Airbus A320 CBT Answers V2.0 [PDF]

Zitiervorschau

With With aa full full load load of of passengers passengers and and in in aa high high temperature area, , how should the pack temperature area area, how should the pack flow flow be be set? ? set set?

A

To LOW, LOW, in order to minimize the amount of hot air sent to the cabin zones. zones.

B

To NORM, NORM, as the system is fully automatic apart from temperature settings. settings.

C

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

D

To HIGH and cockpit TEMP SELECTOR to HOT in order to have maximum cooling air to the cabin. cabin.

AIR COND – 2A00

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

A

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

B

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

C

To regulate the hot air pressure. pressure.

D

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

AIR COND - 2A01

With panel With reference reference to to the the AIR AIR COND COND panel, panel,, which which statement is correct? ? statement is correct correct?

OFF

A

Pack flow selector is used to select a comfortable temperature. temperature.

B

On the ECAM BLEED page, page, the left system pack compressor outlet temperature should be in amber. amber.

C

All the indications on ECAM BLEED page and AIR COND panel are correct according to the configuration. configuration.

D

[][][][][][]

[][]

It is necessary to select the ENG 1 Bleed pb sw to OFF. OFF.

AIR COND - 2A02

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

A

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

B

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

C

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

D

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

Forward Cargo Ventilation Controller

Aft Cargo Ventilation Controller

AIR COND - 2A03

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

A

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

B

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

C

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

D

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

AIR COND - 2A04

Both Both engines engines are are running running and and the the APU APU bleed bleed has has been switched OFF. . been switched OFF OFF. Which ? correct Which statement statement is is correct? correct?

A

Nothing happens until APU shut down is complete. complete.

B

All the indications are correct. correct.

C

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

D

The ENGINE H. H.P valve should be closed with the engine at idle power. power.

AIR COND - 2A05

IfIf the close the PACK PACK FLOW FLOW CONTROL CONTROL valves valves close, close,, what what will will be the subsequent position of the TRIM AIR be the subsequent position of the TRIM AIR valves valves and ? valve and the the HOT HOT AIR AIR valve? valve? Hot HotAir Air Valve Valve

A

- The TRIM AIR valves remain open. open. - The HOT AIR valve closes. closes.

HOT AIR Mixing Unit

B

- The TRIM AIR valves remain open. open. - The HOT AIR valve remains open. open.

C

- The TRIM AIR valves close. close. - The HOT AIR valve remains open

D

- The TRIM AIR valves close. close. - The HOT AIR valve closes. closes.

Pack 1

Pack 2

Hot Bleed Air

AIR COND - 2A07

Have COND” COND” page. page Have aa look look at at the the ECAM ECAM ““COND” page.. Why Why are are two different temperature values displayed for two different temperature values displayed for each each zone ? aircraft zone of of the the aircraft? aircraft?

A

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

B

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

C

The lower value is the temperature of the air entering a zone (DUCT INLET temperature). temperature). The upper value is the actual zone temperature monitored by the zone control computer. computer.

D

The lower value is the BLEED AIR temperature. temperature. The upper value is the pack temperature of the MIXED AIR in the zone. zone.

AIR COND - 2A08

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

A

HOT AIR

Extracting air from the AVIONICS BAY. BAY. Mixing Unit

B

Reducing the BLEED AIR requirement and therefore saving fuel. fuel.

C

Accelerating pressurization. pressurization.

D

Accelerating the removal of cabin smoke. smoke.

the

cabin

Cabin Cabin Fan Fan

Pack 1

Pack 2

Cabin Cabin Fan Fan

zones

AIR COND - 2A09

With aircraft With only only aa few few passengers passengers on on the the aircraft, aircraft,, the the pack flow control selector should be set : LO pack flow control selector should be set to to LO: LO:

A

To decrease the BLEED AIR demand from the engines and therefore to save fuel. fuel.

B

To decrease the BLEED AIR demand from the APU. APU.

C

To decrease the cabin temperature. temperature.

D

To decrease the HOT AIR demand from the engine bleeds. bleeds.

AIR COND - 2A0B

Have COND” ALTN COND” page Have aa look look at at the the ECAM ECAM ““COND” page :: ““ALTN MODE” ” is MODE displayed MODE” is displayed. displayed.. What ? happened What happened? happened?

A

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

B

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

C

Temperature regulation is completely lost. lost.

AIR COND - 2A0C

Have COND” PACK COND” page Have aa look look at at the the ECAM ECAM ““COND” page :: ““PACK REG” ” is REG displayed REG” is displayed. displayed.. What ? mean What does does itit mean? mean?

A

The ZONE CONTROLLER has failed, failed, temperature regulation is not done via the HOT AIR valve. valve.

B

The ZONE CONTROLLER has failed and the two packs deliver a fixed temperature

C

The two packs are lost and there is no more air conditioning. conditioning.

D

All the valves are closed and the RAM AIR must be used for the cabin air conditioning. conditioning.

AIR COND - 2A0D

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

A

The RAM AIR pb has been pressed. pressed.

B

On the ECAM SD, SD, the RAM AIR inlet valve should be amber if it is fully open in flight. flight.

C

Aircraft is depressurized, depressurized, but after the RAM AIR valve opens at least one pack should be pressurized again. again.

D

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

AIR COND - 2A0E

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

A

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

B

Monitor the function of the outflow valve. valve.

C

Protect against excessive cabin altitude. altitude.

D

Protect against excessive differential pressure. pressure.

PRES – 2B00

On On the the CABIN CABIN PRESS PRESS panel panel with with aa LDG LDG ELEV ELEV set set manually, , is there still an automatic control manually manually, is there still an automatic control of of the the cabin ? altitude cabin altitude? altitude?

A

No, No, in this case the cabin altitude has to be controlled through the MAN V/ V/S CTL. CTL.

B

Yes, Yes, SYS1 SYS1 is still controlling the cabin altitude through the outflow valve. valve.

C

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

D

No, No, in this case the cabin altitude has to be controlled through the LDG ELEV selector. selector.

PRES – 2B01

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

A

5.3 psi

B

6.9 psi

C

7.6 psi

D

8.6 psi

??

PRES – 2B02

Regarding system Regarding the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system,, what should the differential pressure be on what should the differential pressure be on the the ground? ? ground ground?

A

0 psi

B

0.5 psi

C

1.0 psi

D

8.6 psi

PRES – 2B03

On system On the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system,, safety …. valves safety valves… valves….

the the

A

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

B

Are controlled with the MODE SEL pb. pb.

C

Are controlled with the DITCHING pb. pb.

D

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

PRES – 2B04

On panel On the the CABIN CABIN PRESS PRESS panel, panel,, the the LDG LDG ELEV ELEV has has been set manually. . been set manually manually. What What is is the the approximate approximate value value ??

A

6 ft. ft.

B

60 ft. ft.

C

600 ft. ft.

D

6000 ft. ft.

PRES – 2B05

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

A

The outflow valve. valve.

B

The air intake valve. valve.

C

The air outlet valve. valve.

D

The safety valve. valve.

PRES – 2B06

On page On the the ECAM ECAM STATUS STATUS page, page,, as as you you can can see see cabin cabin pressure control is manual. . You want descend pressure control is manual manual. You want descend from from FL ? 330 ATL FL 390 390 to to FL FL 330. 330.. What What is is your your target target CABIN CABIN ATL? ATL?

A

0 ft. ft.

B

5000 ft. ft.

C

5900 ft. ft.

D

6500 ft. ft.

PRES – 2B07

On /S CTL panel V On the the CABIN CABIN PRESS PRESS panel, panel,, with with the the MAN MAN V/ V/S CTL held ... DN position valve held in in the the DN, DN,, the the position, position,, the the outflow outflow valve... valve...

A

Opens, Opens, the cabin altitude raises. raises.

B

Opens, Opens, the cabin altitude drops. drops.

C

Closes, Closes, the cabin altitude raises. raises.

D

Closes, Closes, the cabin altitude drops. drops.

PRES – 2B08

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

A

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

B

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

C

Intermediate configuration (a/c in flight, flight, high skin temperature). temperature).

VENT – 2C00

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

A

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

B

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

C

Intermediate configuration (a/c in flight, flight, high temperature). temperature).

VENT – 2C01

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

A

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

B

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

C

Intermediate configuration (a/c in flight, flight, high temperature). temperature).

VENT – 2C02

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

A C B

VENT – 2C03

You FCU You are are climbing climbing to to the the altitude altitude set set in in FCU. FCU.. What happens if the V/ / S FPA selector knob What happens if the V V/S-FPA selector knob is is pushed? ? pushed pushed?

A

The aircraft immediately levels off. off.

B

The V/ V/S-FPA target is unchanged. unchanged.

C

The aircraft follows the selected V/ V/S-FPA. FPA.

AUTO FLT - 2201

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

A

The aircraft reverts to TRK. TRK.

B

The HDG/ HDG/TRK target changes. changes.

C

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

D

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

AUTO FLT – 2202

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

A

The aircraft reverts to the original FF-PLN. PLN.

B

The HDG target changes to TRK. TRK.

C

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

D

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

AUTO FLT – 2203

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

A B

C

D

AUTO FLT – 2204

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

A

Track

B

Heading

AUTO FLT – 2205

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

A

The active lateral mode which is a constraint. constraint.

B

The armed lateral mode. mode.

C

The armed lateral mode which is a constraint. constraint.

D

The active lateral mode. mode.

AUTO FLT – 2207

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

A

The active lateral mode which is a constraint. constraint.

B

The armed lateral mode. mode.

C

The armed lateral mode which is a constraint. constraint.

D

The active lateral mode. mode.

AUTO FLT – 2208

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

A

disconnected. disconnected.

B

armed. armed.

C

active. active.

AUTO FLT – 2209

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

A

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

B

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

C

As soon as the aircraft passes FL 60, 60, the target altitude on the PFD will change to FL 150 and the aircraft continues to climb. climb.

D

The aircraft will level off at FL 60. 60. The PF must pull the ALT selection knob a second time to climb to FL 150. 150.

AUTO FLT – 220C

The 150 The FCU FCU target target altitude altitude is is FL FL 150, 150,, you you are are climbing climbing toward constraint toward an an ALT ALT constraint. constraint.. What What will will happen happen ifif the the PF PF pushes pushes the the ALT ALT selection selection knob? ? knob knob? NOTE: : The 60.. NOTE FL NOTE: The constraint constraint alt alt is is FL60 FL60.

A

The aircraft will level off at FL 60. 60. The PF must push or pull the ALT selection knob a second time to climb to FL 150. 150.

B

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

C

As soon as the aircraft passes FL 60, 60, the target on the PFD will change to FL 150 and the aircraft continues to climb. climb.

D

No change, change, the aircraft will stop the climb at FL 60 until passing the constraint then continue climb to FL 150. 150.

AUTO FLT – 220D

The 150 The FCU FCU target target altitude altitude is is FL FL 150, 150,, you you are are climbing climbing toward constraint toward an an ALT ALT constraint. constraint.. What /TRK HDG What will will happen happen ifif the the PFpulls PFpulls the the HDG/ HDG/TRK selection ? now selection knob knob now? now?

A

The aircraft will continue on the present heading, heading, stop the climb at FL 60. 60.

B

The aircraft will stay on the present heading, heading, disregard the constraint and climb to FL 150. 150.

C

The aircraft will follow the FF-PLN, PLN, stop the climb at FL 60 until passing the constraint then continue climb to FL 150. 150.

D

The aircraft will follow the FF-PLN, PLN, disregard the constraint and climb to FL 150. 150.

AUTO FLT – 220E

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

A

It means these waypoints will be overflown. overflown.

B

It means these waypoints are compulsory reporting points. points.

C

It indicates altitude constraints at these waypoints. waypoints.

D

It indicates speed constraints at these waypoints. waypoints.

AUTO FLT – 220F

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

A

The FMGC warns you about a possible overspeed. overspeed.

B

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

C

Due to some environmental circumstances, circumstances, the aircraft missed a speed constraint. constraint.

D

You are advised to slow the aircraft to loose energy so that you will be able to intercept the descent path. path.

AUTO FLT – 220G

The /c is 250 as aa/c FL FCU The a/ is climbing climbing to to FL250 FL250 as set set on on the the FCU, FCU,, an an altitude constraint has been inserted at FL90 90. altitude constraint has been inserted at FL FL90.. What /c reaches 90? ? aa/c FL What is is the the procedure procedure when when the the a/ reaches FL90 FL90?

A

The pilot flying must push the ALT knob. knob.

B

The pilot flying must turn the ALT knob. knob.

C

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

D

The a/ a/c will not match the constraint, constraint, the pilot has to climb by using V/ V/S mode. mode.

AUTO FLT – 220H

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

A

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

B

Randomly at power up. up.

C

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

D

It is always FMGC1 FMGC1.

AUTO FLT – 220J

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

A

The FMGC1 FMGC1.

B

The FMGC2 FMGC2.

C

The randomly chosen FMGC. FMGC.

AUTO FLT – 220K

Setting Setting the the thrust thrust levers levers onto onto TOGA TOGA will will arm arm the the A / THR. . THR A/THR. Where /THR is ? A armed Where do do you you check check that that the the A/ A/THR is armed? armed?

A

On the FMA, FMA, in the Autothrust mode column. column.

B

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

C

On the thrust levers FLEX detent. detent.

D

On the MCDU takeoff page. page.

AUTO FLT – 220M

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

A

The altitude window shows digits as the target altitude is always set manually by the pilot. pilot.

B

The altitude selector knob has not been pushed. pushed.

C

The altitude selector knob has not been pulled. pulled.

D

Both autopilots must be engaged. engaged.

AUTO FLT – 220N

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

A

The target speed is managed by the FMGC. FMGC.

B

A speed target is selected. selected.

C

The pilot has pulled the speed selector knob. knob.

D

The autothrust mode is speed. speed.

AUTO FLT – 220O

You mode You are are in in managed managed speed speed mode. mode.. IfIf you you pull pull the the speed selector knob, , which speed value speed selector knob knob, which speed value will will appear appear on on the the FCU FCU window window ??

A

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

B

VLS + 20 kt. kt.

C

The current speed or mach that is used by the FMGC. FMGC.

D

VMO or MMO. MMO.

AUTO FLT – 220P

When When can can you you engage engage autopilots autopilots 1+2 1+2 at at the the same same time? ? time time?

A

Never. Never.

B

For any kind of approach. approach.

C

As soon as the APPR mode is armed for an ILS approach. approach.

D

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

AUTO FLT – 220S

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

A

ALT is armed, armed, a constraint has been inserted in the FF-PLN. PLN.

B

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

C

The aircraft is on descent and the target altitude is higher than the current aircraft altitude. altitude.

D

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

AUTO FLT – 220U

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

A

A/THR is armed. armed.

B

A/THR is disconnected. disconnected.

C

A/THR is available. available.

D

A/THR is active. active.

AUTO FLT – 220V

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

A

Provide guidance, guidance, if a localizer is available for taketake-off and rollroll-out phases. phases.

B

Provide guidance after taketake-off up to 1000 feat AGL to maintain the runway center line. line.

C

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

D

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

AUTO FLT – 2210

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

A

The thrust has been manually set to TOGA. TOGA.

B

The autothrust system is inoperative. inoperative.

C

The FMGC guidance autothrust command is unserviceable. unserviceable.

D

The pilot has disconnected the autothrust system. system.

AUTO FLT – 2212

A /THR is ? armed mean A/THR is armed. armed.. What What does does itit mean? mean?

A

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

B

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

C

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

AUTO FLT – 2213

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

A

We have reached the thrust reduction altitude. altitude.

B

The autothrust levers are stuck and can not be put in the climb detent. detent.

C

The pilot has forgotten to enter the FLEX temperature on the MCDU taketake-off page before taking off. off.

D

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

AUTO FLT – 2214

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

A

The speed is controlled by the thrust and the rate of climb by the autopilot. autopilot.

B

The speed and the rate of climb are maintained by the autopilot. autopilot.

C

The climb is controlled by the thrust and the target speed is maintained by the autopilot which adjust the pitch. pitch.

D

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

AUTO FLT – 2215

The The aircraft aircraft levels levels off off at at 13000 13000 feet feet ALT ALT green green on on the the FMA, : FMA mode FMA,, the the autothrust autothrust is is in in SPEED SPEED mode: mode:

A

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

B

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

C

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

D

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

AUTO FLT – 2216

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

A

To engage the manual mode of the autothrust. autothrust.

B

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

C

To disconnect the A/ A/THR. THR.

AUTO FLT – 2217

According indications According to to FCU FCU and and FMA FMA indications, indications,, what what happened? ? happened happened?

A

The pilot flying has set the thrust levers to IDLE to reduce the thrust for landing. landing.

B

The autothrust is now disconnected. disconnected.

C

The autothrust manual mode is engaged. engaged.

D

A and B are correct. correct.

AUTO FLT – 2218

Have -PLN page. FF-PLN page Have aa look look at at the the MCDU MCDU Fpage.. Notice Notice the the small white arrow shown on the right top small white arrow shown on the right top. top.. ItIt indicates indicates that that ::

A

We can move this page to the right. right.

B

Another page is automatically displayed in relation to the phase of the flight. flight.

C

We can access to another page by acting on NEXT PAGE key. key.

AUTO FLT – 221C

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

A

The runway threshold position. position.

B

The aircraft present position. position.

C

The airport reference point position. position.

D

The alternate airport position

AUTO FLT – 221D

The -PLN page FF-PLN The Fpage shown shown in in the the MCDU MCDU is is ::

A

The FF-PLN page A. A.

B

The FF-PLN page B. B.

AUTO FLT – 221E

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

A

It is the secondary FF-PLN. PLN.

B

It is a temporary FF-PLN. PLN.

C

It is the engine out standard instrument departure. departure.

D

It is the standard departure for light airplanes. airplanes.

AUTO FLT – 221H

Have R is MCDU 23 Have aa look look at at the the MCDU, MCDU,, the the ILS ILS 23R 23R is aa currently currently selected : approach means selected approach, approach,, the the green green color color means: means:

A

This approach is inserted into the active F-PLN. PLN.

B

This approach is displayed in green before insertion in the FF-PLN. PLN.

C

This approach can not be selected. selected.

AUTO FLT – 221K

The L has 23 selected The ILS ILS 23L 23L has been been currently currently selected, selected,, the the yellow yellow fonts : means fonts means: means:

A

The selection has been made on the secondary FPLN. FPLN.

B

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

C

The selection is temporary and must be inserted to become active or erased to be rejected. rejected.

D

The crew has made a wrong selection. selection.

AUTO FLT – 221L

The -PLN waypoint FF-PLN The lateral lateral revision revision page page from from aa Fwaypoint shows /TO data : VIAGO field used shows VIAGO/ VIAGO/TO data field, field,, itit is is used: used:

A

To buildbuild-up a FF-PLN waypoint by waypoint. waypoint.

B

To enter VIA a beacon TO a waypoint. waypoint.

C

To build routes using airways. airways.

D

To enter VIAGO/ VIAGO/TO a new airport. airport.

AUTO FLT – 221M

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

A

The PROG page. page.

B

The PERF takeoff page. page.

C

The A/ A/C STATUS page. page.

D

The FUEL PRED page. page.

AUTO FLT – 221P

Which Which data data do do you you need need to to enter enter in in MCDU MCDU in in order order to ? computation to obtain obtain the the operating operating speed speed computation? computation?

A

The flaps lever moving onto the take off setting. setting.

B

ZFWCG. ZFWCG.

C

The ZFW and block fuel. fuel.

D

The block fuel only. only.

AUTO FLT – 221Q

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

A

V2 as manually set on the FCU by the pilot flying. flying.

B

V1.

C

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

D

V2 + 10. 10.

AUTO FLT – 221S

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

A

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

B

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

C

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

AUTO FLT – 221T

FCU 150,, the FL FCU clearance clearance is is FL150 FL150, the aircraft aircraft is is climbing climbing toward FL60 60 as shown on PFD. . toward FL FL60 as shown on PFD PFD. Why 60 displayed ? FL magenta Why is is FL60 FL60 displayed in in magenta? magenta?

A

This is an altitude constraint. constraint.

B

A speed constraint is entered. entered.

C

The active vertical mode is not OP CLB. CLB.

D

The aircraft rate of climb is too low. low.

AUTO FLT – 221W

Have ND Have aa look look at at the the ND, ND,, ahead ahead of of the the aircraft aircraft symbol symbol and -PLN, FF-PLN, PLN, aa small and along along the the Fsmall magenta magenta arrow arrow is is shown. shown shown.. What ? mean What does does itit mean? mean?

A

The aircraft is in OP CLB mode. mode.

B

The altitude constraint cannot be satisfied. satisfied.

C

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

D

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

AUTO FLT – 221X

On path running On the the climb climb flight flight path, path,, 22 engines engines running, running,, the the SRS SRS ((speed speed reference system) ) provides a pitch attitude reference system system) provides a pitch attitude to : maintain to maintain: maintain:

A

V2.

B

V2 + 10. 10.

C

F speed. speed.

D

The existing speed. speed.

AUTO FLT – 221Y

You target You are are flying flying aa selected selected HDG HDG target. target.. How How do do you you proceed -PLN? FF-PLN? PLN? proceed to to resume resume the the normal normal F-

A

I turn right to intercept the FF-PLN after the TO waypoint. waypoint.

B

I maintain the present heading and I push the heading selector knob to arm the NAV mode. mode.

C

I maintain the present heading waiting for the automatic interception. interception.

D

I pull the HDG selector knob. knob.

AUTO FLT – 221Z

You target You are are flying flying aa selected selected heading heading target. target.. A A white white dot dot is displayed on the FCU beside the selected HDG is displayed on the FCU beside the selected HDG. HDG.. What ? mean What does does itit mean? mean?

A

The lateral managed mode has been selected and is armed. armed.

B

The lateral selected mode is not satisfactory. satisfactory.

C

The managed mode is active. active.

D

The selected mode is not engaged. engaged.

AUTO FLT – 2220

ALT engaged ALT mode mode is is engaged, engaged,, MCDU MCDU PERF PERF page page indicates indicates CLB. ? CLB Why CLB.. Why? Why?

A

The FMGS is unable to control the climb. climb.

B

FL290 FL290 is the FCU selection, selection, and is below the CRZ FL. FL.

C

The FMGS assumes that you will continue the CLB higher than 290. 290.

D

B and C are correct. correct.

AUTO FLT – 2221

ALT 290,, MCDU FL ALT mode mode is is engaged engaged at at FL290 FL290, MCDU PERF PERF page page indicates CLB. . How do you obtain ALT CRZ indicates CLB CLB. How do you obtain ALT CRZ on on the the FMA FL290 FL290)) ?? FMA at at that that altitude altitude ((FL290)

A

Set the new altitude clearance FL290 FL290 on the MCDU PROG page. page.

B

Set the new altitude clearance on the FCU. FCU.

C

Push the altitude selector knob to continue the climb as programmed before. before.

AUTO FLT – 2222

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

A

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

B

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

C

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

D

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

AUTO FLT – 2223

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

A

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

B

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

C

Only automatically at the deceleration point. point.

AUTO FLT – 2225

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

A

Which autopilot is engaged. engaged.

B

The vertical mode previously flown. flown.

C

Which FMGC is the master. master.

D

The aircraft configuration. configuration.

AUTO FLT – 2226

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

A

By pulling the heading selector knob. knob.

B

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

C

By pressing the approach mode pushbutton. pushbutton.

D

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

AUTO FLT – 2227

You descent You are are in in descent. descent.. A A small small magenta magenta dot dot is is displayed beside the altitude scale. . displayed beside the altitude scale scale. ItIt is : to is used used to: to:

A

Warn the pilot about a possible wrong altitude setting on the FCU. FCU.

B

Highlight any vertical deviation of the aircraft from the computed descent profile. profile.

C

Warn the pilot that the speed must be reduced to regain the computed descent profile. profile.

D

Indicate that the expedite mode must be engaged. engaged.

AUTO FLT – 2228

We around We are are at at go go around, around,, GA GA TRK TRK is is shown shown on on the the FMA FMA lateral mode. . lateral mode mode. What ? mean What does does itit mean? mean?

A

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

B

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

C

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

D

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

AUTO FLT – 222B

Any triggered Any time time the the alpha alpha floor floor protection protection is is triggered, triggered,, TOGA thrust is automatically set by the autothrust TOGA thrust is automatically set by the autothrust. autothrust.. When is this protection available? ? When is this protection available available?

A

Throughout the whole flight envelope. envelope.

B

Only available on configuration 2, 3 or full (with flaps extended). extended).

C

From lift off until 20 feet on approach. approach.

D

From lift off until 100 feet on approach. approach.

AUTO FLT – 222D

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

A

First time to disconnect the autopilot. autopilot. Second time to confirm the disconnection. disconnection.

B

For the first time to disconnect the autopilot for the second time to get a definite priority on his side. side.

C

For the first time to disconnect the autopilot for the second time to reset all the related warnings. warnings.

D

For the first time to disconnect the autopilot for the second time to reset the master FMGC. FMGC.

AUTO FLT – 222J

What ATHR limited” ” amber limited What does does the the autopilot autopilot ““ATHR limited” amber message /WD mean? ? E mean message displayed displayed on on the the ECAM ECAM E/ E/WD mean?

A

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

B

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

C

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

D

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

AUTO FLT – 222L

Both Both autopilots autopilots are are engaged engaged which which FMGC FMGC is is master? ? master master?

A

FMGC1 FMGC1.

B

FMGC2 FMGC2.

C

It depends on the active flight phase. phase.

D

None as the two FMGC’ FMGC’s are acting independently. independently.

FMGC 1

FMGC 2

AUTO FLT – 222N

FD1 1 +2 FD ON engaged FD1 +2 are are ON, ON,, no no AP AP is is engaged, engaged,, which which FMGC FMGC is is master? ? master master?

A

The switching occurs at every FMGC power up. up.

B

It depends on which ATHR channel is engaged. engaged.

C

FMGC2 FMGC2.

D

FMGC1 FMGC1.

FMGC 1

FMGC 2

AUTO FLT – 222O

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

A

FMGC1 FMGC1.

B

FMGC2 FMGC2.

C

None, None, the two FMGC’ FMGC’s are acting independently. independently.

D

It depends on which FMGC was the master at the time of dual mode failure. failure.

FMGC 1

FMGC 2

AUTO FLT – 222P

The OPP FMGC ” message PROCESS The ““OPP FMGC IN IN PROCESS” PROCESS” message is is displayed displayed in in amber amber on on the the scratchpad scratchpad of of the the MCDU1 1. MCDU MCDU1. What ? mean What does does itit mean? mean?

A

MCDU1 MCDU1 is driven by FMGC2 FMGC2.

B

The FMGC2 FMGC2 is now master. master.

C

The FMGC2 FMGC2 performance became better than the FMGC1 FMGC1.

AUTO FLT – 222Q

The SET OFFSIDE ” amber MODE The message message ““SET OFFSIDE RANGE RANGE MODE” MODE” amber appears on the ND1 1 . appears on the ND ND1. What ? mean What does does itit mean? mean?

A

The selection of the offside range mode will allow the display of the navigation map on this side. side.

B

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

C

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

D

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

AUTO FLT – 222R

The 1 has ? FCU failed now The FCU1 FCU1 has failed, failed,, how how can can we we use use the the FCU FCU now? now?

A

Normal use of the FCU as the FCU channel 2 has taken over automatically. automatically.

B

The FCU is totally unserviceable. unserviceable.

C

Only the lateral modes can be set from the FCU panel. panel.

D

Some FCU functions LOC and APP pushbuttons are not available. available.

AUTO FLT – 222T

The failed The FCU FCU 11 and and 22 have have failed, failed,, how how the the pilot pilot can can control ? modes control the the vertical vertical and and lateral lateral modes? modes?

A

Both AP’ AP’s are lost but the FCU controls and indications are still available. available.

B

Only the FD1 FD1 and 2 are available. available.

C

The vertical and lateral modes cannot be controlled from the FCU. FCU. Only the manual flight on raw data is possible. possible.

D

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

AUTO FLT – 222U

The independent operation” ” is operation The message message ““independent operation” is displayed displayed on both MCDU scratchpads. . on both MCDU scratchpads scratchpads. What ? mean What does does itit mean? mean?

A

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

B

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

C

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

AUTO FLT – 222V

Due data base ), we validity Due to to aa major major mismatch mismatch ((data base validity) validity), we are are on independent operation” ” mode. operation mode on FMGC FMGC ““independent operation” mode.. When When the the discrepancy disappears discrepancy disappears, disappears,, what what will will be be your your action action to to recover ? mode recover the the dual dual mode? mode?

A

I will reset the two FMGC circuit breakers. breakers.

B

I will select MCDU menu and FMGC on each FMGC. FMGC.

C

As the FMGC1 FMGC1 is now the master, master, I will only reset the FMGC2 FMGC2 circuit breaker. breaker.

D

I do nothing as the system reverts automatically to “dual mode” mode”.

AUTO FLT – 222W

The 1 failed OPP FMGC ” is FMGC PROCESS The FMGC1 FMGC1 failed and and ““OPP FMGC IN IN PROCESS” PROCESS” is displayed on the MCDU1 1 . The FMGC2 2 has taken displayed on the MCDU MCDU1. The FMGC FMGC2 has taken over over automatically automatically ::

A

The entry can be done from either MCDU. MCDU.

B

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

C

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

FMGC 1

FMGC 2

AUTO FLT – 222X

You THR IDLE/ /DES” IDLE DES” modes You are are in in ““THR IDLE/DES” modes with with autopilot autopilot 11 engaged and the FCU 1 fails. . engaged and the FCU 1 fails fails. What ? required What is is the the action action required? required?

A

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

B

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

C

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

AUTO FLT – 222Z

You mechanic You want want to to speak speak to to the the mechanic. mechanic.. He He is is somewhere around the aircraft but you ’t see can somewhere around the aircraft but you can’ can’t see him. . How do you get his attention? ? him him. How do you get his attention attention?

A

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

B

I use the MECH pb sw on the CALLS panel. panel.

C

I use VHF 3 to call him. him.

D

I select the MECH transmission key on the ACP. ACP.

COMM - 2300

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

A

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

B

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

C

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

D

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

COMM – 2301

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

A

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

B

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

C

The aircraft must be off the ground. ground.

D

The engines must be shut down for at least 5 minutes. minutes.

COMM – 2302

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

RMP 1

A

It is an indication for a SELCAL. SELCAL.

B

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

RMP 2

C

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

D

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

COMM – 2303

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

RMP 1

A

Pressing the SEL pb on RMP 1.

B

Pressing the VHF 1 and SEL pb on RMP 1.

C

Pressing the SEL pb on RMP 2.

D

Pressing the VHF 2 on RMP 2.

RMP 2

COMM – 2304

On system failure On the the VHF VHF system, system,, in in case case of of RMP RMP 11 failure, failure,, VHF VHF 11 is lost is lost. lost..

A

True. True.

B

False. False.

COMM – 2305

With With the the AUDIO AUDIO SWITCHING SWITCHING knob knob in in the the CAPT CAPT 33 position, position position,, the the captain captain substitutes substitutes ACP ACP 33 for for ACP ACP 11..

A

True. True.

B

False. False.

COMM – 2306

On panel On the the communication communication control control panel, panel,, the the amber amber CALL light indicates that somebody is CALL light indicates that somebody is trying trying to to reach reach you you via via VHF VHF 33..

A

True. True.

B

False. False.

COMM – 2307

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

A

You must check that the external power is available and then switch it on. on.

B

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

C

You have to switch each battery on by its associated pb sw to check the voltage. voltage.

ELEC - 2400

According indications According to to these these indications, indications,, which which statement statement is is true true ??

A

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

B

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

C

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

D

I can only check the battery voltages, voltages, with batteries on. on.

ELEC – 2401

You batteries You want want to to recharge recharge the the batteries. batteries.. How ? proceed How do do you you proceed? proceed?

A

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

B

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

C

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

D

I have to call a mechanic because the batteries can only be charged by maintenance. maintenance.

ELEC – 2402

What What is is the the meaning meaning of of the the green green AVAIL AVAIL light light ??

A

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

B

The external power is plugged in. in.

C

The external power panel door has been opened. opened.

D

The AVAIL light always illuminates on ground. ground.

ELEC – 2403

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

A

You have to switch the generators to ON. ON.

B

A failure has been detected. detected. The generators will not be able to supply the electrical system after engine start

C

There is an internal self test in progress. progress. The fault lights and the amber indications should disappear after 30 seconds. seconds.

D

On ground these indications are normal when the engines are not running. running.

ELEC – 2404

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

A

10 minutes

B

One hour

C

20 minutes

D

Several hours

ELEC – 2405

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

A

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

B

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

C

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

D

Both battery voltages are now above the minimum voltage. voltage.

ELEC – 2406

You APU You have have started started the the APU. APU.. Observe Observe ECAM ECAM ELEC ELEC page page !! Why Why is is the the electrical electrical system system still still supplied supplied by by external external power power only only ??

A

External power was connected first. first.

B

External power has priority over the APU generator. generator.

C

The APU generator is still switched off. off.

D

The external power voltage is more stable. stable.

ELEC – 2407

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

A

engines, engines, external power, power, APU. APU.

B

APU, APU, engines, engines, external power. power.

C

external power, power, engines, engines, APU. APU.

D

APU, APU, external power, power, engines. engines.

ELEC – 2408

On Panel On the the ELEC ELEC Panel, Panel,, you you have have lifted lifted the the IDG IDG red red guard. . guard guard. How How do do you you disconnect disconnect the the IDG IDG now now ??

A

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

B

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

C

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

D

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

ELEC – 2409

You You are are in in an an ELECTRICAL ELECTRICAL EMERGENCY EMERGENCY CONFIGURATION, CONFIGURATION occurred CONFIGURATION,, shortly shortly after after the the fault fault occurred, occurred,, you notice the red FAULT light on the RAT you notice the red FAULT light on the RAT & & EMER EMER GEN pushbutton. . GEN pushbutton pushbutton. How How do do you you interpret interpret this this indication indication ??

A

The EMER GEN is not supplying the system. system.

B

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

C

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

ELEC – 240C

You You are are in in an an ELECTRICAL ELECTRICAL EMERGENCY EMERGENCY CONFIGURATION, CONFIGURATION CONFIGURATION,, on on ELEC ELEC panel panel you you have have depressed the GEN 1 and GEN 2 pb for reset. depressed the GEN 1 and GEN 2 pb for reset reset.. The unsuccessful The reset reset was was unsuccessful. unsuccessful.. Why must you Why must you push push the the BUS BUS TIE TIE pb pb sw sw to to OFF OFF ??

A

To separate both sides of the electrical system. system.

B

To connect both generators directly to the AC ESS BUS. BUS.

C

To connect both sides of the electrical system. system.

D

To switch both generators to the opposite side AC BUS. BUS.

ELEC – 240D

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

A

If there was a short circuit, circuit, you might recover one generator now. now.

B

Because the generators had time to cool down and now a reset might be successful. successful.

C

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

ELEC – 240E

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

A

Disconnect the corresponding generator from its drive shaft. shaft.

B

Reconnect the generator to its drive mechanism. mechanism.

C

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

D

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

ELEC – 240I

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

A

At the engine RPM trough their gearbox connection. connection.

B

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

C

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

D

No necessity to control the generator speed because the AC network operates under variable frequency. frequency.

GEN 1

GEN 2

IDG 1

IDG 2

ELEC – 240J

The : AC buses The Electrical Electrical System System includes includes two two buses: buses: AC ESS ESS BUS and DC ESS BUS. . BUS and DC ESS BUS BUS. In In normal normal configuration configuration ::

A

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

B

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

C

To balance the Elec load GEN 1 is directly supplying the AC ESS BUS. BUS.

D

To balance the Elec load GEN 2 is directly supplying the AC ESS bus. bus.

ELEC – 240K

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

A

From AC bus 2 to AC bus 1.

B

From AC bus 1 to AC bus 2.

C

From the APU generator. generator.

D

From ESS DC bus. bus.

ELEC – 240M

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

A

B

C

ELEC – 240N

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

A

B

C

ELEC – 240O

The The emergency emergency electrical electrical generator generator used used as as aa back back up up is is hydraulically hydraulically driven driven by by the the RAT RAT which which automatically automatically extends extends when when both both AC AC BUS BUS 11 and and AC AC BUS 2 are lost and the aircraft speed is BUS 2 are lost and the aircraft speed is above above 100kts kts.. 100 100kts.

A

True. True.

B

False. False.

ELEC – 240P

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

A

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

B

The APU GEN pb SW on overhead panel is off. off.

C

The APU is not fully available yet. yet.

D

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

ELEC – 240Q

Looking Page Looking at at the the ECAM ECAM ELEC ELEC Page, Page,, to to connect connect APU APU GEN: : GEN GEN:

A

Push APU GEN pb sw located overhead panel. panel.

B

Wait until 1st Engine is Started. Started.

C

Deselect EXT PWR. PWR.

D

SWITCH OFF BAT 1+2. 1+2.

ELEC – 240R

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

A

APU GEN shares 36% 36% of the elec network load, load, the remaining 64% being taken by the external power. power.

B

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

C

The external power is supplying the network. network.

ELEC – 240S

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

A

Switched ON. ON.

B

Switched OFF. OFF.

C

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

ELEC – 240U

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

A

24V 24V.

B

25,5V 25,5V.

C

28V 28V.

ELEC – 240V

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

A

The ground cart is supplying the aircraft network. network.

B

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

C

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

ELEC – 240X

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

A

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

B

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

C

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

ELEC – 240Y

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

A

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

B

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

C

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

ELEC – 240Z

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

A

Yes. Yes.

B

No. No. The APU should continue powering the aircraft until crew switch it off. off.

C

No. No. GEN1 GEN1 should supply AC1 AC1 and AC2 AC2.

D

No. No. GEN2 GEN2 should supply AC1 AC1 and AC2 AC2.

ELEC – 2410

At gate down At the the gate, gate,, with with both both engines engines shut shut down, down,, is is this this ECAM ECAM ELEC ELEC page page configuration configuration correct correct ??

A

Yes. Yes.

B

No. No.

C

The crew should shut down one engine at a time to reach this configuration. configuration.

D

The crew should select EXT POWER ON. ON.

ELEC – 2411

You gate You are are at at the the gate, gate,, APU APU GEN GEN is is supplying supplying the the network, network in network,, the the EXT EXT POWER POWER is is plugged plugged in. in.. What What will will happen happen when when EXT EXT POWER POWER is is selected selected ON? ? ON ON?

A

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

B

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

C

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

D

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

ELEC – 2412

GEN GEN 11 is is now now inoperative inoperative due due to to the the ECAM ECAM procedure procedure application application following following an an IDG IDG OIL OIL LO LO PR PR caution. caution caution.. Is ? available Is the the associated associated AC AC BUS BUS still still available? available?

A

Yes. Yes. AC ESS is supplying the AC 1.

B

Yes. Yes. GEN 2 has taken over. over.

C

No. No. GEN 2 will be disconnected from AC BUS 2 within 10 minutes. minutes.

D

No. No. APU must be started to recover AC BUS 1.

ELEC – 2413

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

A

Minimum 3 seconds. seconds.

B

Maximum 3 seconds. seconds.

C

Until fault amber light goes out. out.

D

No time limit. limit.

ELEC – 2414

In caution In case case of of GEN GEN 22 OVERLOAD OVERLOAD ECAM ECAM caution, caution,, how how do ? generator do you you off off load load the the generator? generator?

A

By starting the APU to connect a third generator to share the load. load.

B

By switching OFF the galley. galley.

C

By transferring load on GEN1 GEN1 in order to keep the galley operating. operating.

ELEC – 2416

Following Following aa GEN GEN 22 OVERLOAD OVERLOAD and and the the shedding shedding of of the ? correct the galley galley is is the the ELEC ELEC page page correct? correct?

A

Yes. Yes.

B

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

C

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

ELEC – 2417

In flight FAULT In flight, flight,, following following an an AC AC BUS BUS 11 FAULT, FAULT,, AC AC ESS ESS FEED : to FEED pb pb sw sw must must be be depressed depressed in in order order to: to:

A

Recover AC ESS FEED from AC BUS 2.

B

Recover AC1 AC1 bus. bus.

C

Recover AC2 AC2 bus. bus.

ELEC – 241A

AC AC BUS BUS 11 FAULT FAULT will will definitively definitively lead lead to to the the DC DC and loss and AC AC ESS ESS buses buses loss: loss::

A

Yes. Yes.

B

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

C

No. No. DC and AC ESS buses will be recovered by pushing on the AC ESS FEED pb sw. sw.

ELEC – 241B

Following fault Following an an AC AC BUS BUS 11 fault, fault,, pushing pushing the the AC AC ESS ESS FEED : you FEED pb pb sw sw on on ELEC ELEC overhead overhead panel panel allows allows you: you:

A

To recover the AC ESS BUS power only. only.

B

To recover the DC ESS BUS power only. only.

C

To recover AC and DC ESS buses. buses.

D

To recover AC BUS 1 power. power.

ELEC – 241C

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

A

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

B

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

C

The emergency generator is not connected. connected.

ELEC – 241D

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

A

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

B

Even after having reset one generator successfully. successfully.

C

Even if BUS TIE pb sw is pushed. pushed.

D

Even if APU is started. started.

ELEC – 241F

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

A

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

B

Reset each AC generator. generator.

C

Manually lower RAT by pushing its pb SW

D

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

ELEC – 241H

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

A

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

B

Electrical network is automatically transferred to the batteries. batteries.

C

You have to stop AC generator by pressing the “MAN ONON-AUTO” AUTO” pb switch. switch.

D

You have to switch ON the both batteries. batteries.

ELEC – 241J

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

A

No. No. The upper ECAM screen is only used for E/ E/WD display. display.

B

Yes, Yes, by pressing and holding its associated pb SW on the ECAM control panel. panel.

ELEC – 241M

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

A

The DC ESS. ESS.

B

The complete DC network. network.

C

The AC ESS. ESS.

D

The AC and DC ESS. ESS.

ELEC – 241N

In smoke In case case of of avionics avionics bay bay smoke, smoke,, GEN GEN 11 LINE LINE pb pb is is selected OFF. . selected OFF OFF. What ? happen What will will happen? happen?

A

All warnings will be reset. reset.

B

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

C

GEN1 GEN1 will be disconnected from the network. network.

D

Fire extinguisher bottle will be armed. armed.

ELEC – 241O

Which Which of of these these areas areas have have NO NO fire fire extinguishing extinguishing system ? installed system installed? installed?

A

C

Cabin. Cabin.

D

Avionic bay. bay.

B

Engine / APU. APU.

Cargo compartments. compartments.

FIRE - 2600

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

A

C

Cabin. Cabin.

D

Avionic bay. bay.

B

Engine / APU. APU.

Cargo compartments. compartments.

FIRE – 2601

ItIt is day is the the first first flight flight of of the the day. day.. Before performing the APU test Before performing the APU fire fire test, test,, you you have have to to check that... ... check that that...

A

The APU FIRE pb is in and guarded and AC power is supplied. supplied.

B

The APU FIRE pb is in and guarded and the APU is running. running.

C

The APU FIRE pb is in with the guard in the UP position and the AGENT light is extinguished. extinguished.

D

The APU FIRE pb is in and guarded and the AGENT light is extinguished. extinguished.

FIRE – 2602

The power The aircraft aircraft is is not not yet yet supplied supplied with with AC AC power. power.. Can ? test Can you you perform perform the the APU APU FIRE FIRE test? test?

A

Yes. Yes.

B

No. No.

FIRE – 2603

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

A

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

B

On the FIRE Control Panel, Panel, the APU FIRE red light and SQUIB light will illuminate. illuminate. But the APU FIRE warning will not be triggered on ECAM. ECAM.

C

No test is possible until AC power is connected on the Electrical network. network.

FIRE – 2604

The successful The APU APU FIRE FIRE test test is is successful. successful..

A

True. True.

B

False. False.

FIRE – 2605

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

A

Yes. Yes.

B

No. No.

FIRE – 2606

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

A

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

B

Both fire detection loops of engine 1 have failed. failed. Fire detection for engine 1 is inoperative. inoperative.

C

One fire detection loop of engine 1 has failed. failed. Fire detection for engine 1 is still available. available.

D

One fire detection loop of engine 1 has failed. failed. Fire detection for engine 1 is inoperative. inoperative.

FDU

FIRE – 2607

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

A

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

B

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

C

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

D

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

FIRE – 2608

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

A

There is only one fire bottle which has been discharged into both cargo compartments. compartments.

B

The FWD and AFT fire bottles have both been discharged into their associated compartment. compartment.

C

Now there is no longer any available agent which can be discharged in either the FWD or the AFT cargo compartment. compartment.

D

The FWD and AFT fire bottles have both been discharged into the FWD compartcompartment. ment.

FIRE – 2609

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

A

Ailerons and rudder. rudder.

B

THS and rudder. rudder.

C

Elevator and ailerons. ailerons.

D

THS and elevator. elevator.

FLT CTL - 2701

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

A

2 hydraulic sources with 4 actuators

B

1 hydraulic source with 2 actuators

C

4 hydraulic sources with 4 actuators

D

3 hydraulic sources with 4 actuators

FLT CTL - 2702

What ? indicate What does does the the white white cross cross indicate? indicate?

A

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

B

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

C

It is an indication for the rudder pedals deflections during the flight control check. check.

FLT CTL - 2703

In Law In Normal Normal Law, Law,, ifif one one sidestick sidestick is is rapidly rapidly pulled pulled fully back, , can the airplane’ ’ s maximum fully back back, can the airplane airplane’s maximum allowable allowable ““G” G” load load be be exceeded exceeded ??

A

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

B

Yes, Yes, until maximum pitch attitude is reached. reached.

C

No. No. At maximum “G” load, load, the sidesticks are dede-activated for 5 seconds. seconds.

D

No. No. The load factor limitation overrides sidestick commands to avoid excessive “G” loads. loads.

FLT CTL - 2704

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

A

B

C

FLT CTL - 2705

According indications According to to these these indications, indications,, ifif you you release release the the sidestick … now sidestick now… now…

A

The bank angle will automatically return to 33º 33º.

B

The bank angle will not change. change.

C

The bank angle will return to wings level, level, because the bank protection is active. active.

D

The bank angle will return to 20º 20º.

FLT CTL - 2706

In Law In Normal Normal Law, Law,, what what is is the the maximum maximum bank bank angle angle you you can can reach reach with with the the sidestick sidestick fully fully deflected deflected ??

A

33º 33º

B

There is no bank limitation. limitation.

C

80 º

D

67 º

FLT CTL - 2707

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

A

Normal Law. Law.

B

Alternate Law. Law.

C

Direct Law. Law.

D

Mechanical Back Up. Up.

FLT CTL - 2708

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

A

Normal Law

B

Alternate Law

C

Direct Law

D

Mechanical Back Up

FLT CTL - 2709

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

A

Normal Law

B

Alternate Law

C

Direct Law

D

Mechanical Back Up

FLT CTL – 270A

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

A

Normal Law

B

Alternate Law

C

Direct Law

D

Mechanical Back Up

FLT CTL – 270B

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

A

The aircraft’ aircraft’s attitude will stay constant. constant.

B

The pitch will stay constant, constant, the bank angle will slowly decrease. decrease.

C

The bank angle will stay constant, constant, the pitch will slowly decrease. decrease.

D

The aircraft’ aircraft’s attitude will slowly tend towards “wings level” level” and “pitch 0”.

FLT CTL – 270C

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

A

The High Angle Of Attack protection is active. active.

B

The Alpha Floor protection is active. active.

C

The Load Factor Limitation is active. active.

D

There is no protection active yet. yet.

FLT CTL – 270D

Let’ ’s assume, Let assume Let’s assume,, you you have have set set idle idle power power and and pulled pulled the sidestick back to maintain altitude. . the sidestick back to maintain altitude altitude. Observe Observe the the PFD. ... PFD now PFD.. IfIf you you release release the the sidestick sidestick now... now...

A

The aircraft will descend at 135 kts. kts.

B

The aircraft will descend at 150 kts. kts.

C

The aircraft will maintain altitude until 120 kts are reached .

D

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

FLT CTL – 270E

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

A

The High Angle Of Attack protection is active. active.

B

The Alpha Floor protection is active. active.

C

The Load Factor Limitation is active. active.

D

There is no protection active. active.

FLT CTL – 270F

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

A

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

B

The speed will fall below 120 kts. kts. To avoid a stall, stall, climb power will be automatically set. set.

C

The High Angle Of Attack protection will override the sidestick input. input. The pitch will be lowered to maintain 120 kts. kts.

D

The speed will fall further. further. At 114 kts the pitch will be lowered to maintain 114 kts. kts.

FLT CTL – 270G

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

A

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

B

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

C

The Alpha Floor protection will override sidestick inputs. inputs. The nose will be lowered. lowered.

D

A stall is detected. detected.

FLT CTL – 270H

To ... turn To fly fly aa coordinated coordinated turn... turn...

A

No rudder inputs are required. required.

B

You have to center the sideslip indicator with the rudder pedals. pedals.

C

Only small rudder inputs are required. required.

FLT CTL – 270I

In Law In Normal Normal Law, Law,, is is there there aa maximum maximum pitch pitch attitude attitude ??

A

A

Yes, Yes, indicated by the green dashes (A).

B

B

Yes, Yes, indicated by the green dashes (B).

C

No. No.

D

Yes, Yes, pitch is limited to 20º 20º nose up. up.

FLT CTL – 270J

In Law In Normal Normal Law, Law,, is is there there aa maximum maximum bank bank angle angle ?? a

A

No. No.

B

Yes, Yes, indicated by the green dashes (b).

C

Yes, Yes, indicated by the white dashes (a).

D

Yes, Yes, bank is limited to 80º 80º.

b

FLT CTL – 270K

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

A

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

B

The ailerons are controlled directly by the sidesticks. sidesticks.

C

The bank angle limit protection is lost. lost.

D

The bank angle protection is active. active.

FLT CTL – 270L

The ’s sidestick CPT The CPT’ CPT’s sidestick is is deflected deflected fully fully left left and and the the FO’ ’s sidestick FO FO’s sidestick is is simultaneously simultaneously deflected deflected fully fully right. right right.. Which Which indications indications do do you you expect expect ??

A

B

C

D

FLT CTL – 270M

IfIf both ... back both pilots pilots deflect deflect their their sidesticks sidesticks fully fully back... back...

A

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

B

The “pitch up” up” order is 1.5 times greater than with only one stick deflected. deflected.

C

No inputs are send to the flight control computers unless one pilot presses the take over pb on his stick. stick.

D

The “pitch up” up” order is equal to a single stick fully deflected. deflected.

FLT CTL – 270N

IfIf the ... pb the FO FO presses presses the the take take over over pb... pb...

A

The CPT is unable to rere-activate his sidestick. sidestick.

B

The CPT’ CPT’s sidestick is still active. active. It will be dede-activated after 40 secs. secs.

C

The CPT can rere-activate his sidestick by pressing the take over pb for more than 40 secs. secs.

D

The CPT can rere-activate his sidestick immediately by pressing his take over pb. pb.

CPT CPT

FO FO

FLT CTL – 270O

Let’ ’s assume Let Let’s assume the the FO FO presses presses his his take take over over pb pb and and releases ... secs releases itit after after more more than than 40 40 secs... secs...

40 sec

A

The CPT’ CPT’s sidestick is dede-activated unless he presses his take over pb. pb.

B

The CPT is unable to rere-activate his sidestick for the rest of the flight. flight.

C

Both sidesticks are active. active.

D

The CPT’ CPT’s sidestick is active as long as the FO’ FO’s sidestick is in neutral position

CPT CPT

FO FO

FLT CTL – 270P

With engaged With either either AP AP engaged, engaged,, which which statement statement is is true true ??

A

Both sidesticks are locked in neutral position. position. The lock can not be overridden

B

Both sidesticks are dede-activated until the AP is disengaged. disengaged.

C

Both sidesticks are locked in neutral position. position. By applying a certain force, force, the lock can be overridden but the AP remains engaged. engaged.

D

Both sidesticks are locked in neutral position. position. By applying a certain force, force, the lock can be overridden and the AP is disengaged. disengaged.

FLT CTL – 270Q

What What will will happen happen next next ??

A

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

B

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

C

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

FLT CTL – 270R

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

A

The left SPRL 3 failed to extend. extend.

B

The right SPRL 3 failed to extend. extend.

C

The left SPRL 3 failed to retract. retract.

D

The right SPRL 3 failed to retract. retract.

FLT CTL – 270S

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

A

Auto flap retraction at 210 kts. kts.

B

Auto flap and slat retraction at 210 kts. kts.

C

High Speed protection will become active, active, the autopilot will increase the pitch. pitch.

D

High Speed protection will become active, active, the autothrust will reduce thrust. thrust.

FLT CTL – 270T

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

A

A hydraulic device locks the flaps in their present position. position.

F/CTL FLAPS LOCKED -WING TIP BRK ON MAX SPEED . . . . . . . .

B

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

C

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

D

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

FLT CTL – 270U

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

A

True. True.

B

False. False.

FUEL - 2800

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

A

The Center Tank Pumps alone. alone.

B

The Center Tank Pumps and the inner tank pumps. pumps.

C

The inner Tank Pumps alone. alone.

FUEL – 2801

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

A

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

B

The center tank quantity is 0.

C

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

D

The quantity in the approaching low level. level.

inner

tanks

is

FUEL – 2802

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

A

The aircraft systems are ready to start refueling. refueling.

B

The refueling control panel door is not closed. closed.

C

Refueling is completed, completed, the required amount of fuel has been pumped into the tanks. tanks.

D

A reminder that you still have to refuel. refuel.

FUEL – 2803

On amber On this this ECAM ECAM FUEL FUEL SD SD page page what what does does an an amberamberboxed ? mean boxed FOB FOB indication indication mean? mean?

A

Not all the fuel on board is useable anymore. anymore.

B

The fuel temperature exceeds a limit. limit.

C

A fuel imbalance has been detected. detected.

D

A disagreement between fuel measured and fuel entered on the MCDU has been detected. detected.

FUEL – 2804

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

A

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

B

It is switched on with the Mode SEL pb in AUTO and supplying fuel

C

It is switched on with the Mode SEL pb in MAN and supplying fuel. fuel.

D

It is switched on with the Mode SEL pb in AUTO but not supplying fuel. fuel.

FUEL – 2805

This This is is your your ECAM ECAM FUEL FUEL page page after after engine engine shutdown. . You notice the transfer shutdown open shutdown. You notice the transfer valves valves are are open. open.. What are your actions to close them? ? What are your actions to close them them?

A

You have to switch the inner tank pumps off. off.

B

You have to push the MODE SEL pb sw to manual. manual.

C

You have to open and then close the crossfeed valve again. again.

D

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

FUEL – 2806

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

A

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

B

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

C

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

D

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

FUEL – 2807

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

A

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

B

During taketake-off, off, the center tank fuel is pumped to the rear to trim the aircraft. aircraft.

C

To feed the 2 engines from 2 different sources ( the inner tanks ).

FUEL – 2808

What -off? take off? What is is the the minimum minimum fuel fuel quantity quantity for for taketake-off?

A

2400 lbs. lbs.

B

3300 lbs. lbs.

C

4700 lbs. lbs.

D

5300 lbs. lbs.

FUEL – 2809

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

A

C

B

D

FUEL – 280A

You You are are in in cruise cruise and and according according to to those those indications, , a failure occurred in indications system indications, a failure occurred in the the fuel fuel system. system.. Why didn' ' t you get a master caution or a chime? ? Why didn didn't you get a master caution or a chime chime?

A

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

B

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

C

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

FUEL – 280B

In PR In case case of of R R TK TK PUMP PUMP 11 ++ 22 LO LO PR, PR,, can can you you still still use use fuel ? tank fuel out out of of the the right right inner inner tank? tank?

A

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

B

No, No, the fuel of this tank is lost. lost.

C

Yes, Yes, the fuel flows via transfer valves to the outer tank. tank.

D

Yes, Yes, the fuel flows via spill valves to the center tank. tank.

FUEL – 280C

The The normal normal pressure pressure for for the the hydraulic hydraulic system system is is 2000 2000 psi psi

A

True. True.

B

False. False.

HYD - 2900

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

A

500 psi

B

1000 psi

C

2000 psi

D

3000 psi

HYD – 2901

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

A

The ELEC pump. pump.

B

The RAT. RAT.

C

The PTU. PTU.

D

Both the GREEN and YELLOW systems. systems.

HYD – 2902

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

A

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

B

The ELEC pump has been switched off. off.

C

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

HYD – 2903

You message You get get aa YY RSVR RSVR LO LO AIR AIR PR PR message. message.. The first step of the procedure The first step of the procedure asks asks you you to to switch switch the PTU off. . Why? ? the PTU off off. Why Why?

A

Because it is faulty. faulty.

B

You want to unpressurize the BLUE system. system.

C

You want to increase the air pressure by isolating the YELLOW system. system.

D

You want to avoid the pressurization of the yellow system by the PTU after you switched the ENG 2 pump off. off.

HYD – 2904

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

A

The GREEN is supplying by BLUE system. system.

B

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

C

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

D

The YELLOW system is supplying the GREEN system. system.

HYD – 2905

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

A

B

C

HYD – 2906

What ? mean What does does an an amber amber RAT RAT indication indication mean? mean?

A

The RAT is faulty. faulty.

B

The RAT is deployed. deployed.

C

The RAT is pressurizing the BLUE system. system.

HYD – 2907

What What is is the the correct correct PTU PTU indication indication ifif itit is is delivering delivering power ? system power to to the the GREEN GREEN system? system?

A

B

C

HYD – 2908

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

A

B

C

D ICE - 3000

In In flight flight the the ECAM ECAM SD SD page page displays displays the the following following indications. ? indications means indications.. What What does does itit means? means?

A

The right wing antianti-ice valve failed to open. open.

B

The left wing antianti-ice valve failed to close. close.

C

Both wing antianti-ice valves failed to open. open.

D

Both wing antianti-ice valves failed to close. close.

ICE – 3001

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

A

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

B

When in AUTO mode, mode, the windows are heated only when necessary. necessary.

C

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

D

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

ICE – 3002

Which ? protection Which sources sources are are used used for for ice ice and and rain rain protection? protection?

A

Electrical heating. heating.

B

Hot air. air.

C

Electrical heating and warm air from the cabin. cabin.

D

Electrical heating and hot air. air.

ICE – 3003

IfIf one -ice system anti fails one engine engine antianti-ice system fails, fails,, the the second second one one takes -icing for anti engines takes over over and and provides provides antianti-icing for both both engines. engines..

A

True. True.

B

False. False.

ICE – 3004

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

A

B

C

D

ICE – 3005

In flight ON In flight, flight,, after after switching switching wing wing Anti Anti Icing Icing System System ON, ON,, the ECAM E/ / WD page displays “ WING A. . ICE SYS the ECAM E E/WD page displays “WING A A. ICE SYS FAULT” ” which FAULT means FAULT” which means. means..

A

The right wing Anti Ice failed to open. open.

B

Both wing Anti Ice failed to open. open.

C

Both wing Anti Ice failed to closed. closed.

D

The left wing Anti Ice failed to OPEN. OPEN.

ICE – 3007

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

A

Operates only in flight and is fully automatic in case of icing conditions. conditions.

B

Operates automatically after engine start, start, the pilots can have manual control through the ENG1 ENG1 and ENG2 ENG2 antianti-ice pb. pb.

C

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

D

Is controlled manually by the pilot through the ENG1 ENG1 and ENG2 ENG2 antianti-ice pb. pb.

ICE – 3008

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

A

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

B

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

C

Because of ice detection, detection, the system asks the pilot to switch the A. A.ICE system on. on.

D

At least one ENG A. A.ICE switch is in the ON position. position.

ICE – 3009

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

A

The right wing antianti-ice valve failed to open. open.

B

The left wing antianti-ice valve failed to close. close.

C

Both wing antianti-ice valves failed to open. open.

D

Both wing antianti-ice valves failed to close. close.

ICE – 300A

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

D

C

A

C

D

B EIS/ECAM – 3A00

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

D

C

A

C

D

B EIS/ECAM – 3A01

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

D

C

A

C

D

B EIS/ECAM – 3A02

Please Please indicate indicate the the ND ND 22..

A

B

C

D

EIS/ECAM – 3A03

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

A

Red. Red.

B

B

Amber. Amber.

C

Green. Green.

D

White. White.

A

C

D EIS/ECAM – 3A04

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

A

Red. Red.

B

B

Amber. Amber.

C

Green. Green.

D

White. White.

A

C

D EIS/ECAM – 3A05

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

A

Red. Red.

B

B

Amber. Amber.

C

Green. Green.

D

White. White.

A

C

D EIS/ECAM – 3A06

On page On the the ECAM ECAM SD SD page, page,, what what does does an an advisory advisory message ? mean message mean? mean?

A

The parameter is about to reach a limit. limit.

B

The parameter is out of limits. limits.

C

The parameter has a faulty indication. indication.

1.1 5.1

EIS/ECAM – 3A07

You warning You have have an an ENG ENG 11 FIRE FIRE warning. warning.. On On the the ECAM ECAM EE/WD /WD page, , what does the green arrow page page, what does the green arrow at at the the bottom ? mean bottom of of the the page page mean? mean?

A

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

B

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

C

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

EIS/ECAM – 3A08

On page On the the ECAM ECAM ENGINE ENGINE system system page, page,, you you observe observe the VIB ( N 2 ) indication. . What is the name the VIB (N2) indication indication. What is the name of of such such an an indication pulsing? ? indication pulsing pulsing?

A

Alert. Alert.

B

Warning. Warning.

C

Caution. Caution.

D

Advisory. Advisory.

1.1 5.1

EIS/ECAM – 3A09

On /WD page, E page On the the ECAM ECAM E/ E/WD page,, after after the the engine engine shutdown, , you observe a pulsing shutdown message shutdown, you observe a pulsing STS STS message. message.. What does it mean? ? What does it mean mean?

A

It is an indication that the aircraft has not yet reached the shutdown status. status.

B

It is an indication that at least one system requires crew attention. attention.

C

It is an indication that there is at least one inoperative system in the STS. STS.

D

It is an indication that an aircraft system requires maintenance attention. attention.

EIS/ECAM – 3A0A

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

A

Press and hold the corresponding button on the ECP. ECP.

B

Switch the SD to one of the ND’ ND’s.

C

Switch the SD to one of the PFD’ PFD’s.

EIS/ECAM – 3A0B

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

A

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

B

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

C

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

D

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

EIS/ECAM – 3A0C

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

A

Only ECAM cautions are lost. lost.

B

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

C

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

D

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

EIS/ECAM – 3A0D

On On the the ECAM ECAM STATUS STATUS page page ,, what what does does aa CANCELLED ? mean CANCELLED CAUTION CAUTION mean? mean?

A

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

B

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

C

The FWC is working in a degraded mode and is not able anymore to detect this failure. failure.

D

Because it was a false warning, warning, maintenance inhibited it. it.

EIS/ECAM – 3A0E

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

A

By resetting the appropriate circuit breaker. breaker.

B

By pressing and holding any CLR pb for more than 3 seconds. seconds.

C

Only maintenance can reset this function. function.

D

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

EIS/ECAM – 3A0F

The Digital Flight The location location of of the the DFDR DFDR ((Digital Flight Data Data Recorder) ) is Recorder Recorder) is ::

A

Inside the Cockpit. Cockpit.

B

Installed in the tail Section of the aircraft, aircraft, and the data is stored on a tape Contained in fire and shock proof box. box.

C

In the passenger Cabin for protection reason. reason.

EIS/ECAM – 3A0H

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

A

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

B

The DFDR is energized during the first 5 minutes after the aircraft electric network is energized and then after the first engine start. start.

C

The DFDR will be energized at lift off. off.

EIS/ECAM – 3A0I

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

A

Aircraft lighting is selected OFF. OFF.

B

On landing. landing.

C

After first engine start. start.

D

When both engines are started. started.

EIS/ECAM – 3A0J

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

A

False. False.

B

True. True.

EIS/ECAM – 3A0L

When occurs When aa DFDR DFDR fault fault occurs, occurs,, itit will will be be signaled signaled by by ::

A

A fault light illuminating amber on overhead panel. panel.

B

An ECAM caution message. message.

C

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

D

A MAINTENANCE message in the status page. page.

EIS/ECAM – 3A0M

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

200

A

150 kt. kt.

180 F

B C

160 kt. kt.

160 140

169 kt. kt.

120

D

185 kt. kt.

EIS/EFIS – 3B00

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

250

220

A

180 kt. kt.

200 S

B

191 kt. kt.

C

215 kt. kt.

180 160 140

D

250 kt. kt.

EIS/EFIS – 3B01

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

200

A

140 kt. kt.

B

155 kt. kt.

C

180 = 160

F

140 175 kt. kt.

120

D

185 kt. kt.

EIS/EFIS – 3B02

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

A

It marks the landing elevation. elevation.

B

It marks the selected altitude. altitude.

C

It marks the preselected altitude. altitude.

FL 70 7000

30.08 STD

D

It marks the decision height. height.

QNH

EIS/EFIS – 3B03

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

A

80 ft/ ft/min in climb. climb.

B

800 ft/ ft/min in descent. descent.

C

80 ft/ ft/min in descent. descent.

FL 70 7000

30.08 STD

D

QNH

800 ft/ ft/min in climb. climb.

EIS/EFIS – 3B04

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

A

069. 069.

B

080. 080.

C

084. 084.

EIS/EFIS – 3B05

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

A

069. 069.

B

080. 080.

C

084. 084.

EIS/EFIS – 3B06

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

A

069. 069.

B

080. 080.

C

084. 084.

EIS/EFIS – 3B07

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

A

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

B

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

C

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

D

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

EIS/EFIS – 3B08

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

A

The heading to the next waypoint PAS is 108, 108, it is at 28 NM, NM, time left to the waypoint is 9 minutes and 8 seconds. seconds.

B

The heading to the next waypoint PAS is 108, 108, it is at 28 NM, NM, time to the destination is 9 hours and 8 minutes. minutes.

C

The track to the next waypoint PAS is 108, 108, it is at 28 NM, NM, elapsed time of this flight is 9 minutes and 8 seconds. seconds.

D

The track to the next waypoint PAS is 108, 108, it is at 28 NM, NM, it will be overflown at 9:08. 08.

EIS/EFIS – 3B09

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

A

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

280

B

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

C

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

D

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

260 240 = 220 o EIS/EFIS – 3B0L

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

A

The ECON speed range during managed descent. descent.

360

B

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

C

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

340 320 300

D

The lower magenta symbol represents VLS. VLS.

.636 EIS/EFIS – 3B0O

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

A

No, No, it is not possible because each airline has its own configuration. configuration.

B

Yes, Yes, by rotating the outer scale of baro reference selector on the EFIS panel. panel.

1020

C

No, No, the crew should refer to a conversion table. table.

D

Yes, Yes, but only the Captain side is equipped with this conversion. conversion.

1020

EIS/EFIS – 3B0R

On column On the the PFD PFD altitude altitude column, column,, which which statement statement is is correct? ? correct correct?

A

V/S 80 FPM, FPM, aircraft passing altitude 5780’ 5780’.

B

V/S 800 FPM, FPM, red ribbon represents the height above the surface. surface.

C

V/S 8000 FPM, FPM, aircraft passing altitude 5780’ 5780’.

FL 70 7000 30.08 STD

D

The blue line represents the MDA selected by the crew on the MCDU. MCDU.

QNH

EIS/EFIS – 3B0S

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

A

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

B

Crew is pushing the baro reference selector to change from local QNH to the STD setting. setting.

STD

C

The rate of descent is 240 FPM. FPM.

FL 70 STD

D

Aircraft passing altitude is 8500 ft. ft.

EIS/EFIS – 3B0T

With /compass scale HDG With regard regard to to the the HDG/ HDG/compass scale on on the the bottom : PFD bottom line line of of the the PFD: PFD:

A

The present mag. mag. track is 080. 080.

B

The present heading is 080 (since (since there is no drift). drift).

C

The selected heading is 086 and the track is 080. 080.

D

The target selected heading is 080° 080°. Present mag. mag. HDG is 086° 086°. Present mag. mag. track is 086° 086°.

---

080

17000

EIS/EFIS – 3B0U

On /WD, E WD, how On this this E/ E/WD, how do do you you interpret interpret the the NW NW STRG STRG DISC ? memo DISC memo? memo?

A

The nose wheel steering has been disconnected by ground personnel. personnel.

B

A failure in the nose wheel steering system has been detected. detected.

C

One of the pilots has pushed the PEDALS DISC pushbutton located on the steering handwheel. handwheel.

D

The nose wheel steering computer has finished it’ it’s self test. test. Nose wheel steering is now available. available.

PARK BRK NW STRG DISC

L/G BRK - 3200

During ° 22 is back nn° started During push push back, back,, engine engine n° is started. started.. On On memo memo page page this this action action induces induces the the NW NW TRG TRG DISC DISC indication. : For indication amber indication.. ECAM ECAM changing changing to to amber: amber: For which which reason? ? reason reason?

NW STRG DISC

A

The NW STRG disconnect mechanism has failed. failed.

B

The yellow hydraulic system has build up pressure which might damage the NW STRG system when set to towing position. position.

C

The nose wheel steering has been rereconnected by ground personnel. personnel. The amber indication will disappear as soon as you start taxi. taxi.

D

The nose wheel steering is still disconnected. disconnected. The memo has become amber because one engine is running. running.

L/G BRK – 3201

Push completed taxi Push back back is is completed. completed.. Before Before starting starting to to taxi, taxi,, you you check /WD page. E page check the the ECAM ECAM E/ E/WD page.. Which Which indications indications confirm confirm that that you you can can start start to to taxi taxi immediately? ? immediately immediately?

A

B

L/G BRK – 3202

After check After starting starting to to taxi taxi you you perform perform the the brake brake check. check.. While While pressing pressing on on top top of of the the rudder rudder pedals pedals you you feel feel the airplane decelerating but the BRAKES pressure the airplane decelerating but the BRAKES pressure indication indication remains remains 00.. Which statement Which statement is is true true ??

A

The BRAKES pressure indicator has failed. failed.

B

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

C

You must perform the check again and press harder on the brakes until you get an indication. indication.

D

The indication is normal because with manual braking you are not able to apply enough pressure to be displayed on the BRAKES indicator. indicator.

L/G BRK – 3203

Aircraft Aircraft has has to to land land on on aa wet wet runway runway .. According to these indications; ; the /BRAKE is AUTO According to these indications indications; the AUTO/ AUTO/BRAKE is active. . active active.

A

True. True.

B

False. False.

GW

L/G BRK – 3204

On page On the the ECAM ECAM SD SD WHEEL WHEEL page, page,, the the 22 triangles triangles appearing : mean appearing below below each each landing landing gear gear mean: mean:

A

Each triangle represents one tire. tire.

B

There are two computers providing information on the gear position. position. Each triangle represents the position detected by its associated computer. computer.

C

Each triangle represents one braking system (normal/ normal/alternate) alternate) available for the associated gear. gear. GW

D

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

L/G BRK – 3205

You /G selector LL/G You have have just just set set the the L/ selector to to the the DOWN DOWN position. ... position indications position.. According According to to these these indications... indications...

A

The L/ L/G is locked. locked. The L/ L/G doors are open. open.

B

The computers providing gear position information have failed. failed.

C

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

D

The L/ L/G control system has failed. failed. The gear will not extend. extend.

L/G BRK – 3206

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

A

The nose gear is in transit. transit.

B

All gears are down and locked. locked.

C

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

D

The nose gear is down and locked. locked. The nose gear doors are open. open.

GW

L/G BRK – 3207

How How do do you you interpret interpret aa green green arc arc appearing appearing over over one ? indication one wheel wheel indication? indication?

A

It marks the hottest brake with a temperature of more than 100 º Celsius. Celsius.

B

It indicates an abnormal high temperature. temperature.

C

The ANTI/ ANTI/SKID system is automatically releasing the pressure of that brake. brake. GW

D

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

L/G BRK – 3208

The actions The pilot pilot flying flying asks asks you you to to perform perform ECAM ECAM actions. actions.. What are your actions according to the first What are your actions according to the first line line of of the ECAM procedure ? the ECAM procedure ?

A

I must put the L/ L/G selector to the UP position. position.

B

The system is trying to recycle the gear automatically. automatically. I must wait until the first line disappears. disappears.

C

I must put the L/ L/G selector to the UP position and immediately to the DOWN position again. again.

D

I must put the L/ L/G selector to the UP position, position, wait until the gear has retracted, retracted, and then to the DOWN position again. again.

L/G CTL

GW

L/G BRK – 3209

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

A

According to the procedure L/ L/G GRAVITY EXTENSION which is found in the Quick Reference Hand book (QRH). QRH).

B

Recycle the L/ L/G a second time. time. This time the gear will free fall automatically. automatically.

C

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

D

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

L/G CTL

GW

L/G BRK – 320A

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

A

The gear is in the downlock position. position.

B

The gear is down but not locked. locked.

C

After GRAVITY EXTENSION the gear indications on the ECAM WHEEL page are not reliable. reliable.

GW

L/G BRK – 320B

You /BRK selected AUTO You perform perform aa landing landing with with AUTO/ AUTO/BRK selected to to MED. MED MED.. After After touch touch down down you you observe observe the the following following indications. indications indications.. At moment At this this moment, moment,, which which statement statement is is true true ??

A

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

B

The ANTI/ ANTI/SKID system is releasing brake pressure for wheels 2 and 4.

C

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

D

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

L/G BRK – 320C

You ON You have have just just set set the the parking parking brake brake handle handle to to ON. ON.. Which indication CONFIRMS that the parking brake Which indication CONFIRMS that the parking brake is is actually actually set set ??

A

B

PARK PARK BRK BRK

L/G BRK – 320D

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

A

Landing light. light.

B

RWY turnoff light. light.

C

T/O light. light.

D

Taxi light. light.

LIGHTS - 3300

Where ? panel Where is is the the location location of of the the exterior exterior light light panel? panel?

A

B

C LIGHTS - 3301

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

A

B

C LIGHTS - 3302

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

A

When the aircraft touches down. down.

B

When the first reverser is opened. opened.

C

When the landing lights are switched off. off.

D

When the last engine has been shut down. down.

LIGHTS - 3303

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

A

STROBE, STROBE, BEACON, BEACON, NAV, NAV, LAND, LAND, T.O. and RWY TURN OFF lights. lights.

B

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

C

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

D

STROBE, STROBE, BEACON, BEACON, NAV and LAND lights. lights.

LIGHTS - 3304

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

A B C NAV - 3400

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

A

PPOS. PPOS.

B

HDG. HDG.

ALIGN

C

STS. STS.

D

TEST. TEST.

ALIGN

ALIGN

NAV - 3401

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

A

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

B

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

C

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

D

It is an indication that the time to the next waypoint is 10 minutes. minutes.

ALIGN

ALIGN

ALIGN

NAV - 3402

An selected An ILS ILS approach approach is is selected. selected.. Please Please indicate indicate the the displays displays with with information information about about ILS ILS 22..

A

PFD 1 and ND 1.

B

PFD 2 and ND 2.

C

PFD 1 and ND 2.

D

PFD 2 and ND 1.

NAV - 3403

Is Is itit possible possible to to get get information information about about ILS ILS 22 on on the the CAPT ? side CAPT side? side?

A

Yes, Yes, on the PFD 1.

B

Yes, Yes, on the ND 1.

C

No, No, it is not possible. possible.

NAV - 3404

Which -aids are ? Nav DDRMI Which NavNav-aids are displayed displayed on on the the DDRMI? DDRMI?

A

VOR 1 and VOR 2.

B

ADF 1 and ADF 2.

C

VOR 1 and ADF 2.

D

VOR 2 and ADF 1.

NAV - 3405

Please panel Please indicate indicate the the location location of of the the GPWS GPWS panel. panel..

C

B D

A NAV - 3406

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

C

B D

A NAV - 3407

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

A

B NAV - 3409

On ND On the the ND. ND.. What ? mean What does does the the MAN MAN indication indication mean? mean?

A

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

B

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

C

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

NAV – 340A

According According to to this this ND ND display display please please select select the the present WX RADAR mode, , on the WX present WX RADAR mode mode, on the WX RADAR RADAR control panel control panel. panel..

A

WX. WX.

B

WX/ WX/TURB. TURB.

C

MAP. MAP.

NAV – 340C

According According to to this this ND ND display display please please select select the the present WX RADAR mode, , on the WX present WX RADAR mode mode, on the WX RADAR RADAR control panel control panel. panel..

A

WX. WX.

B

WX/ WX/TURB. TURB.

C

MAP. MAP.

NAV – 340D

On panel On the the GNADIRS GNADIRS control control panel, panel,, during during the the IRS IRS alignment, , the ALIGN lights start flashing. alignment alignment, the ALIGN lights start flashing flashing.. What ? wrong What is is wrong? wrong?

A

System discovered a discrepancy between the position in the database and the position entered on the MCDU. MCDU.

B

At least one of the IR lost the NAV capability. capability.

C

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

D

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

NAV – 340E

Between Between the the ND ND and and MCDU MCDU you you are are performing performing aa NAV ? check you NAV ACCUR ACCUR check. check.. Does Does itit satisfy satisfy you? you?

A

Yes, Yes, raw data and FMGS position are the same or the difference is within acceptable limits. limits.

B

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

C

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

NAV – 340F

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

A

C

D

B

NAV – 340G

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

A

D

B

C OXY - 3500

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

B

A

C

OXY - 3501

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

A

B

C OXY - 3502

After deployment After aa cabin cabin mask mask deployment, deployment,, what what is is their their effective ? use activated effective time time of of use, use,, once once activated? activated?

A

21 minutes. minutes.

B

37 minutes. minutes.

C

13 minutes. minutes.

D

5 minutes. minutes.

OXY - 3503

On Panel On the the crew crew OXYGEN OXYGEN MASK MASK Regulator Regulator Panel, Panel,, which which statement best reflects the function of the /100% N statement best reflects the function of the N/ N/100% supply ? selector supply selector? selector?

A

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

B

The N position provides an air/ air/oxygen mixture, mixture, 100% delivers pure oxygen. oxygen.

C

N position cuts the oxygen supply, supply, 100% position enables normal oxygen supply. supply.

D

The N/ N/100% selector is to be used during the preflight check to check the oxygen supply to the mask. mask.

OXY - 3504

A

The operative The cockpit cockpit CREW CREW OXYGEN OXYGEN being being operative, operative,, which pb has to be pressed to switch the which pb has to be pressed to switch the system system OFF? ? OFF OFF?

B

C

D OXY - 3506

After OFF After switching switching the the cockpit cockpit CREW CREW OXYGEN OXYGEN OFF, OFF,, which ? see which ECAM ECAM indication indication would would you you see? see?

A

B

C

D OXY - 3507

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

C

A

B PNEU - 3600

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

A

True. True.

B

False. False.

PNEU - 3601

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

A

The engines are running and supplying bleed air. air.

B

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

C

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

D

The engines are not running, running, a GND HP air unit is supplying bleed air. air.

PNEU - 3602

After After starting starting both both engines engines and and according according to to those those AIR COND panel and ECAM BLEED page AIR COND panel and ECAM BLEED page indications, (s) provide ? indications source air indications,, which which source( source(s) provide the the bleed bleed air? air?

A

The engines. engines.

B

The APU. APU.

C

The engines and the APU together. together.

PNEU - 3603

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

A

At or close to taketake-off power. power.

B

The engines are not running. running.

C

At or slightly above idle power. power.

PNEU - 3604

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

A

The APU supplies both sides of the system. system.

B

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

C

The APU supplies left side and engine 2 the right side of the system. system.

D

There will be no bleed air supplied. supplied.

PNEU - 3605

The ON The APU APU BLEED BLEED pb pb has has just just been been switched switched ON. ON.. On the ECAM BLEED page what do the On the ECAM BLEED page what do the related related indications ? mean indications mean? mean?

A

The X BLEED valve has failed to open. open.

B

The X BLEED valve has failed to close. close.

C

The X BLEED valve is in transit. transit.

D

The X BLEED valve is open. open.

PNEU - 3606

Following /WD fault E Following an an ENG ENG 11 BLEED BLEED fault, fault,, the the ECAM ECAM E/ E/WD procedure ; on applied procedure has has been been applied; applied; on the the ECAM ECAM status status page page how how do do we we interpret interpret the the STATUS STATUS information information message ? green message in in green? green?

A

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

B

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

C

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

PNEU - 3607

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

A

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

B

No, No, the crew should select X bleed valve selector to (shut) shut) position to close the valve manually after one engine is started. started.

C

No, No, IP HP valves should be closed. closed.

D

Yes, Yes, all the indications are correct, correct, HP valves open because of high air demand with engine at low RPM. RPM.

PNEU – 360A

An An ENG ENG indicated indicated message. message message..

11 BLEED BLEED fault fault has has occurred occurred by the related /WD E by the related ECAM ECAM E/ E/WD

and and is is failure failure

A

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

B

The left hand Bleed can’ can’t be recovered. recovered.

C

APU bleed can never supply the left side. side.

PNEU – 360C

The running The APU APU is is still still running, running,, itit is is in in the the 22 min min cool cool down down period period because because you you have have just just finished finished using using the the APU air APU bleed bleed air. air.. You notice you indications You notice you still still have have APU APU AVAIL AVAIL indications. indications.. What is the reason for that ? What is the reason for that ?

A

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

B

The APU is still running. running. It is in the 2 min cool down period because you have used APU bleed before. before.

C

The APU is still running because it always needs a 2 min cool down period after the APU MASTER SW has been switched off. off.

D

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

APU - 4900

After off After the the engines engines have have been been switched switched off, off,, you you realize available realize that that there there is is no no external external power power available. available.. According According to to the the indications indications can can you you still still interrupt interrupt the ? sequence the APU APU shut shut down down sequence? sequence?

A

No, No, I have to wait until the APU AIR INLET FLAP is fully closed and then start the APU again. again.

B

Yes, Yes, I simply push the APU MASTER SW back to ON. ON.

C

Yes, Yes, I simply push the APU START switch to ON. ON.

D

No, No, I have to wait until the AVAIL indications disappear and then start the APU again. again.

APU - 4901

Which Which ECAM ECAM APU APU page page corresponds corresponds to to these these indications indications on on the the overhead overhead panel panel ??

A

B

C

APU - 4902

You APU You are are attempting attempting to to start start the the APU. APU.. After After 20 20 seconds seconds you you get get the the following following indications indications that ’t get didn start that you you didn’ didn’t get during during the the last last APU APU start. start.. Can ? start Can you you continue continue the the APU APU start? start?

A

No. No. A low oil level has been detected and any start attempt will damage the APU. APU.

B

Yes, Yes, you simple have to wait 20 sec until the LOW OIL LEVEL advisory disappears and then go ahead with the APU start. start.

C

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

D

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

APU - 4903

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

APU APU APU APU

A

The APU will still run for 2 minute cooling period and then shutdown. shutdown.

B

The APU will shutdown right away. away.

C

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

D

Nothing happen because air conditioning is selected on. on.

APU - 4904

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

A

15 000 ft

B

39 000 ft

C

20 000 ft

APU - 4905

What What is is the the maximum maximum altitude altitude the the APU APU may may be be used used for for bleed bleed air air supply supply with with 11 pack pack operating operating ??

ALTITUDE ALTITUDE (Ft) (Ft) 39 39 000 000

25 25 000 000

A

15 000 ft

B

20 000 ft

C

25 000 ft

D

39 000 ft

20 20 000 000 15 15 000 000

?

APU - 4906

According According to to the the ECAM ECAM APU APU page page indications indications ::

A

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

B

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

C

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

D

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

APU - 4907

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

A

An APU AUTO SHUT DOWN will occur because of APU failure to reach 90%

B

You have to abort the start by pushing the APU MASTER SW to off. off.

C

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

D

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

APU - 4908

You You are are performing performing the the walk walk around around with with the the APU APU running and nobody is in the cockpit. . running and nobody is in the cockpit cockpit. What ? FIRE What will will happen happen in in case case of of an an APU APU FIRE? FIRE?

A

An APU EMER shut down will occur and the APU fire bottle will be discharged automatically. automatically.

B

You have to perform the ECAM actions to shut down the APU and extinguish the fire from the cockpit. cockpit.

C

An APU AUTO shut down will occur but you have to discharge the APU fire bottle from the cockpit manually. manually.

D

An EMER AUTO shut down will occur but you have to discharge the APU fire bottle manually either from the cockpit or by pushing the APU SHUT DOWN switch on the external power panel. panel.

APU - 4909

During During external external walk walk around around in in the the APU APU area area the the checking of APU Fire extinguisher overpressure checking of APU Fire extinguisher overpressure indication red disc) ) in disc indication ((red disc) in place place means means ::

A

Indication is correct for normal operation. operation.

B

Indication is not correct and you call the maintenance. maintenance.

C

Is abnormal because it should be a green disc. disc.

D

Is only visible with either APU started on AC GROUND POWER connected. connected.

APU – 490A

During around During walk walk around, around,, status status of of APU APU Fire Fire extinguisher extinguisher overpressure red disc) ) is disc overpressure indication indication ((red disc) is made made by by

A

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

B

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

C

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

D

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

APU – 490B

To : system select To use use the the APU APU bleed bleed system, system,, the the crew crew will will select: select:

A

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

B

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

C

The ENG1 ENG1 and ENG2 ENG2 BLEED pbs. pbs.

D

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

APU – 490C

The The APU APU provides provides

A

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

B

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

C

Electric Power for electric system on ground and in flight. flight.

D

B and C. C.

APU – 490D

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

A

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

B

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

C

Available as soon as engines are shut down. down.

D

Available when APU is running, running, APU GEN is ON and EXT PWR is not ON. ON.

APU – 490E

The The APU APU can can be be started started using using

A

Aircraft batteries. batteries.

B

Power from aircraft DC busses. busses.

C

Ground external power source. source.

D

Any of the above. above.

APU – 490F

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

C

B

B

A DOORS - 5200

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

A

The door is fully open. open.

B

The door is fully closed. closed.

C

The door is unlocked. unlocked.

D

The door is inoperative. inoperative.

DOORS - 5201

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

A

True. True.

B

False. False.

DOORS - 5202

You -back on push You are are ready ready for for pushpush-back on the the ECAM ECAM SD SD DOOR/ / OXY page. . What should the DOOR DOOR DOOR/OXY page page. What should the DOOR Page Page look look like ? now like now? now?

A

B

C

D

DOORS - 5203

You gate You have have reached reached the the gate. gate.. Somebody Somebody is is about about to to open the left forward door from the outside. open the left forward door from the outside outside.. What What will ? case will happen happen in in this this case? case?

A

The slide will be deployed. deployed.

B

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

C

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

DOORS - 5204

On /OXY page DOOR On the the ECAM ECAM SD SD DOOR/ DOOR/OXY page this this indication indication means. means means..

A

Overwing exits and right rear door slides are armed, armed, left forward cabin door and forward cargo door indicate a malfunction. malfunction.

B

The left forward cabin door and the forward cargo door are unlocked, unlocked, the overwing exits and the right rear door slides are armed. armed.

C

The left forward cabin door and the forward cargo door are unlocked, unlocked, the overwing exits and the right rear door slides are not armed. armed.

D

Overwing exits and right rear door slides are not armed, armed, left forward cabin door and forward cargo door indicating a malfunction. malfunction.

DOORS - 5205

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

A

FULL. FULL.

B

CLIMB and FLEX/ FLEX/MCT. MCT.

C

CLIMB and TO/ TO/GA. GA.

D

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

ENG - 7000

You -off. ’t have take off. You don You are are about about to to perform perform aa taketake-off. You don’ don’t have inserted a FLEX temperature. . inserted a FLEX temperature temperature. Which -off? take off? Which thrust thrust lever lever detent detent shall shall be be used used for for taketake-off?

A

FULL. FULL.

B

CLIMB. CLIMB.

C

FLEX/ FLEX/MCT. MCT.

D

TO/ TO/GA. GA.

ENG - 7001

During During the the automatic automatic start start sequence sequence of of ENG ENG 22,, you you notice that only igniter B is powered. . notice that only igniter B is powered powered. Is ? normal Is this this normal? normal?

A

No, No, normally igniter A is used for the engine start. start.

B

No, No, normally both igniters are used for engine start. start.

C

Yes, Yes, igniter B is always used for the engine start. start.

D

Yes, Yes, igniters are used alternatively for engine start, start, in this case B. B.

ENG - 7002

You -off with take You are are performing performing aa taketake-off with the the thrust thrust levers levers in /THR now ? position A active in the the FLEX FLEX position. position.. Is Is A/ A/THR now active? active?

A

Yes. Yes.

B

No. No.

ENG - 7003

You You are are performing performing aa take take off off with with thrust thrust levers levers in in FLEX /THR become ? position A active FLEX position. position.. When When does does A/ A/THR become active? active?

A

As soon as the thrust levers are pulled back into the CLIMB position. position.

B

As soon as you pass the thrust reduction altitude. altitude.

C

As soon as you engage the autopilot. autopilot.

D

As soon as you push the A/ A/THR pb manually on. on.

ENG - 7004

You -off with take power You are are performing performing aa taketake-off with TOGA TOGA power. power.. When /THR become ? A active When does does the the A/ A/THR become active? active?

A

As soon as the thrust levers are pulled back into the FLEX position. position.

B

As soon as you push the A/ A/THR pb manually on. on.

C

As soon as you engage the autopilot. autopilot.

D

As soon as the thrust levers are pulled back into the CLIMB position. position.

ENG - 7005

What ? mean What does does an an amber amber REV REV indication indication mean? mean?

A

The reversers are faulty. faulty.

B

The reversers are fully deployed. deployed.

C

The reversers are stuck. stuck.

D

The reversers are unlocked. unlocked.

ENG - 7006

On /WD, E WD, with On the the ECAM ECAM E/ E/WD, with thrust thrust levers levers reverser reverser to to reverse position. . What does a green REV reverse position position. What does a green REV indication indication mean? ? mean mean?

A

The reversers are faulty. faulty.

B

The reversers are fully deployed. deployed.

C

The reversers are stuck. stuck.

D

The reversers are unlocked. unlocked.

ENG - 7007

Before Before engine engine starting starting the the Eng Eng FADEC FADEC should should be be energized: : which control do you activate energized energized: which control do you activate in in order order to to energize ? start energize the the FADEC FADEC prior prior to to engine engine start? start?

A

B

C

D ENG - 7008

During During the the manual manual start start sequence sequence of of ENG ENG 22,, you you notice that both igniters are powered. . notice that both igniters are powered powered. Is ? normal Is this this normal? normal?

A

No, No, normally igniter A is used for the engine start. start.

B

Yes, Yes, for manual start both igniters are always used. used.

C

No, No, normally igniter B is used for the engine start. start.

D

Yes, Yes, both igniters are used for every start. start.

ENG - 7009

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

A

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

B

It indicates an engine failure. failure.

C

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

ENG – 700A

On /WD page, E page On the the ECAM ECAM E/ E/WD page,, what what is is the the meaning meaning of of the ? indication the amber amber CHK CHK indication? indication?

A B

It is an indication that the EGT of ENG 1 is out of the normal range. range.

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

C H K

ENG 1 EGT DISCREPANCY

C

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

D

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

ENG – 700B

You procedure You are are in in the the middle middle of of the the engine engine start start procedure. procedure.. Is ? start Is this this an an automatic automatic start start or or aa manual manual start? start?

A

Automatic. Automatic.

B

Manual. Manual.

ENG – 700C

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

A

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

B

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

C

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

ENG – 700D

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

A

Ignition start. start.

B

Ignition cutcut-out. out.

C

Fuel flow start. start.

D

Starter engagement. engagement.

ENG – 700E

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

A

Starter valve closure. closure.

B

Starter valve engagement. engagement.

C

Fuel flow start. start.

D

Ignition start. start.

ENG – 700F