 4 4 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?

It is an indicator for the It is an indicator for the sidesticksidestickdeflections during the flight control deflections during the flight control check.check.

It is an indicator for the control surfaces It is an indicator for the control surfaces deflections during the flight control deflections during the flight control check.check.

It is an indication for the rudder pedals It is an indication for the rudder pedals deflections during the flight control deflections 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 one In Normal Law, if one sidesticksidestick is rapidly pulled is rapidly pulled fully back, can the airplanefully back, can the airplane’’s maximum allowable s maximum allowable ““GG”” load be exceeded ?load be exceeded ?

Yes. Rapid Yes. Rapid sidesticksidestick deflection must deflection must never be made.never be made.

Yes, until maximum pitch attitude isYes, until maximum pitch attitude isreached.reached.

No. At maximum No. At maximum ““GG”” load, the load, the sidestickssidesticksare deare de--activated for 5 seconds.activated for 5 seconds.

No. The load factor limitation overridesNo. The load factor limitation overridessidesticksidestick commands to avoid excessivecommands to avoid excessive““GG”” loads.loads.

With the sidestick fully forward, what will be the maximum airspeed indication?With the With the sidesticksidestick fully forward, what will be the fully forward, what will be the maximum airspeed indication?maximum airspeed indication?

According to these indications, if you release the sidestick now...According to these indications, if you release the According to these indications, if you release the sidesticksidestick now...now...

The bank angle will automatically return The 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 angle you can reach with the sidestick fully deflected ?In Normal Law, what is the maximum bank angle In Normal Law, what is the maximum bank angle you can reach with the you can reach with the sidesticksidestick fully deflected ?fully deflected ?

3333ºº

There is no bank limitation.There is no bank limitation.

80 80 ºº

67 67 ºº

According to these indications, which flight control law is active ?According to these indications, which flight control According to these indications, which flight control law is active ?law is active ?

Normal Law.Normal Law.

Alternate Law.Alternate Law.

Direct Law.Direct Law.

Mechanical Back Up.Mechanical Back Up.

According to these indications, which flight control law is active ?According to these indications, which flight control According to these indications, which flight control law is active ?law is active ?

Normal LawNormal Law

Alternate LawAlternate Law

Direct LawDirect Law

Mechanical Back UpMechanical Back Up

Which ECAM FUEL page corresponds to this E/WD?Which ECAM FUEL page corresponds to this Which ECAM FUEL page corresponds to this E/WD?E/WD?

Which ECAM FUEL page corresponds to this E/WD?Which ECAM FUEL page corresponds to this Which ECAM FUEL page corresponds to this E/WD?E/WD?

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?

The fuel system is not connected to the The fuel system is not connected to the Flight Warning Computer.Flight Warning Computer.

Inner tank pump failures never trigger a Inner tank pump failures never trigger a warning because the fuel can be used by warning because the fuel can be used by gravity feeding.gravity feeding.

Due to redundancy, loss of one pump is Due 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?

The fuel system is not connected to the The fuel system is not connected to the Flight Warning Computer.Flight Warning Computer.

Due to redundancy, loss of one pump is Due to redundancy, loss of one pump is only level 1 caution.only level 1 caution.

Inner tank pump failures never trigger a Inner tank pump failures never trigger a warning because the fuel can be used by warning because the fuel can be used by gravity feeding.gravity feeding.

Yes, the fuel of this tank is available by Yes, the fuel of this tank is available by gravity feeding.gravity feeding.

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 use fuel out of the right inner tank?In case of R TK PUMP 1 + 2 LO PR, can you still use In 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?

In case of R TK PUMP 1 + 2 LO PR, can you still use fuel out of the right inner tank?In case of R TK PUMP 1 + 2 LO PR, can you still use In 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?

Yes, the fuel of this tank is available by Yes, the fuel of this tank is available by gravity feeding.gravity feeding.

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.

According to this SD FUEL page indications, only the Center Tank Pumps are feeding the engines.According to this SD FUEL page indications, only According to this SD FUEL page indications, only the Center Tank Pumps are feeding the engines.the Center Tank Pumps are feeding the engines.

True.True.

False.False.

According to this SD FUEL page indications, only the Center Tank Pumps are feeding the engines.According to this SD FUEL page indications, only According to this SD FUEL page indications, only the Center Tank Pumps are feeding the engines.the Center Tank Pumps are feeding the engines.

True.True.

False.False.

According to this FUEL SD page indications, which pumps are feeding the engines?According to this FUEL SD page indications, which According to this FUEL SD page indications, which pumps are feeding the engines?pumps are feeding the engines?

The Center Tank Pumps alone.The Center Tank Pumps alone.

The Center Tank Pumps and the inner The 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, which pumps are feeding the engines?According to this FUEL SD page indications, which According to this FUEL SD page indications, which pumps are feeding the engines?pumps are feeding the engines?

The Center Tank Pumps alone.The Center Tank Pumps alone.

The Center Tank Pumps and the inner The 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 to the inner tanks?Why has the fuel been transferred from the outer to Why has the fuel been transferred from the outer to the inner tanks?the inner tanks?

The temperature in the outer tank was too The 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 too The temperature in the inner tank was too low.low.

The quantity in the inner tanks is The quantity in the inner tanks is approaching low level.approaching low level.

Why has the fuel been transferred from the outer to the inner tanks?Why has the fuel been transferred from the outer to Why has the fuel been transferred from the outer to the inner tanks?the inner tanks?

The temperature in the outer tank was too The 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 too The temperature in the inner tank was too low.low.

The quantity in the inner tanks is The quantity in the inner tanks is approaching low level.approaching low level.

On the ECAM E/WD page the message REFUELG appears in the MEMO. What does it mean?On the ECAM E/WD page the message REFUELG On the ECAM E/WD page the message REFUELG appears in the MEMO. What does it mean?appears in the MEMO. What does it mean?

The aircraft systems are ready to start The aircraft systems are ready to start refueling.refueling.

The refueling control panel door is notThe refueling control panel door is notclosed.closed.

Refueling is completed, the required Refueling is completed, the required amount of fuel has been pumped into the amount 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 REFUELG appears in the MEMO. What does it mean?On the ECAM E/WD page the message REFUELG On the ECAM E/WD page the message REFUELG appears in the MEMO. What does it mean?appears in the MEMO. What does it mean?

The aircraft systems are ready to start The aircraft systems are ready to start refueling.refueling.

The refueling control panel door is notThe refueling control panel door is notclosed.closed.

Refueling is completed, the required Refueling is completed, the required amount of fuel has been pumped into the amount 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 amberOn this ECAM FUEL SD page what does an amber--boxed FOB indication mean?boxed FOB indication mean?

Not all the fuel on board is useable Not 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 measured A disagreement between fuel measured and fuel entered on the MCDU has been and 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 amberOn this ECAM FUEL SD page what does an amber--boxed FOB indication mean?boxed FOB indication mean?

Not all the fuel on board is useable Not 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 measured A disagreement between fuel measured and fuel entered on the MCDU has been and fuel entered on the MCDU has been detected.detected.

On the ECAM FUEL SD page what does this indication of a Center Tank Pump mean?On the ECAM FUEL SD page what does this On the ECAM FUEL SD page what does this indication of a Center Tank Pump mean?indication of a Center Tank Pump mean?

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininAUTO and supplying fuelAUTO and supplying fuel

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininMAN and supplying fuel.MAN and supplying fuel.

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininAUTO but not supplying fuel.AUTO but not supplying fuel.

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininMAN and CTR TK pump not supplying MAN and CTR TK pump not supplying fuel.fuel.

On the ECAM FUEL SD page what does this indication of a Center Tank Pump mean?On the ECAM FUEL SD page what does this On the ECAM FUEL SD page what does this indication of a Center Tank Pump mean?indication of a Center Tank Pump mean?

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininMAN and CTR TK pump not supplying MAN and CTR TK pump not supplying fuel.fuel.

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininAUTO and supplying fuelAUTO and supplying fuel

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininMAN and supplying fuel.MAN and supplying fuel.

It is switched on with the Mode SEL It is switched on with the Mode SEL pbpb ininAUTO 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 engine This 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?

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 totomanual.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 valves There are no actions required. The valves will close automatically during the next will close automatically during the next refueling.refueling.

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 engine This 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?

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 totomanual.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 valves There are no actions required. The valves will close automatically during the next will close automatically during the next refueling.refueling.

On the ECAM, the message OUTER TK FUEL XFRD appears in the MEMO. What does it mean?On the ECAM, the message OUTER TK FUEL XFRD On the ECAM, the message OUTER TK FUEL XFRD appears in the MEMO. What does it mean?appears in the MEMO. What does it mean?

Fuel is transferred from the inner tank toFuel is transferred from the inner tank tothe outer tank.the outer tank.

Fuel is transferred from the outer tank to Fuel is transferred from the outer tank to the inner tank.the inner tank.

Fuel is transferred from the inner tank to Fuel is transferred from the inner tank to the center tank.the center tank.

Fuel is transferred from the center tank to Fuel is transferred from the center tank to the inner tank.the inner tank.

On the ECAM, the message OUTER TK FUEL XFRD appears in the MEMO. What does it mean?On the ECAM, the message OUTER TK FUEL XFRD On the ECAM, the message OUTER TK FUEL XFRD appears in the MEMO. What does it mean?appears in the MEMO. What does it mean?

Fuel is transferred from the inner tank toFuel is transferred from the inner tank tothe outer tank.the outer tank.

Fuel is transferred from the outer tank to Fuel is transferred from the outer tank to the inner tank.the inner tank.

Fuel is transferred from the inner tank to Fuel is transferred from the inner tank to the center tank.the center tank.

Fuel is transferred from the center tank to Fuel is transferred from the center tank to the inner tank.the inner tank.

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 switch What is the reason the center tank pumps switch automatically off when the slats are extended for automatically off when the slats are extended for taketake--off?off?

To keep the center of gravity as low as To keep the center of gravity as low as possible.possible.

During takeDuring take--off, the center tank fuel is off, 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 different To 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 switch What is the reason the center tank pumps switch automatically off when the slats are extended for automatically off when the slats are extended for taketake--off?off?

To keep the center of gravity as low as To keep the center of gravity as low as possible.possible.

During takeDuring take--off, the center tank fuel is off, 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 different To 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?

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?

2400 lbs.2400 lbs.

3300 lbs.3300 lbs.

4700 lbs.4700 lbs.

5300 lbs.5300 lbs.

The normal pressure for the hydraulic system is 2000 psiThe normal pressure for the hydraulic system is The normal pressure for the hydraulic system is 2000 2000 psipsi

True.True.

False.False.

2000 2000 psipsi

3000 3000 psipsi

What is the normal pressure in the hydraulic system?What is the normal pressure in the hydraulic What is the normal pressure in the hydraulic system?system?

500 500 psipsi

1000 1000 psipsi

The PTU.The PTU.

Both the GREEN and YELLOW Both the GREEN and YELLOW systemssystems..

According to this indication, the BLUE system is powered by...According to this indication, the BLUE system is According to this indication, the BLUE system is powered by...powered by...

The ELEC pump.The ELEC pump.

The RAT.The RAT.

Users connected to the YELLOW system Users connected to the YELLOW system are no longer supplied with hydraulic are no longer supplied with hydraulic pressure.pressure.

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 RSVR We have completed the procedure for HYD Y RSVR LO AIR PR, what does the YELLOW indication in LO AIR PR, what does the YELLOW indication in amber mean?amber mean?

YELLOW is amber because ENG 2 is not YELLOW is amber because ENG 2 is not running.running.

The ELEC pump has The ELEC pump has beenbeen switched off.switched off.

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 you the yellow system by the PTU after you switch the ENG 2 pump off.switch the ENG 2 pump 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 switch The first step of the procedure asks you to switch the PTU off. Why?the PTU off. Why?

Because it is faulty.Because it is faulty.

You want to You want to unpressurizeunpressurize the BLUE the BLUE system.system.

The BLUE and the YELLOW systems are The BLUE and the YELLOW systems are supplying the GREEN system.supplying the GREEN system.

The YELLOW system is supplying the The YELLOW system is supplying the GREEN system.GREEN system.

Which statement is true?Which statement is true?Which statement is true?

The GREEN system is supplied by the The GREEN system is supplied by the BLUE system.BLUE system.

The YELLOW system is supplying the The 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 check As part of the cockpit preparation, you must check the hydraulic fluid level. What should the indication the hydraulic fluid level. What should the indication look like?look like?

The RAT is pressurizing the BLUE The RAT is pressurizing the BLUE system.system.

What is the meaning of the RAT indication, as displayed on this HYD ECAM page?What is the meaning of the RAT indication, as What is the meaning of the RAT indication, as displayed on this HYD ECAM page?displayed on this HYD ECAM page?

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 delivering power to the GREEN system?What is the correct PTU indication if it is delivering What is the correct PTU indication if it is delivering power to the GREEN system?power to the GREEN system?

On the ECAM BLEED SD page, what is the normal indication in flight with WING ANTI-ICE on?On the ECAM BLEED SD page, what is the normal On the ECAM BLEED SD page, what is the normal indication in flight with WING ANTIindication in flight with WING ANTI--ICE on?ICE on?

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.

You are in flight. According to these indications….You are in flight. According to these indicationsYou are in flight. According to these indications……..

The right wing antiThe right wing anti--ice valve failed to ice valve failed to open.open.

The left wing antiThe left wing anti--ice valve failed to close.ice valve failed to close.

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.

In flight the ECAM SD page displays the following indications. What does it mean?In flight the ECAM SD page displays the following In flight the ECAM SD page displays the following indications. What does it mean?indications. What does it mean?

The right wing antiThe right wing anti--ice valve failed to ice valve failed to open.open.

The left wing antiThe left wing anti--ice valve failed to close.ice valve failed to close.

When in AUTO mode, the windows are When in AUTO mode, the windows are only heated on ground.only heated on ground.

When pushed on, window heating will When pushed on, window heating will perform a 30 seconds test on ground and perform a 30 seconds test on ground and then switch off until takethen switch off until take--off.off.

When pushed prior to engine start, the When pushed prior to engine start, the windows are manually heated.windows are manually heated.

Concerning the PROBE/WINDOW HEAT pb, which one of the following statements is true?Concerning the PROBE/WINDOW HEAT pb, which Concerning the PROBE/WINDOW HEAT pb, which one of the following statements is true?one of the following statements is true?

When pushed on after takeWhen pushed on after take--off, the off, the windows are heated only when necessary.windows are heated only when necessary.

Electrical heating only.Electrical heating only.

Hot air only.Hot air only.

Electrical heating and warm air from the Electrical heating and warm air from the cabin.cabin.

Electrical heating and hot air.Electrical heating and hot air.

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?

If one engine anti-ice system fails, the second one takes over and provides anti-icing for both engines.If one engine antiIf one engine anti--ice system fails, the second one ice system fails, the second one takes over and provides antitakes over and provides anti--icing for both engines.icing for both engines.

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 the When flying in icing conditions, what will be the correct ECAM BLEED system page indication with correct ECAM BLEED system page indication with both WING and ENG antiboth WING and ENG anti--ice systems ON?ice systems ON?

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.

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 displays the ECAM E/WD page displays ““WING A.ICE SYS WING A.ICE SYS FAULTFAULT””. What does it mean?. What does it mean?

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.

Cannot be used simultaneously with the Cannot be used simultaneously with the wing antiwing anti--ice system due to engine ice system due to engine limitations.limitations.

Is controlled manually by the pilot Is controlled manually by the pilot through the ENG1 and ENG2 antithrough the ENG1 and ENG2 anti--ice ice pbpb..

In case of Icing condition, the engine Anti-Ice system...In case of Icing condition, the engine AntiIn case of Icing condition, the engine Anti--Ice Ice system...system...

Operates only in flight and is fully Operates 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 controlthrough the ENG1 and ENG2 antithrough the ENG1 and ENG2 anti--ice ice pbpb..

Because of ice detection, the system asks Because 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 the At least one ENG A.ICE switch is in the ON position.ON position.

According to the ECAM Memo Page these indications mean:According to the ECAM Memo Page these According to the ECAM Memo Page these indications mean:indications mean:

The ENG A.ICE system is inoperative.The ENG A.ICE system is inoperative.

The ENG A.ICE has automatically started The ENG A.ICE has automatically started without any crew action.without any crew action.

Pull the GRAVITY GEAR EXTN Pull the GRAVITY GEAR EXTN handcrankhandcrankand turn it clockwise 3 turns.and turn it clockwise 3 turns.

Pull the GRAVITY GEAR EXTN Pull the GRAVITY GEAR EXTN handcrankhandcrankand turn it counterclockwise 3 turns.and turn it counterclockwise 3 turns.

After a disagreement on landing gear position, you have recycled the L/G but there are still indications as shown.How do you perform the next ECAM action?

After a disagreement on landing gear position, you After a disagreement on landing gear position, you have recycled the L/G but there are still indications have 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?

According to the procedure L/G GRAVITYAccording to the procedure L/G GRAVITYEXTENSION which is found in the Quick EXTENSION 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 timethe gear will free fall automatically.the gear will free fall automatically.

After GRAVITY EXTENSION the gearAfter GRAVITY EXTENSION the gearindications on the ECAM WHEEL pageindications on the ECAM WHEEL pageare not reliable.are not reliable.

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, you After a disagreement on landing gear position, you have performed the L/G GRAVITY EXTENSION have performed the L/G GRAVITY EXTENSION procedure.procedure.According to these indications, which statement is According to these indications, which statement is true ?true ?

The gear is in the The gear is in the downlockdownlock position.position.

The gear is down but not locked.The gear is down but not locked.

The ANTI/SKID system for wheels 1 andThe ANTI/SKID system for wheels 1 and3 is inoperative.3 is inoperative.

The AUTO/BRK is applying pressure toThe AUTO/BRK is applying pressure tobrake 2 and 4 only.brake 2 and 4 only.

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 following MED. After touch down you observe the following indications.indications.At this moment, which statement is true ?At this moment, which statement is true ?

The ANTI/SKID system is increasing brakeThe ANTI/SKID system is increasing brakepressure for wheels 2 and 4.pressure for wheels 2 and 4.

The ANTI/SKID system is releasing brakeThe ANTI/SKID system is releasing brakepressure 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 brake Which indication CONFIRMS that the parking brake is actually set ?is actually set ?

PARK BRKPARK BRK

One of the pilots has pushed the PEDALSOne of the pilots has pushed the PEDALSDISC pushbutton located on the steeringDISC pushbutton located on the steeringhandwheelhandwheel..

The nose wheel steering computer hasThe nose wheel steering computer hasfinished itfinished it’’s self test.s self test.Nose wheel steering is now available.Nose wheel steering is now available.

On this E/WD, what does the “NW STRG DISC”memo mean?On this E/WD, what does the On this E/WD, what does the ““NW STRG DISCNW STRG DISC””memo mean?memo mean?

The nose wheel steering has been The 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 steeringsystem has been detected.system has been detected.

PARK BRKNW STRG DISC

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 assoon as you start taxi.soon as you start taxi.

The nose wheel steering is stillThe nose wheel steering is stilldisconnected. The memo has becomedisconnected. The memo has becomeamber because one engine is running.amber because one engine is running.

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 to 2 is started, leading to the the ““NW STRG DISCNW STRG DISC”” memo.memo.What is the correct statement?What is the correct statement?

The NW STRG disconnect mechanism hasThe NW STRG disconnect mechanism hasfailed.failed.

The yellow hydraulic system has build upThe yellow hydraulic system has build uppressure which might damage the NWpressure which might damage the NWSTRG system when set to towing STRG system when set to towing position.position.

NW STRG DISCAPU BLEED

You must perform the check again andYou must perform the check again andpress harder on the brakes until you getpress harder on the brakes until you getan 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 applyenough pressure to be displayed on theenough pressure to be displayed on theBRAKES indicator.BRAKES indicator.

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 feel While pressing on top of the rudder pedals you feel the airplane decelerating but the BRAKES pressure the airplane decelerating but the BRAKES pressure indication remains 0.indication remains 0.Which statement is true ?Which statement is true ?

The BRAKES pressure indicator hasThe BRAKES pressure indicator hasfailed.failed.

The indication is normal because the The indication is normal because the ““BRAKESBRAKES”” press indicator is active on press indicator is active on brake system alternate mode (yellow brake system alternate mode (yellow supply).supply).

According to these indications, the AUTO/BRAKE is active.According to these indications, the AUTO/BRAKE is According to these indications, the AUTO/BRAKE is active.active.

True.True.

False.False.

Each triangle represents one brakingEach triangle represents one brakingsystem (normal/alternate) available forsystem (normal/alternate) available forthe associated gear.the associated gear.

The front triangle indicates that The front triangle indicates that AUTO/BRK is available and the one in the AUTO/BRK is available and the one in the back means that ANTI/SKID is available back means that ANTI/SKID is available for that gear.for that gear.

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, appearing What is the meaning of the 2 triangles, appearing below each landing gear, on the WHEEL ECAM below each landing gear, on the WHEEL ECAM page?page?

Each triangle represents one tire.Each triangle represents one tire.

There are two computers providingThere are two computers providinginformation on the gear position. Eachinformation on the gear position. Eachtriangle represents the position detectedtriangle represents the position detectedby its associated computer.by its associated computer.

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 the The L/G is up and not locked in the selected position. The L/G doors are openselected position. The L/G doors are open

You have just set the L/G selector to the DOWN position. 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...

The computers providing gear positionThe computers providing gear positioninformation have failed.information have failed.

One L/G control system is inoperative.One L/G control system is inoperative.The nose landing gear is not The 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.

How do you interpret the following indications?How do you interpret the following indications?How do you interpret the following indications?

The nose gear is in transit.The nose gear is in transit.

All gears are down and locked.All gears are down and locked.

The ANTI/SKID system is automaticallyThe ANTI/SKID system is automaticallyreleasing the pressure of that brake.releasing the pressure of that brake.

The L/G control system has detected a The L/G control system has detected a low tire profile.low tire profile.

What is the meaning of the green arc appearing over wheel #2?What is the meaning of the green arc appearing What is the meaning of the green arc appearing over wheel #2?over wheel #2?

It marks the hottest brake with aIt marks the hottest brake with atemperature of more than 100 temperature of more than 100 ºº Celsius.Celsius.

It indicates an abnormal high temperature.It indicates an abnormal high temperature.

I must put the L/G selector to the UPI must put the L/G selector to the UPposition and immediately to the DOWNposition and immediately to the DOWNposition again.position again.

I must put the L/G selector to the UPI must put the L/G selector to the UPposition, 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.

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 of What are your actions according to the first line of the ECAM procedure ?the ECAM procedure ?

I must put the L/G selector to the UPI must put the L/G selector to the UPposition.position.

The system is trying to recycle the gearThe system is trying to recycle the gearautomatically. I must wait until the firstautomatically. I must wait until the firstline disappears.line disappears.

T/O light.T/O light.

Taxi light.Taxi light.

During your walk-around, you see that one light needs a new bulb. What is the purpose of this light?During your walkDuring your walk--around, you see that one light around, 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?

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?

Where are the controls for the seat belts and no smoking signs located?Where are the controls for the seat belts and no Where are the controls for the seat belts and no smoking signs located?smoking signs located?

When the landing lights are switched off.When the landing lights are switched off.

When the last engine has been shut When the last engine has been shut down.down.

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 light On the EXT LT control panel, the STROBE light selector is set to AUTO. In this position, when do selector is set to AUTO. In this position, when do they stop flashing?they stop flashing?

When the aircraft touches down.When the aircraft touches down.

When the first reverser is opened.When the first reverser is opened.

BEACON,LAND, STROBE, T.O. and NAV BEACON,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.

According to these panels, which lights are actually illuminated?According to these panels, which lights are actually According to these panels, which lights are actually illuminated?illuminated?

Which of these buttons control IR and ADR?Which of these buttons control IR and ADR?Which of these buttons control IR and ADR?

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 one It is an indication that at least one navaidnavaidhas been manually tuned.has been manually tuned.

It is an indication that the WX RADAR Tilt It 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 RADARGain has been manually adjusted.Gain has been manually adjusted.

MAN

Mountains.Mountains.

Turbulences.Turbulences.

Water.Water.

What is the meaning of the magenta color of some radar returns?What is the meaning of the magenta color of some What is the meaning of the magenta color of some radar returns?radar returns?

What is the meaning of the black color on the radar image?What is the meaning of the black color on the radar What is the meaning of the black color on the radar image?image?

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 IRS On 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 discrepancy System discovered a discrepancy between the position in the database and between 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 NAV At least one of the IR lost the NAV capability. capability.

The system is performing a test before the The system is performing a test before the final alignment.final alignment.

The alignment process stopped at 1 The alignment process stopped at 1 minute of the end and is waiting for the minute of the end and is waiting for the coordinates to be inserted.coordinates to be inserted.

Between the ND and MCDU you are performing a NAV ACCUR check. Does it satisfy you?Between the ND and MCDU you are performing a Between 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 within same or the difference is within acceptable limits.acceptable limits.

No, there is a major discrepancy between No, there is a major discrepancy between raw data and FMGS positions.raw data and FMGS positions.

No, the accuracy is displayed LOW on the No, the accuracy is displayed LOW on the MCDU PROG page.MCDU PROG page.

One of the IR has an attitude problem. Please perform the correct action.One of the IR has an attitude problem. Please One of the IR has an attitude problem. Please perform the correct action.perform the correct action.

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 position On the GNADIRS control panel, what is the position for the DATA selector to see the remaining time for for the DATA selector to see the remaining time for alignment?alignment?

PPOS.PPOS.

HDG.HDG.

STS.STS.

TEST.TEST.

ALIGN ALIGN ALIGN

What does the indication TTN 10 on the GNADIRS panel mean?What does the indication TTN 10 on the GNADIRS What does the indication TTN 10 on the GNADIRS panel mean?panel mean?

It is an indication that IR3 has calculated a It is an indication that IR3 has calculated a heading of 10 degrees to True North. heading of 10 degrees to True North.

It is an indication that it will take 10 It is an indication that it will take 10 minutes to complete the alignment.minutes to complete the alignment.

It is an indication that the heading It is an indication that the heading calculated by IR3 differs by 10 degrees calculated by IR3 differs by 10 degrees from the average.from the average.

It is an indication that the time to the next It 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 the displays with information about ILS 2.An ILS approach is selected. Please indicate the An ILS approach is selected. Please indicate the displays with information about ILS 2.displays with information about ILS 2.

PFD 1 and ND 1.PFD 1 and ND 1.

PFD 2 and ND 2.PFD 2 and ND 2.

PFD 1 and ND 2.PFD 1 and ND 2.

PFD 2 and ND 1.PFD 2 and ND 1.

Is it possible to get information about ILS 2 on the CAPT side?Is it possible to get information about ILS 2 on the Is it possible to get information about ILS 2 on the CAPT side?CAPT side?

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.

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.

Please indicate the location of the ATC and TCAS panel.Please indicate the location of the ATC and TCAS Please indicate the location of the ATC and TCAS panel.panel.

Which situation corresponds to the WX RADAR settings?Which situation corresponds to the WX RADAR Which situation corresponds to the WX RADAR settings?settings?

What is the appropriate ECAM page to get information about the oxygen system?What is the appropriate ECAM page to get What is the appropriate ECAM page to get information about the oxygen system?information about the oxygen system?

In case of an ECAM procedure calling for a Manual deployment of the masks, indicate which control pbhas to be pressed.

In case of an ECAM procedure calling for a Manual In case of an ECAM procedure calling for a Manual deployment of the masks, indicate which control deployment of the masks, indicate which control pbpbhas to be pressed.has to be pressed.

On the passenger OXYGEN control panel, which indication confirms the deployment of the masks?On the passenger OXYGEN control panel, which On the passenger OXYGEN control panel, which indication confirms the deployment of the masks?indication confirms the deployment of the masks?

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 duringthe preflight check to check the oxygen the preflight check to check the oxygen supply to the mask.supply to the mask.

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, which On 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 maximum The 100% position provides the maximum pressure, N provides the normal pressure, pressure, N provides the normal pressure, which is lower.which is lower.

The N position provides an air/oxygen The 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, which which pbpb has to be pressed to switch the system has to be pressed to switch the system OFF? OFF?

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?

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 the On the ECAM control panel, please select the appropriate ECAM page to get information about appropriate ECAM page to get information about the PNEUMATIC system.the PNEUMATIC system.

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 has Both engines are running and APU BLEED has been switched OFF. Is the ECAM BLEED page been switched OFF. Is the ECAM BLEED page display correct ?display correct ?

No, APU bleed closed, but X bleed valve No, APU bleed closed, but X bleed valve has to stay open. has to stay open.

No, the crew should select X bleed valve No, the crew should select X bleed valve selector to (shut) position to close the selector 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, HP valves open because of high air demand valves 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 is An ENG 1 BLEED fault has occurred and is indicated by the related ECAM E/WD failure indicated by the related ECAM E/WD failure message. message.

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.

The ENG 1 BLEED valve has been The ENG 1 BLEED valve has been automatically closed.automatically closed.

On ground, on the ECAM SD “BLEED” page the GND symbol is always displayed.On ground, on the ECAM SD On ground, on the ECAM SD ““BLEEDBLEED”” page the page the GND symbol is always displayed.GND symbol is always displayed.

True.True.

False.False.

According to the ECAM BLEED page message and “AIR COND” control panel indications.According to the ECAM BLEED page message and According to the ECAM BLEED page message and ““AIR CONDAIR COND”” control panel indications.control panel indications.

The engines are running and supplying The engines are running and supplying bleed air.bleed air.

The engines are not running, the APU is The engines are not running, the APU is supplying bleed air.supplying bleed air.

The engines are running, the APU is The engines are running, the APU is supplying bleed air.supplying bleed air.

The engines are not running, a GND HP The 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 those After starting both engines and according to those AIR COND panel and ECAM BLEED page AIR 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.

The APU.The APU.

The engines and the APU together.The engines and the APU together.

What is the engine power according to this ECAM indication?What is the engine power according to this ECAM What is the engine power according to this ECAM indication?indication?

At or close to takeAt or close to take--off power.off power.

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 page indications, which source(s) will supply bleed air when the APU BLEED pb is pressed.

According to the present AIR COND control panel According to the present AIR COND control panel switch positions and ECAM BLEED page switch positions and ECAM BLEED page indications, which source(s) will supply bleed air indications, which source(s) will supply bleed air when the APU BLEED when the APU BLEED pbpb is pressed. is pressed.

The APU supplies both sides of the The APU supplies both sides of the system.system.

The APU supplies the left side of the The APU supplies the left side of the system only.system only.

The APU supplies left side and engine 2 The 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 BLEED The APU BLEED pbpb has just been switched ON.has just been switched ON.On the ECAM BLEED page what do the related On 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.

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 status page how do we interpret the STATUS information message in green?

Following an ENG 1 BLEED fault, the ECAM E/WD Following an ENG 1 BLEED fault, the ECAM E/WD procedure has been applied; on the ECAM status procedure has been applied; on the ECAM status page how do we interpret the STATUS information page how do we interpret the STATUS information message in green? message in green?

One pack has been automatically One pack has been automatically switched off because one ENG BLEED switched off because one ENG BLEED system cannot supply WAI and 2 packs.system cannot supply WAI and 2 packs.

One pack has to be switched OFF if WING One pack has to be switched OFF if WING ANTI ICE (WAI) is used because one ENG ANTI ICE (WAI) is used because one ENG BLEED system cannot supply WAI and 2 BLEED system cannot supply WAI and 2 packs together. packs together.

If WAI, has to be used, the X BLEED valve If WAI, has to be used, the X BLEED valve is automatically closed. Therefore, pack 1 is automatically closed. Therefore, pack 1 will no longer be supplied.will no longer be supplied.

A green disc, which means the bottle A green disc, which means the bottle pressure is normal.pressure is normal.

A red disc, which means the APU FIRE A red disc, which means the APU FIRE EXTING BOTTLE has not been discharged EXTING BOTTLE has not been discharged overboard.overboard.

What is the normal APU Fire extinguisher overpressure indication, and how do you interpret it?

What is the normal APU Fire extinguisher What is the normal APU Fire extinguisher overpressure indication, and how do you interpret overpressure indication, and how do you interpret it?it?

A red disc, which means the APU FIRE A red disc, which means the APU FIRE EXTING BOTTLE has been discharged EXTING BOTTLE has been discharged due to an APU fire.due to an APU fire.

A pressure gage visible from outside A pressure gage visible from outside which indicates the bottle pressure.which indicates the bottle pressure.

The ENG1 and ENG2 BLEED The ENG1 and ENG2 BLEED pbspbs..

This is an automatic sequence initiated This is an automatic sequence initiated when second or Eng starting is selected.when second or Eng starting is selected.

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 BLEED The APU BLEED pbpb on AIR COND on AIR COND overhead panel.overhead panel.

The bleed rotary selector on AIR COND The bleed rotary selector on AIR COND overhead panel.overhead panel.

Bleed air for engine start on ground and Bleed air for engine start on ground and air conditioning in flight only.air conditioning in flight only.

Electric Power only for electric system on Electric 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 power On ground and in flight: electric power and bleed air for air conditioning.and bleed air for air conditioning.

On ground and in flight, electric power for On ground and in flight, electric power for the aircraft electric system and bleed air the aircraft electric system and bleed air for engine start.for engine start.

The APU provides: The APU provides: The APU provides:

The Electric Power supplied from the APU generator isThe Electric Power supplied from the APU The Electric Power supplied from the APU generator isgenerator is

Available as soon as APU is running, even Available as soon as APU is running, even if APU GEN is not selected ON.if APU GEN is not selected ON.

Only available if the ground External Only available if the ground External Power is already connected to the a/c Power is already connected to the a/c Electric network .Electric network .

Available as soon as engines are shut Available as soon as engines are shut down.down.

Available when APU is running, APU GEN Available 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 is still running because it always The APU is still running because it always needs a cool down period after the APU needs 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 cool The APU is still running. It is in the cool down period because you have used APU down period because you have used APU bleed before.bleed before.

The APU is still running. You have to The APU is still running. You have to push the START SW to initiate the shut push the START SW to initiate the shut down sequence.down sequence.

The APU has shut down but the AIR The APU has shut down but the AIR INLET FLAP is not fully closed yet.INLET FLAP is not fully closed yet.

Yes, I simply push the APU STARTYes, I simply push the APU STARTswitch 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 theAPU again.APU again.

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, you After 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 interrupt According 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 INLETFLAP is fully closed and then start theFLAP is fully closed and then start theAPU 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 these indications on the overhead panel ?Which ECAM APU page corresponds to these Which ECAM APU page corresponds to these indications on the overhead panel ?indications on the overhead panel ?

Any start attempt with a detected LOW Any start attempt with a detected LOW OIL LEVEL will lead to an AUTOOIL LEVEL will lead to an AUTOSHUTDOWN to prevent the APU to be SHUTDOWN to prevent the APU to be damaged.damaged.

Yes. The APU will run for another 60 Yes. The APU will run for another 60 hours after the LOW OIL LEVEL has been hours after the LOW OIL LEVEL has been detected.detected.

You are attempting to start the APU.After 20 seconds you get the following indications that 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 indications After 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 andany start attempt will damage the APU.any start attempt will damage the APU.

Yes, you simple have to wait 20 sec until Yes, you simple have to wait 20 sec until the LOW OIL LEVEL advisory disappears the 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 cool The APU will keep on running to cool down and then shutdown.down and then shutdown.

APU will shutdown only if external power APU will shutdown only if external power is connected.is connected.

Nothing happen because air conditioning Nothing happen because air conditioning is selected on.is selected on.

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 APU After engine shut down, APU running but APU bleed has not been used, when you select APU bleed has not been used, when you select APU MASTER SW pb off.MASTER SW pb off.

The APU will shutdown right away.The APU will shutdown right away.

15 000 ft15 000 ft

In flight APU starting limitation isIn flight APU starting limitation isIn flight APU starting limitation is

39 000 ft39 000 ft

20 000 ft20 000 ft

25 000 ft25 000 ft

39 000 ft39 000 ft

What is the maximum altitude the APU may be used for bleed air supply with 1 pack operating ?What is the maximum altitude the APU may be used What 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

20 000 ft20 000 ft

ALTITUDE (Ft)ALTITUDE (Ft)

20 00020 000

39 00039 000

15 00015 000

25 00025 000

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 is The APU is running and available. It is providing bleed air and electrical power.providing bleed air and electrical power.

The APU is running and available. It is The APU is running and available. It is providing bleed air only.providing bleed air only.

The APU is running and available. It is The APU is running and available. It is providing electrical power only.providing electrical power only.

The APU is running and available . It is The APU is running and available . It is providing neither electrical power nor providing neither electrical power nor bleed air.bleed air.

On the ground, during APU start, the master caution and single chime come ON and you notice on the ECAM, that the APU won’t exceed 53% N1.Which statement is true?

On the ground, during APU start, the master On the ground, during APU start, the master caution and single chime come ON and you notice caution 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 occur An APU AUTO SHUT DOWN will occur because of APU failure to reach 90% N1.because of APU failure to reach 90% N1.

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 occur An APU EMER SHUT DOWN will occur because APU EGT overheating may cause because APU EGT overheating may cause an APU fire.an APU fire.

The FLAP will remain open after APU The FLAP will remain open after APU shutdown to vent the APU compartment.shutdown to vent the APU compartment.

An APU AUTO shut down will occur butAn APU AUTO shut down will occur butyou have to discharge the APU fire bottleyou have to discharge the APU fire bottlefrom the cockpit manually.from the cockpit manually.

An EMER AUTO shut down will occur butAn EMER AUTO shut down will occur butyou have to discharge the APU fire bottleyou have to discharge the APU fire bottlemanually either from the cockpit or bymanually either from the cockpit or bypushing the APU SHUT DOWN switch onpushing the APU SHUT DOWN switch onthe external power panel.the external power panel.

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 andthe APU fire bottle will be dischargedthe APU fire bottle will be dischargedautomatically. automatically.

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 firefrom the cockpit.from the cockpit.

Please indicate the stowing place for the escape ropes.Please indicate the stowing place Please indicate the stowing place for the escape ropes.for the escape ropes.

The door is unlocked.The door is unlocked.

The door is inoperative.The door is inoperative.

On the ECAM DOOR/OXY page, what does an amber door indication mean?On the ECAM DOOR/OXY page, what does an On 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.

The door is fully closed.The door is fully closed.

According to this indication, the Cargo door is inoperative.According to this indication, the Cargo door is According to this indication, the Cargo door is inoperative.inoperative.

True.True.

False.False.

Nothing. Opening from outside disarms Nothing. Opening from outside disarms the slide.the slide.

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. What open 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.

Nothing. The door can't be open from Nothing. The door can't be open from outside as long as the outside as long as the slideslide is armed.is armed.

The left forward cabin door and theThe left forward cabin door and theforward cargo door are unlocked, theforward cargo door are unlocked, theoverwingoverwing exits and the right exits and the right rearrear doordoorslides are not armed.slides are not armed.

OverwingOverwing exits and right rear door slidesexits and right rear door slidesare not armed, left forward cabin door andare not armed, left forward cabin door andforward cargo door indicating a forward cargo door indicating a malfunction.malfunction.

On the ECAM SD DOOR/OXY page this indication means.On the ECAM SD DOOR/OXY page this indication On 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 andforward cargo door indicate a forward cargo door indicate a malfunction.malfunction.

The left forward cabin door and the The left forward cabin door and the forward cargo door are unlocked, theforward cargo door are unlocked, theoverwingoverwing exits and the right rear doorexits and the right rear doorslides are armed.slides are armed.

You are at the gate, according to this DOOR/OXY ECAM 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 EMERGENCY ECAM page, the EMERGENCY EXITsEXITs are disarmed.are disarmed.

True.True.

False.False.

CLIMB and TO/GA.CLIMB and TO/GA.

FLEX/MCT and TO/GA.FLEX/MCT and TO/GA.

Regarding engine THRUST LEVERS position, which detent(s) can be used for take-off?Regarding engine THRUST LEVERS position, which Regarding engine THRUST LEVERS position, which detent(sdetent(s) can be used for take) can be used for take--off?off?

FULL.FULL.

CLIMB and FLEX/MCT.CLIMB and FLEX/MCT.

It indicates a failure in the engine fire It indicates a failure in the engine fire extinguishing system.extinguishing system.

What is the meaning of an amber FAULT light on the ENG panel?What is the meaning of an amber FAULT light on What is the meaning of an amber FAULT light on the ENG panel?the ENG panel?

It indicates a failure in the automatic start It indicates a failure in the automatic start sequence.sequence.

It indicates an engine failure.It indicates an engine failure.

It is an indication of a discrepancy It is an indication of a discrepancy between the digital EGT indication and between the digital EGT indication and the value indicated by the needle.the value indicated by the needle.

It is an indication of a discrepancy It is an indication of a discrepancy between the value shown on the ECAM between the value shown on the ECAM and the real value. and the real value.

On the ECAM E/WD page, what is the meaning of the amber CHK indication?On the ECAM E/WD page, what is the meaning of On 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 is It is an indication that the EGT of ENG 1 is out of the normal range.out of the normal range.

It is an indication of a discrepancy It is an indication of a discrepancy between EGT of ENG1 and ENG2.between EGT of ENG1 and ENG2.

CHK

ENG 1 EGT DISCREPANCY

It is an indication of a discrepancy It is an indication of a discrepancy between the digital EGT indication and between the digital EGT indication and the value indicated by the needle.the value indicated by the needle.

It is an indication of a discrepancy It is an indication of a discrepancy between the value shown on the ECAM between the value shown on the ECAM and the real value. and the real value.

On the ECAM E/WD page, what is the meaning of the amber CHK indication?On the ECAM E/WD page, what is the meaning of On 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 is It is an indication that the EGT of ENG 1 is out of the normal range.out of the normal range.

It is an indication of a discrepancy It is an indication of a discrepancy 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.

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.

Manual.Manual.

FADEC does not monitor the manual FADEC does not monitor the manual start at all. All steps and possible start at all. All steps and possible corrective actions have to be performed corrective actions have to be performed by the pilots.by the pilots.

During a manual start, what is the role of the FADEC?During a manual start, what is the role of the During a manual start, what is the role of the FADEC?FADEC?

It has a passive monitoring role, the crew It has a passive monitoring role, the crew has to monitor the start carefully to take has to monitor the start carefully to take corrective actions in case of corrective actions in case of malfunctions.malfunctions.

There is no difference between There is no difference between automatic and normal start, FADEC automatic and normal start, FADEC monitors and reacts to possible failures monitors and reacts to possible failures during the start sequence.during the start sequence.

FADEC does not monitor the manual FADEC does not monitor the manual start at all. All steps and possible start at all. All steps and possible corrective actions have to be performed corrective actions have to be performed by the pilots.by the pilots.

During a manual start, what is the role of the FADEC?During a manual start, what is the role of the During a manual start, what is the role of the FADEC?FADEC?

It has a passive monitoring role, the crew It has a passive monitoring role, the crew has to monitor the start carefully to take has to monitor the start carefully to take corrective actions in case of corrective actions in case of malfunctions.malfunctions.

There is no difference between There is no difference between automatic and normal start, FADEC automatic and normal start, FADEC monitors and reacts to possible failures monitors and reacts to possible failures during the start sequence.during the start sequence.

Fuel flow start.Fuel flow start.

Starter engagement.Starter engagement.

Which step of a manual start is taken over by the FADEC?Which step of a manual start is taken over by the Which step of a manual start is taken over by the FADEC?FADEC?

Ignition start.Ignition start.

Ignition cutIgnition cut--out.out.

Fuel flow start.Fuel flow start.

Starter engagement.Starter engagement.

Which step of a manual start is taken over by the FADEC?Which step of a manual start is taken over by the Which step of a manual start is taken over by the FADEC?FADEC?

Ignition start.Ignition start.

Ignition cutIgnition cut--out.out.

Fuel flow start.Fuel flow start.

Ignition start.Ignition start.

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 pages From ECAM E/WD and SD engine pages determinate which step of a manual start is taken determinate which step of a manual start is taken over by the FADEC?over by the FADEC?

Starter valve closure.Starter valve closure.

Starter valve engagement.Starter valve engagement.

Fuel flow start.Fuel flow start.

Ignition start.Ignition start.

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 determinate From ECAM E/WD and SD engine page determinate which step of a manual start is taken over by the which step of a manual start is taken over by the FADEC.FADEC.

Starter valve closure.Starter valve closure.

Starter valve engagement.Starter valve engagement.

FLEX/MCT.FLEX/MCT.

TO/GA.TO/GA.

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 takeYou are about to perform a take--off. You donoff. You don’’t have t 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.

CLIMB.CLIMB.

Yes, igniter B is always used for the Yes, igniter B is always used for the engine start.engine start.

Yes, igniters are used alternatively for Yes, igniters are used alternatively for engine start, in this case B.engine start, in this case B.

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, you During 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 the No, normally igniter A is used for the engine start.engine start.

No, normally both igniters are used for No, normally both igniters are used for engine start.engine start.

Yes, igniter B is always used for the Yes, igniter B is always used for the engine start.engine start.

Yes, igniters are used alternatively for Yes, igniters are used alternatively for engine start, in this case B.engine start, in this case B.

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, you During 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 the No, normally igniter A is used for the engine start.engine start.

No, normally both igniters are used for No, normally both igniters are used for engine start.engine start.

You are performing a take-off with the thrust levers in the FLEX position. Is A/THR now active?You are performing a takeYou are performing a take--off with the thrust levers off with the thrust levers in the FLEX position. Is A/THR now active?in the FLEX position. Is A/THR now active?

Yes.Yes.

No.No.

You are performing a take-off with the thrust levers in the FLEX position. Is A/THR now active?You are performing a takeYou are performing a take--off with the thrust levers off with the thrust levers in the FLEX position. Is A/THR now active?in the FLEX position. Is A/THR now active?

Yes.Yes.

No.No.

As soon as you engage the autopilot.As soon as you engage the autopilot.

As soon as you push the A/THR As soon as you push the A/THR pbpbmanually on.manually on.

You are performing a take off with thrust levers in FLEX 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 pulled As soon as the thrust levers are pulled back into the CLIMB position.back into the CLIMB position.

As soon as you pass the thrust reduction As soon as you pass the thrust reduction altitude.altitude.

As soon as you engage the autopilot.As soon as you engage the autopilot.

As soon as you push the A/THR As soon as you push the A/THR pbpbmanually on.manually on.

You are performing a take off with thrust levers in FLEX 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 pulled As soon as the thrust levers are pulled back into the CLIMB position.back into the CLIMB position.

As soon as you pass the thrust reduction As soon as you pass the thrust reduction altitude.altitude.

As soon as you engage the autopilot.As soon as you engage the autopilot.

As soon as the thrust levers are pulled As soon as the thrust levers are pulled back into the CLIMB position.back into the CLIMB position.

You are performing a take-off with TOGA power. When does the A/THR become active?You are performing a takeYou 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?

As soon as the thrust levers are pulled As soon as the thrust levers are pulled back into the FLEX position.back into the FLEX position.

As soon as you push the A/THR As soon as you push the A/THR pbpbmanually on.manually on.

As soon as you engage the autopilot.As soon as you engage the autopilot.

As soon as the thrust levers are pulled As soon as the thrust levers are pulled back into the CLIMB position.back into the CLIMB position.

You are performing a take-off with TOGA power. When does the A/THR become active?You are performing a takeYou 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?

As soon as the thrust levers are pulled As soon as the thrust levers are pulled back into the FLEX position.back into the FLEX position.

As soon as you push the A/THR As soon as you push the A/THR pbpbmanually on.manually on.

The reversers are stuck.The reversers are stuck.

The reversers are unlocked.The reversers are unlocked.

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.

The reversers are fully deployed.The reversers are fully deployed.

The reversers are stuck.The reversers are stuck.

The reversers are unlocked.The reversers are unlocked.

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.

The reversers are fully deployed.The reversers are fully deployed.

The reversers are stuck.The reversers are stuck.

The reversers are unlocked.The reversers are unlocked.

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 to On the ECAM E/WD, with thrust levers reverser to reverse position. What does a green REV indication reverse position. What does a green REV indication mean?mean?

The reversers are faulty.The reversers are faulty.

The reversers are fully deployed.The reversers are fully deployed.

The reversers are stuck.The reversers are stuck.

The reversers are unlocked.The reversers are unlocked.

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 to On the ECAM E/WD, with thrust levers reverser to reverse position. What does a green REV indication reverse position. What does a green REV indication mean?mean?

The reversers are faulty.The reversers are faulty.

The reversers are fully deployed.The reversers are fully deployed.

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 be Before engine starting the Eng FADEC should be energized: which control do you activate in order to energized: which control do you activate in order to energize the FADEC prior to engine start?energize the FADEC prior to engine start?

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 be Before engine starting the Eng FADEC should be energized: which control do you activate in order to energized: which control do you activate in order to energize the FADEC prior to engine start?energize the FADEC prior to engine start?

No, normally igniter B is used for the No, normally igniter B is used for the engine start.engine start.

Yes, both igniters are used for every start.Yes, both igniters are used for every start.

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, you During the manual start sequence of ENG 2, you notice that both igniters are powered. notice that both igniters are powered. Is this normal?Is this normal?

No, normally igniter A is used for the No, normally igniter A is used for the engine start.engine start.

Yes, for manual start both igniters are Yes, for manual start both igniters are always used.always used.

No, normally igniter B is used for the No, normally igniter B is used for the engine start.engine start.

Yes, both igniters are used for every start.Yes, both igniters are used for every start.

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, you During the manual start sequence of ENG 2, you notice that both igniters are powered. notice that both igniters are powered. Is this normal?Is this normal?

No, normally igniter A is used for the No, normally igniter A is used for the engine start.engine start.

Yes, for manual start both igniters are Yes, for manual start both igniters are always used.always used.