With With only only aa few few passengers passengers on on the the aircraft, aircraft, the the pack pack flow flow control control selector selector should should be be set set to to LO: LO:
To decrease the BLEED AIR demand from the engines and therefore to save fuel.
To decrease the BLEED AIR demand from the APU.
To decrease the cabin temperature.
To decrease the HOT AIR demand from the engine bleeds.
Have COND” ALTN COND” page Have aa look look at at the the ECAM ECAM ““COND” page :: ““ALTN MODE” ” is MODE MODE” is displayed. displayed. What What happened? happened?
Channel 1 of ZONE CONTROLLER has failed and the pilot has closed the HOT AIR and TRIM AIR valves.
Channel 1 of ZONE CONTROLLER has failed and channel 2 has taken over, thus the HOT AIR and TRIM AIR valves have closed automatically.
Temperature regulation is completely lost.
Looking Looking at at the the ECAM ECAM BLEED BLEED page page and and AIR AIR COND COND overhead overhead panel, panel, what what can can be be concluded? concluded?
The RAM AIR inlet has been opened.
On the ECAM SD, the RAM AIR inlet valve should be amber if it is fully open in flight.
Aircraft is depressurized, but after the RAM AIR valve opens at least one pack should be pressurized again.
Aircraft is depressurized, but the X BLEED valve should be open since both engines are running.
During During taxi, taxi, with with aa full full load load of of passengers passengers and and in in aa high high temperature temperature area, area, how how should should the the pack pack flow flow be set? be set?
To LO, in order to minimize the amount of hot air sent to the cabin zones.
To NORM, as the system is fully automatic apart from temperature settings.
To HI, in order to help reduce the cabin temperature.
To HI and cockpit TEMP SELECTOR to HOT in order to have maximum cooling air to the cabin.
In In the the AIR AIR COND COND system system what what is is the the function function of of the the TRIM TRIM AIR AIR valve? valve?
To optimize the zone temperature by adding cold air.
To optimize the zone temperature by adding hot air.
To regulate the hot air pressure.
To regulate the pack outlet pressure to each zone.
For For the the Normal Normal Operation Operation of of the the CARGO CARGO COND COND SYSTEM SYSTEM ::
The pilot ensures that there are no lights illuminated on the pb sw and that the temperature is set as required.
The system display will be found on the ECAM BLEED page.
The pilot has no control of the system temperature.
The system display will be found on the ECAM PRESS page.
Forward Cargo Ventilation Controller
Aft Cargo Ventilation Controller
Which Which of of the the following following statements statements is is correct? correct?
Crew should SWITCH OFF both packs just before engines start.
Crew should SWITCH OFF both engine bleed valves just before engine start.
During engine start, all the current indications on ECAM BLEED page and COND overhead panel are correct.
Crew should select X bleed valve selector to SHUT position to pressurize the left side first.
Both Both engines engines are are running running and and the the APU APU bleed bleed has has been been switched switched OFF. OFF. Which Which statement statement is is correct? correct?
The X BLEED should have remained open.
All the indications are correct.
The crew should set X BLEED valve selector to SHUT position.
The ENGINE H.P valve must be closed with the engine at idle power.
IfIf the the PACK PACK FLOW FLOW CONTROL CONTROL valves valves close, close, what what will will be be the the subsequent subsequent position position of of the the TRIM TRIM AIR AIR valves and the HOT AIR valve? valves and the HOT AIR valve? Hot HotAir Air Valve Valve
- The TRIM AIR valves remain open. - The HOT AIR valve closes.
HOT AIR Mixing Unit
- The TRIM AIR valves remain open. - The HOT AIR valve remains open.
- The TRIM AIR valves close. - The HOT AIR valve remains open
- The TRIM AIR valves close. - The HOT AIR valve closes.
Pack 1
Pack 2
Hot Bleed Air
Have COND” COND” page. Have aa look look at at the the ECAM ECAM ““COND” page. Why Why are are two two different different temperature temperature values values displayed displayed for for each each zone zone of of the the aircraft? aircraft?
The lower value is the pack outlet temperature. The upper value is the actual zone temperature monitored by the zone control temperature.
The lower value is the temperature of the air controlled by the HOT AIR valve. The upper value is the pack outlet air temperature. The lower value is the temperature of the air entering a zone (DUCT INLET temperature). The upper value is the actual zone temperature monitored by the zone control computer. The lower value is the actual zone temperature. The upper value is the selected zone temperature.
What What is is the the function function of of the the CABIN CABIN AIR AIR FANS? FANS?
HOT AIR
Extracting air from the AVIONICS BAY. Mixing Unit
Reducing the BLEED AIR requirement and therefore saving fuel.
Accelerating pressurization.
the
cabin
zones
Accelerating the removal of cabin smoke.
Cabin Cabin Fan Fan
Pack 1
Pack 2
Cabin Cabin Fan Fan
In In the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system, the the function function of of the the safety safety valves valves is... is...
To provide backup pressure if the cabin pressure controllers should fail.
Monitor the function of the outflow valve.
Protect against excessive cabin altitude.
Protect against excessive differential pressure.
On On the the CABIN CABIN PRESS PRESS panel panel with with aa LDG LDG ELEV ELEV set set manually, manually, is is there there still still an an automatic automatic control control of of the the cabin altitude? cabin altitude?
No, in this case the cabin altitude has to be controlled through the MAN V/S CTL.
Yes, SYS1 is still controlling the cabin altitude through the outflow valve.
Yes, SYS1 is still controlling the cabin altitude through the safety valve. valve.
No, in this case the cabin altitude has to be controlled through the LDG ELEV selector.
In In the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system, what what is is the the maximum maximum allowable allowable differential differential pressure? pressure?
5.3 psi
6.9 psi
??
7.6 psi
8.6 psi
Regarding Regarding the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system, what what should should the the differential differential pressure pressure be be on on the the ground, while at the gate? ground, while at the gate?
0 psi
0.5 psi
1.0 psi
8.6 psi
On On the the CABIN CABIN PRESSURIZATION PRESSURIZATION system, system, safety …. valves safety valves… valves….
the the
Are controlled with the MAN V/S CTL.
Are controlled with the MODE SEL pb. pb.
Are controlled with the DITCHING pb. pb.
Can not be controlled manually and are fully automatic.
On On the the CABIN CABIN PRESS PRESS panel, panel, the the LDG LDG ELEV ELEV has has been been set set manually. manually. What What is is the the approximate approximate value value ??
6 ft.
60 ft.
600 ft.
6000 ft.
On 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
The outflow valve.
The air intake valve.
The air outlet valve.
The safety valve.
On On the the ECAM ECAM STATUS STATUS page, page, as as you you can can see see cabin cabin pressure pressure control control is is manual. manual. You You want want descend descend from from FL 390 to FL 330. What is your target CABIN ATL? FL 390 to FL 330. What is your target CABIN ATL?
0 ft.
5000 ft.
5900 ft.
6500 ft.
On On the the CABIN CABIN PRESS PRESS panel, panel, with with the the MODE MODE SEL SEL set set to to MAN MAN and and the the MAN MAN V/S V/S CTL CTL held held in in the the DN DN position, position, the the outflow outflow valve... valve...
Opens, the cabin altitude raises.
Opens, the cabin altitude drops.
Closes, the cabin altitude raises.
Closes, the cabin altitude drops.
What What ventilation ventilation configuration configuration is is displayed displayed on on the the CAB CAB PRESS PRESS page? page?
Open configuration (a/c on ground).
Closed configuration (a/c in flight).
Intermediate configuration (a/c in flight, high skin temperature).
What What ventilation ventilation configuration configuration is is displayed displayed on on the the CAB CAB PRESS PRESS page? page?
Open configuration (a/c on ground).
Closed configuration (a/c in flight).
Intermediate configuration (a/c in flight, high temperature).
Please Please indicate indicate the the position position of of the the VENTILATION VENTILATION panel. panel.
Please Please indicate indicate the the ECAM ECAM E/WD E/WD screen. screen.
On On the the ECAM ECAM E/WD E/WD page, page, after after the the engine engine shutdown, shutdown, you you observe observe aa pulsing pulsing STS STS message. message. What does it mean? What does it mean?
It is an indication that the aircraft has not yet reached the shutdown status.
It is an indication that at least one system requires crew attention.
It is an indication that there is at least one inoperative system in the STS.
It is an indication that an aircraft system requires maintenance attention.
The The upper upper ECAM ECAM DU DU failed. failed. To To see see the the different different system system pages pages on on the the lower lower DU, DU, you you have have to: to:
Press and hold the corresponding button on the ECP.
Switch the SD to one of the ND’ ND’s.
Switch the SD to one of the PFD’ PFD’s.
Both Both ECAM ECAM screens screens failed. failed. What What happens happens to to the the E/WD E/WD indication? indication?
The E/WD is automatically transferred to one of the ND’ ND’s.
The E/WD is automatically transferred to one of the PFD’ PFD’s.
To get E/WD information, it must be manually transferred to one of the ND’ ND’s.
To get E/WD information, it must be manually transferred to one of the PFD’ PFD’s.
On On the the ECAM ECAM SYSTEM SYSTEM in in case case of of aa double double FWC FWC failure... failure...
Only ECAM cautions are lost.
ECAM cautions and warnings and aural warnings are lost.
MASTER CAUTION light, MASTER WARNING light and aural warnings are lost.
MASTER CAUTION light, MASTER WARNING light, aural warnings and ECAM cautions and warnings are lost.
On On the the ECAM ECAM STATUS STATUS page page ,, what what does does aa CANCELLED CANCELLED CAUTION CAUTION mean? mean?
The failure message has been previously cancelled with the EMER CANC pb. pb.
The failure message had occurred during the previous flight.
The FWC is working in a degraded mode and is not able anymore to detect this failure.
Because it was a false warning, maintenance inhibited it.
On On the the ECAM ECAM STATUS STATUS page, page, how how can can you you remove remove the the CANCELLED CANCELLED CAUTION CAUTION message? message?
By resetting the appropriate circuit breaker.
By pressing and holding any CLR pb for more than 3 seconds.
Only maintenance can reset this function.
By pressing and holding the RCL pb for more than 3 seconds.
The The location location of of the the DFDR DFDR (Digital (Digital Flight Flight Data Data Recorder) Recorder) is is ::
Inside the Cockpit.
Installed in the tail Section of the aircraft, and the data is stored on a tape Contained in fire and shock proof box.
In the passenger Cabin for protection reason.
When When is is the the DFDR DFDR automatically automatically energized? energized?
The DFDR will be only energized after the first engine start.
The DFDR is energized during 5 minutes and then after the first engine start.
The DFDR will be energized at lift off.
When 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 ::
When aircraft lighting is selected OFF.
On landing.
After first engine start.
When both engines are started.
On On the the pedestal pedestal the the DFDR DFDR EVENT EVENT pb pb can can be be used used to to mark mark an an event event on on the the DFDR DFDR tape. tape.
False.
True.
When When aa DFDR DFDR fault fault occurs, occurs, itit will will be be signaled signaled by by ::
A fault light illuminating amber on overhead panel.
An ECAM caution message.
A low frequency signal sounds through the cockpit loud speaker.
A MAINTENANCE message in the status page.
Please Please indicate indicate the the PFD. PFD.
Please Please indicate indicate the the SD. SD.
Please Please indicate indicate the the ND ND 2. 2.
Color Color coding coding on on the the ECAM ECAM screens: screens: which which color color indicates indicates that that crew crew awareness awareness is is required? required?
Red.
Amber.
Green.
White.
Color Color coding coding on on the the ECAM ECAM screens: screens: which which color color indicates indicates that that there there is is immediate immediate action action required? required?
Red.
Amber.
Green.
White.
Color Color coding coding on on the the ECAM ECAM screens: screens: which which color color indicates indicates aa normal normal condition? condition?
Red.
Amber.
Green.
White.
On On the the ECAM ECAM SD SD page, page, what what does does an an advisory advisory message message mean? mean?
The parameter is about to reach a limit.
The parameter is out of limits. limits.
The parameter has a faulty indication.
1.1 5.1
You You have have an an ENG ENG 11 FIRE FIRE warning. warning. On On the the ECAM ECAM E/WD E/WD page, page, what what does does the the green green arrow arrow at at the the bottom of the page mean? bottom of the page mean?
It indicates that there is a STS page behind.
It indicates that there is a system page behind.
It means that there is more information to be seen.
On On the the ECAM ECAM ENGINE ENGINE system system page, page, you you observe observe the the VIB VIB (N2) (N2) indication. indication. What What is is the the name name of of such such an an indication pulsing? indication pulsing?
Alert.
Warning.
Caution.
Advisory.
1.1 5.1
On On the the PFD, PFD, what what is is the the actual actual speed? speed?
200 150 kt. kt.
160 kt. kt.
180 160 140
169 kt. kt.
120 185 kt. kt.
F
In In flight flight with with the the following following display display on on the the PFD PFD speed speed scale, scale, which which statement statement is is correct? correct?
The present speed is 250 kts selected by the crew and the MAX speed for lowering landing gear is VLE 230 kts. kts.
280 The aircraft’ aircraft’s speed is 250 kts which is a managed speed. The symbol at 230 kts represents the VFE corresponding to the next flap lever position.
The present speed of 250 kts is selected by the crew. The circle at the bottom of the scale represents green dot speed which is the engine out operating speed in clean configuration. The = symbol at 230 kts represents a speed constraint. The circle on the bottom represents green dot speed which is the holding speed.
260 240 = 220 o
On On the the PFD, PFD, the the magenta magenta symbols symbols on on the the speed speed scale scale represent: represent:
The ECON speed range during managed descent.
360 The managed speed by the FMGS during managed climb.
The upper magenta for high speed protection, the lower for turbulence operating speed.
The lower magenta symbol represents VLS.
340 320 300 .636
Is Is itit possible possible to to change change the the baro baro reference reference display display from from Hecto Hecto Pascals Pascals to to inches inches of of mercury mercury and and vice vice versa? versa?
No, it is not possible because each airline has its own configuration.
Yes, by rotating the outer scale of baro reference selector on the EFIS panel.
No, the crew should refer to a conversion table.
Yes, but only the Captain side is equipped with this conversion.
1020
On On the the PFD PFD altimeter altimeter scale, scale, which which statement statement is is correct correct ??
The crew is pushing the baro reference selector to change from STD setting to local QNH.
Crew is pushing the baro reference selector to change from local QNH to the STD setting.
The rate of descent is 240 FPM.
FL 70 STD Aircraft passing altitude is 8500 ft.
On On the the PFD, PFD, what what is is the the maximum maximum speed speed for for the the present present configuration? configuration?
250
220 180 kt. kt.
200 191 kt. kt.
215 kt. kt.
180 160 140
250 kt. kt.
S
On On the the PFD, PFD, what what is is the the maximum maximum speed speed to to select select the the next next flap flap setting? setting?
200 140 kt. kt.
155 kt. kt.
180 = 160 140
175 kt. kt.
120 185 kt. kt.
F
On On the the PFD, PFD, what what is is the the meaning meaning of of the the blue blue ribbon ribbon on on the the altitude altitude scale? scale?
It marks the landing elevation.
It marks the selected altitude.
It marks the preselected altitude.
FL 70 7000
30.08 STD It marks the decision height.
QNH
On On the the PFD, PFD, what what is is the the actual actual vertical vertical speed? speed?
80 ft/min in climb.
800 ft/min in descent.
80 ft/min in descent.
FL 70 7000
30.08 STD QNH
800 ft/min in climb.
On On the the PFD, PFD, what what is is the the actual actual heading? heading?
069.
080.
084.
On On the the PFD, PFD, what what is is the the selected selected heading? heading?
069.
080.
084.
On On the the PFD, PFD, what what is is the the actual actual aircraft aircraft track? track?
069.
080.
084.
On On the the PFD, PFD, which which of of the the following following statements statements is is true? true?
The aircraft is in a climb, drifting to the left.
The aircraft is in a climb, drifting to the right.
The aircraft is in a descent, drifting to the left.
The aircraft is in a descent, drifting to the right.
On On the the ND, ND, which which of of the the following following statements statements is is true? true?
The heading to the next waypoint PAS is 108, it is at 28 NM, time left to the waypoint is 9 minutes and 8 seconds.
The heading to the next waypoint PAS is 108, it is at 28 NM, time to the destination is 9 hours and 8 minutes.
The track to the next waypoint PAS is 108, it is at 28 NM, elapsed time of this flight is 9 minutes and 8 seconds.
The track to the next waypoint PAS is 108, it is at 28 NM, it will be overflown at 9:08.
ATC ATC cleared cleared you you to to FL FL 150. 150. The The PF PF sets sets the the new new altitude altitude on on the the FCU. FCU. What What will will happen happen ifif he he pulls pulls the the ALT selection knob? ALT selection knob?
The aircraft will stop the climb at FL 60 until passing the constraint then continue climb to FL 150.
The aircraft will disregard the constraint and climb to FL 150.
As soon as the aircraft passes FL 60, the target altitude on the PFD will change to FL 150 and the aircraft continues to climb.
The aircraft will level off at FL 60. The PF must pull the ALT selection knob a second time to climb to FL 150.
The The FCU FCU target target altitude altitude is is FL FL 150, 150, you you are are climbing climbing toward an ALT constraint. toward an ALT constraint. What What will will happen happen ifif the the PF PF pushes pushes the the ALT ALT selection knob? selection knob? NOTE: NOTE: The The constraint constraint alt alt is is FL60. FL60.
The aircraft will level off at FL 60. The PF must push or pull the ALT selection knob a second time to climb to FL 150.
The aircraft will disregard the constraint and climb to FL 150.
As soon as the aircraft passes FL 60, the target on the PFD will change to FL 150 and the aircraft continues to climb.
No change, the aircraft will stop the climb at FL 60 until passing the constraint then continue climb to FL 150.
The The FCU FCU target target altitude altitude is is FL FL 150, 150, you you are are climbing climbing toward an ALT constraint. toward an ALT constraint. What What will will happen happen ifif the the PF PF pulls pulls the the HDG/TRK HDG/TRK selection knob now? selection knob now?
The aircraft will continue on the present heading, stop the climb at FL 60.
The aircraft will stay on the present heading, disregard the constraint and climb to FL 150.
The aircraft will follow the FF-PLN, stop the climb at FL 60 until passing the constraint then continue climb to FL 150.
The aircraft will follow the FF-PLN, disregard the constraint and climb to FL 150.
On On the the MCDU, MCDU, you you notice notice that that some some waypoints waypoints have have aa small small triangle triangle behind behind the the name. name. What What does does itit stand stand for? for?
It means these waypoints will be overflown. overflown.
It means these waypoints are compulsory reporting points.
It indicates altitude constraints at these waypoints.
It indicates speed constraints at these waypoints.
You You get get the the message message DECCELERATE DECCELERATE on on the the FMA. FMA. What What does does itit mean? mean?
The FMGC warns you about a possible overspeed. overspeed.
TCAS discovered a possible traffic conflict and warns you to decelerate to keep your separation.
Due to some environmental circumstances, the aircraft missed a speed constraint.
You are advised to slow the aircraft to loose energy so that you will be able to intercept the descent path.
The The a/c a/c is is climbing climbing to to FL250 FL250 as as set set on on the the FCU, FCU, an an altitude altitude constraint constraint has has been been inserted inserted at at FL90. FL90. What What is is the the procedure procedure when when the the a/c a/c reaches reaches FL90? FL90?
The pilot flying must push the ALT knob.
The pilot flying must turn the ALT knob.
No procedure, the a/c will automatically resume the climb after having sequenced the constrained waypoint.
The a/c will not match the constraint, the pilot has to climb by using V/S mode.
In 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 ??
It is the FMGC corresponding to the AP engaged or FMGC1 when both AP engaged.
Randomly at power up.
It is the FMGC corresponding to the Pilot Flying side.
It is always FMGC1.
The The autothrust autothrust system system has has two two channels. channels. Which Which FMGC FMGC controls controls the the A/THR A/THR (both (both FMGCs FMGCs being being operative)? operative)?
The FMGC1.
The FMGC2.
The randomly chosen FMGC.
Setting Setting the the thrust thrust levers levers to to TOGA TOGA will will arm arm the the A/THR. A/THR. Where Where do do you you check check that that the the A/THR A/THR is is armed? armed?
On the FMA, in the Autothrust mode column.
On the FMA, in the AP/FD and A/THR engagement status column.
On the thrust levers FLEX detent.
On the MCDU takeoff page.
Dashes Dashes in in the the FCU FCU window window indicate indicate the the system system has has enough information to manage the settings of the enough information to manage the settings of the targets. targets. Why Why is is the the altitude altitude window window not not dashed? dashed?
The altitude window shows digits as the target altitude is always set manually by the pilot.
The altitude selector knob has not been pushed.
The altitude selector knob has not been pulled.
Both autopilots must be engaged.
The The speed speed window window on on the the FCU FCU is is dashed. dashed. What What does does itit mean? mean?
The target speed is managed by the FMGC.
A speed target is selected.
The pilot has pulled the speed selector knob.
The autothrust mode is speed.
You You are are in in managed managed speed speed mode. mode. IfIf you you pull pull the the speed speed selector selector knob, knob, which which speed speed value value will will appear appear on the FCU window ? on the FCU window ?
The max limit speed according to the aircraft configuration.
VLS + 20 kt. kt.
The current speed.
VMO or MMO.
When When can can you you engage engage autopilots autopilots 1+2 1+2 at at the the same same time? time?
Never.
For any kind of approach.
As soon as the APPR mode is armed for an ILS approach.
As soon as the APPR mode is armed for a non precision approach on managed mode.
ALT ALT magenta magenta is is displayed displayed on on the the FMA. FMA. What What does does itit mean? mean?
ALT is armed and an altitude constraint has been inserted in the FF-PLN.
ALT is armed, the target altitude is given by the ALT window in the FCU.
The aircraft is on descent and the target altitude is higher than the current aircraft altitude.
The target altitude is above the glide slope altitude capture.
What What is is the the meaning meaning of of A/THR A/THR white? white?
A/THR is armed.
A/THR is disconnected.
A/THR is available.
A/THR is active.
Have -PLN page. FF-PLN Have aa look look at at the the MCDU MCDU Fpage. Notice Notice the the small small white white arrow arrow shown shown on on the the right right top. top. ItIt indicates indicates that that ::
We can move this page to the right.
Another page is automatically displayed in relation to the phase of the flight.
Another page is available and can be displayed by selecting the NEXT PAGE key.
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 the INIT INIT PAGE PAGE A, A, the the displayed displayed coordinates coordinates are: are:
The runway threshold position.
The aircraft present position.
The airport reference point position.
The alternate airport position
The -PLN page FF-PLN The Fpage shown shown in in the the MCDU MCDU is is ::
The FF-PLN page A.
The FF-PLN page B.
The The standard standard instrument instrument departure departure is is shown shown on on the the navigation navigation display, display, however however an an amber amber line line can can be be seen: seen:
It is the secondary FF-PLN.
It is a temporary FF-PLN.
It is the engine out standard instrument departure.
It is the standard departure for light airplanes.
Have Have aa look look at at the the MCDU, MCDU, the the ILS ILS 23R 23R is is aa currently currently selected selected approach, approach, the the green green color color means: means:
This approach is inserted into the active F-PLN.
This approach is displayed in green before insertion in the FF-PLN.
This approach can not be selected.
The The ILS ILS 23L 23L has has been been selected. selected. On On the the MCDU, MCDU, what what is is the the meaning meaning of of the the yellow yellow font? font?
The selection has been made on the secondary FPLN.
This selection is definitely done and cannot be erased.
The selection is temporary (not yet inserted).
The crew has made a wrong selection.
The -PLN waypoint FF-PLN The lateral lateral revision revision page page from from aa Fwaypoint shows shows VIA/GO VIA/GO TO TO data data field, field, itit is is used: used:
To buildbuild-up a FF-PLN waypoint by waypoint.
To enter VIA a beacon TO a waypoint.
To build routes using airways.
To enter VIA/GO TO a new airport.
After After engines engines start, start, which which page page shall shall be be used used to to enter enter any any weight weight modification? modification?
The PROG page.
The PERF takeoff page.
The A/C STATUS page.
The FUEL PRED page.
Have Have aa look look at at the the PFD, PFD, the the magenta magenta digit digit value value displayed displayed on on the the top top of of the the speed speed scale scale is: is:
V2 as manually set on the FCU.
V1.
V2 as entered on the MCDU takeoff page.
V2 + 10.
What What is is the the meaning meaning of of RWY RWY green green on on the the FMA FMA ??
The lateral guidance during takeoff roll is linked to the ILS localizer signal.
The aircraft is automatically guided to maintain the runway center line.
The runway used for takeoff is confirmed by ATC.
The The FCU FCU selected selected altitude altitude is is FL150, FL150, the the aircraft aircraft is is climbing climbing toward toward FL60 FL60 as as shown shown on on PFD. PFD. Why Why is is FL60 FL60 displayed displayed in in magenta? magenta?
This is an altitude constraint.
A speed constraint is entered.
The active vertical mode is not OP CLB.
The aircraft rate of climb is too low.
Have Have aa look look at at the the ND. ND. What What is is the the meaning meaning of of the the highlighted highlighted magenta magenta symbol? symbol?
The aircraft is in OP CLB mode.
The altitude constraint cannot be satisfied.
The aircraft will level off at that point to satisfy the altitude constraint.
The aircraft will resume the climb at that point.
On On the the climb climb flight flight path, path, 22 engines engines running, running, the the SRS SRS (speed (speed reference reference system) system) provides provides aa pitch pitch attitude attitude to to maintain: maintain:
V2.
V2 + 10.
F speed.
Green dot speed.
In In this this situation, situation, what what will will happen happen ifif you you push push the the HDG HDG knob? knob?
Nothing will happen as PERUS is the FROM WPT and as such, the active leg cannot be intercepted.
NAV will be armed (blue) and an intercept point will be computed by the FM to intercept the active leg.
The aircraft will follow the selected HDG whatever the action on the FCU is.
The selected target will change from a HDG to a TRK.
What What is is the the meaning meaning of of GA GA TRK, TRK, displayed displayed on on the the FMA? FMA?
The aircraft is guided by the autoflight system along the programmed missed approach navigation.
The aircraft is guided along a new route as the navigation accuracy level reverted to “low” low” at the time of go around.
The aircraft maintains the track followed at mode engagement.
The aircraft proceeds on the fastest way to come back for a new approach.
Any Any time time the the alpha alpha floor floor protection protection is is triggered, triggered, TOGA autothrust TOGA thrust thrust is is automatically automatically set set by by the the autothrust. autothrust.. When is this protection available? When is this protection available?
Throughout the whole flight envelope.
Only available on configuration 2, 3 or full (with flaps extended).
From lift off until 20 feet on approach.
From lift off until 100 feet on approach.
Why Why must must the the pilot pilot press press the the take take over over pushbutton pushbutton on on the the side side stick stick twice twice to to disconnect disconnect the the autopilot? autopilot?
A first time to disconnect the autopilot and a second time to confirm the disconnection.
A the first time to disconnect the autopilot and a second time to get a definite priority on his side.
A first time to disconnect the autopilot and a second time to reset all the related warnings.
A first time to disconnect the autopilot and a second time to reset the master FMGC.
What AUTOFLT A/THR ” message LIMITED What does does the the ““AUTOFLT A/THR LIMITED” LIMITED” message mean? mean?
The autothrust is still active but can control the thrust to IDLE only.
The autothrust is active but the thrust is limited by the thrust levers position.
The autothrust is active but only one channel is operative.
The maximum engine thrust has been automatically reduced by the FADECs. FADECs.
Both Both autopilots autopilots are are engaged engaged which which FMGC FMGC is is master? master?
FMGC1. FMGC 1
FMGC2.
It depends on the active flight phase.
None as the two FMGC’ FMGC’s are acting independently.
FMGC 2
FD1 FD1 +2 +2 are are ON, ON, no no AP AP is is engaged, engaged, which which FMGC FMGC is is master? master?
The switching occurs at every FMGC power up.
It depends on which ATHR channel is engaged.
FMGC2.
FMGC1.
FMGC 1
FMGC 2
In In independent independent operation operation mode mode which which FMGC FMGC is is master? master?
FMGC1.
FMGC2.
None, the two FMGC’ FMGC’s are acting independently.
It depends on which FMGC was the master at the time of dual mode failure.
FMGC 1
FMGC 2
What OPP FMGC ”, PROCESS What is is the the meaning meaning of of ““OPP FMGC IN IN PROCESS” PROCESS”, the the message message displayed displayed here here in in the the scratchpad scratchpad of of MCDU1? MCDU1?
MCDU1 is driven by FMGC2.
The FMGC2 is now master.
The FMGC2 performance became better than the FMGC1.
What SET OFFSIDE ” RNG/MODE What is is the the meaning meaning of of ““SET OFFSIDE RNG/MODE” RNG/MODE” which which appears appears on on ND1? ND1?
The selection of the offside range mode will allow the display of the navigation map on this side.
The selection of the offside range mode will make the FMGC’ FMGC’s resynchronization shorter.
The selection of the offside range mode will make the return on FMGC dual mode easier.
The selection of the offside range mode will reduce the FMGC1 reset duration at one minute.
The The FCU1 FCU1 has has failed, failed, how how can can we we use use the the FCU FCU now? now?
FCU 1 failure has no consequences on the FCU utilization, as the second channel has automatically taken over.
The FCU is totally unserviceable.
Only the lateral modes can be set from the FCU panel.
Some FCU functions LOC and APP pushbuttons are not available.
The The FCU FCU 11 and and 22 have have failed, failed, how how the the pilot pilot can can control control the the vertical vertical and and lateral lateral modes? modes?
Both AP’ AP’s are lost but the FCU controls and indications are still available.
Only the FD1 and 2 are available.
The vertical and lateral modes cannot be controlled from the FCU. Only the manual flight on raw data is possible.
The pilot can control the lateral and vertical modes using the MCDU.
What INDEPENDENT OPERATION” ”, OPERATION What does does ““INDEPENDENT OPERATION”, displayed displayed in in both both MCDU MCDU scratchpads, scratchpads, mean? mean?
The pilot can engage both AP in all phases of flight.
The cross talk function is lost, each FMGC will work independently, the same entry has to be made on both MCDUs. MCDUs.
There is no more radio updating of FMGC position and only the mix coordinates are provided for navigation.
the IRS the
The OPP FMGC ” is PROCESS The FMGC1 FMGC1 failed failed and and ““OPP FMGC IN IN PROCESS” PROCESS” is displayed displayed on on the the MCDU1. MCDU1. The The FMGC2 FMGC2 has has taken taken over over automatically automatically ::
The entry can be done from either MCDU.
The entry can be done from MCDU 1 only.
The entry can be done from MCDU 2 only.
FMGC 1
FMGC 2
You THR IDLE/DES” ” modes IDLE/DES You are are in in ““THR IDLE/DES” modes with with autopilot autopilot 11 engaged engaged and and the the FCU FCU 11 fails. fails. What is the action required? What is the action required?
As the autopilot 1 disengages, engage autopilot 2.
The PFD barometric reference is now only available on standard and the pilot must set the current baro setting on the standby altimeter.
The FCU2 has taken over automatically and the baro reference must be cross checked.
What What happens happens ifif the the HDG HDG selector selector knob knob is is pushed? pushed?
The aircraft reverts to TRK.
The HDG/TRK target changes.
Nothing, the aircraft follows indefinitely the selected HDG/TRK.
The aircraft continues to follow the current HDG until FF-PLN interception.
What What happens happens ifif the the HDG HDG selector selector knob knob is is pulled? pulled?
The aircraft reverts to the original FF-PLN.
The HDG target changes to TRK.
The aircraft follows the selected HDG until intercepting the lateral FF-PLN.
Nothing, the aircraft continues on HDG 140 indefinitely.
Please Please indicate indicate the the position position of of the the two two FLIGHT FLIGHT DIRECTOR DIRECTOR (FD) (FD) controls. controls.
Is Is the the aircraft aircraft following following aa track track or or aa heading? heading?
Track
Heading
Look Look at at the the FMA. FMA. LOC LOC in in blue blue is... is...
The active lateral mode which is a constraint.
The armed lateral mode.
The armed lateral mode which is a constraint.
The active lateral mode.
Look Look at at the the FMA. FMA. NAV NAV in in green green is... is...
The active lateral mode which is a constraint.
The armed lateral mode.
The armed lateral mode which is a constraint.
The active lateral mode.
A/THR A/THR in in blue blue means means itit is... is...
disconnected.
armed.
active.
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 ::
Provide guidance, if a localizer is available for taketake-off and rollroll-out phases.
Provide guidance after taketake-off up to 1000 feat AGL to maintain the runway center line.
Confirm that the aircraft is well established in the glide slope on ILS final approach.
Change over automatically in case of localizer failure on ILS final approach.
What What does does MAN MAN TOGA TOGA indicate indicate on on the the FMA FMA column? column?
The thrust has been manually set to TOGA.
The autothrust system is inoperative.
The FMGC guidance autothrust command is unserviceable.
The pilot has disconnected the autothrust system.
With With all all engines engines operative operative and and A/THR A/THR armed, armed, how how does ? autothrust does aa pilot pilot activate activate the the autothrust? autothrust?
The autothrust will be automatically activated by the FMGC without any pilot action when crossing the thrust reduction altitude.
The autothrust will become active when the pilot sets the thrust levers in the climb detent.
The thrust levers must be set to idle and then in the climb detent to activate the autothrust. autothrust.
““LVR LVR CLB” ” white CLB CLB” white flashing flashing on on the the FMA FMA indicates indicates ::
We have crossed the thrust reduction altitude.
The autothrust levers are stuck and can not be put in the climb detent.
The pilot has forgotten to enter the FLEX temperature on the MCDU taketake-off page before taking off.
The thrust levers will automatically move to the climb detent.
You You are are established established in in climb, climb, THR THR CLB CLB mode mode is is active: active:
The speed is controlled by the thrust and the rate of climb by the autopilot.
The constant rate of climb is maintained by the autopilot.
A/THR commands CLB thrust and AP maintains the target speed by using pitch adjustments.
The speed and the rate of climb are controlled by the thrust.
The The aircraft aircraft has has leveled leveled off off at at 13000 13000 feet, feet, ALT ALT is is green green on on the the FMA FMA and and the the autothrust autothrust is is in in SPEED SPEED mode: mode:
The target speed and the altitude are maintained by the autopilot.
The target speed is maintained by the autopilot and the altitude is controlled by the autothrust. autothrust.
The autothrust system controls the thrust to maintain the target speed and the autopilot maintain the altitude by adjusting the pitch.
The altitude and speed are maintained by the A/THR.
Why Why do do you you set set the the thrust thrust levers levers to to IDLE IDLE for for landing? landing?
To engage the manual mode of the autothrust. autothrust.
To be prepared in case of touch and go.
To disconnect the A/THR.
According According to to these these indications, indications, what what is is the the correct correct statement? statement?
The A/THR is armed.
The A/THR is active.
The A/THR has failed.
The A/THR is disconnected.
ALT ALT mode mode is is engaged, engaged, MCDU MCDU PERF PERF page page indicates indicates CLB. CLB. Why? Why?
The FMGS is unable to control the climb.
FL290 is above the initial CRZ FL.
The FMGS 1 has failed.
FL290 is the FCU selection, and is below the CRZ FL.
ALT ALT mode mode is is engaged engaged at at FL290, FL290, MCDU MCDU PERF PERF page page indicates indicates CLB. CLB. How How do do you you obtain obtain ALT ALT CRZ CRZ on on the the FMA at that flight level (FL290) ? FMA at that flight level (FL290) ?
Set the new altitude clearance FL290 on the MCDU PROG page.
Set the new altitude clearance on the FCU.
Push the altitude selector knob to continue the climb as programmed before.
We We are are in in OP OP DES DES and and THR THR IDLE IDLE modes modes ::
The autothrust maintain the thrust at idle and the auto pilot adjust the pitch to maintain the target speed.
The autothrust adjust the thrust to maintain the target speed and the autopilot control the descent flight path.
The autothrust maintain the thrust at idle and the autopilot control the vertical speed.
The autothrust control the target speed and the rate of descent.
The The approach approach phase phase activation activation can can be be done: done:
Automatically when the aircraft overfly the deceleration point or manually by the pilot on the PERF page
Only manually by the pilot through the MCDU PERF. Page.
Only automatically at the deceleration point.
As As soon soon as as the the approach approach phase phase is is activated, activated, the the managed managed speed speed will will depend depend on: on:
Which autopilot is engaged.
The vertical mode previously flown.
Which FMGC is the master.
The aircraft configuration.
At At 400 400 feet feet RA RA the the LAND LAND mode mode engages. engages. How How can can this this mode mode be be disengaged: disengaged:
By pulling the heading selector knob.
By pulling the V/S - FPA knob.
By pressing the approach mode pushbutton.
By setting TOGA to engage the go around mode.
What What is is the the meaning meaning of of the the small small magenta magenta dot dot displayed displayed by by the the altitude altitude scale? scale?
It warns the pilot about a possible wrong altitude setting on the FCU.
It highlights any vertical deviation of the aircraft from the computed descent profile.
It warns the pilot that the speed must be reduced to regain the computed descent profile.
It indicates that the expedite mode must be engaged.
You You want want to to speak speak to to the the mechanic. mechanic. He He is is somewhere ’t see can somewhere around around the the aircraft aircraft but but you you can’ can’t see him. How do you get his attention? him. How do you get his attention?
I open the side window and try to get his attention.
I use the MECH pb sw on the CALLS panel.
I use VHF 3 to call him.
I select the MECH transmission key on the ACP.
During During Preflight, Preflight, check check of of the the CVR CVR operation operation is is performed performed as as follow. follow.
The system being operative as soon as aircraft Elec Power network is powered, on the RCDR Control panel, press the CVR TEST pb, you get an audio signal for correct operation. On the RCDR control panel, press the GND CTL pb to switch the CVR ON, then press the CVR TEST pb.
The CVR TEST can only be performed after one engine is started then “B” answer is applied.
Be sure the PARKING BRK is ON then repeat “B” answer.
After After landing, landing, to to erase erase the the CVR... CVR...
The aircraft must be on the ground with the parking brake set.
The aircraft must be on the ground with at least one engine running.
The aircraft must be off the ground.
The engines must be shut down for at least 5 minutes.
On On the the RMP RMP control control panel, panel, what what does does the the white white SEL SEL light light mean? mean?
RMP 1
It is an indication for a SELCAL.
It is an indication that the VHF used on RMP 2 is not the standard one.
RMP 2 It indicates that RMP1 is configured to tune VFH2.
It indicates that RMP2 is configured to tune VHF2.
How How do do you you extinguish extinguish the the white white SEL SEL light? light?
RMP 1
Pressing the SEL pb on RMP 1.
Pressing the VHF 1 and SEL pb on RMP 1.
RMP 2 Pressing the SEL pb on RMP 2.
Pressing the VHF 2 on RMP 2.
On On the the VHF VHF system, system, in in case case of of RMP RMP 11 failure, failure, VHF VHF 11 is is lost. lost.
True.
False.
With With the the AUDIO AUDIO SWITCHING SWITCHING knob knob in in the the CAPT CAPT 33 position, position, the the captain captain substitutes substitutes ACP ACP 33 for for ACP ACP 1. 1.
True.
False.
On On the the communication communication control control panel, panel, the the amber amber CALL CALL light light indicates indicates that that somebody somebody is is trying trying to to reach you via VHF 3. reach you via VHF 3.
True.
False.
You You are are in in an an ELECTRICAL ELECTRICAL EMERGENCY EMERGENCY CONFIGURATION, shortly after CONFIGURATION, shortly after the the fault fault occurred, occurred, you you notice notice the the red red FAULT FAULT light light on on the the RAT RAT & & EMER EMER GEN pushbutton. GEN pushbutton. How How do do you you interpret interpret this this indication indication ??
The EMER GEN is not supplying the system.
The fault light on the RAT & EMER GEN pb will extinguish by depressing it.
The FAULT light is always on when you are in ELEC EMER CONFIG.
You You are are in in an an ELECTRICAL ELECTRICAL EMERGENCY EMERGENCY CONFIGURATION, on ELEC panel CONFIGURATION, on ELEC panel you you have have depressed depressed the the GEN GEN 11 and and GEN GEN 22 pb pb for for reset. reset. The 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 ??
To separate both sides of the electrical system.
To connect both generators directly to the AC ESS BUS.
To connect both sides of the electrical system.
To switch both generators to the opposite side AC BUS.
In In an an ELECTRICAL ELECTRICAL EMERGENCY EMERGENCY CONFIGURATION, CONFIGURATION, after performing the initial ECAM procedure, after performing the initial ECAM procedure, you you have 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 ??
If there was a short circuit, you might recover one generator now.
Because the generators had time to cool down and now a reset might be successful.
You should always try two resets if you have a generator failure.
The The purpose purpose of of the the Integrated Integrated Drive Drive Generator Generator (IDG) (IDG) pb pb sw sw is is to: to:
Disconnect the corresponding generator from its drive shaft.
Reconnect the generator to its drive mechanism.
Cut the corresponding generator supply to AC bus 1 or 2.
Cut the corresponding generator supply to the ESS AC bus.
The The engine engine driven driven generators generators are are running. running.
At the engine RPM trough their gearbox connection.
At constant speed by a drive mechanism between the generator and ENG gearbox.
At a intermediate speed controlled by an electronic computer.
No necessity to control the generator speed because the AC network operates under variable frequency.
GEN 1
GEN 2
IDG 1
IDG 2
The The Electrical Electrical System System includes includes two two buses: buses: AC AC ESS ESS BUS BUS and and DC DC ESS ESS BUS. BUS. In In normal normal configuration configuration ::
AC ESS bus is fed by AC bus 1. DC ESS bus is fed by DC bus 1.
AC ESS bus is fed by AC bus 2. DC ESS bus is fed by DC bus 1.
To balance the Elec load GEN 1 is directly supplying the AC ESS BUS.
To balance the Elec load GEN 2 is directly supplying the AC ESS bus.
The The purpose purpose of of AC AC ESS ESS FEED FEED pb pb sw sw is is to to enable enable the the pilot pilot to to switchover switchover the the supply supply of of AC AC ESS ESS bus. bus.
From AC bus 2 to AC bus 1.
From AC bus 1 to AC bus 2.
From the APU generator.
From ESS DC bus.
Please Please indicate indicate the the position position of of the the ELEC ELEC panel. panel.
Please Please indicate indicate the the position position of of the the EMERG EMERG ELEC ELEC PWR PWR panel. panel.
The The emergency emergency electrical electrical generator generator used used as as aa back back up is hydraulically driven by the RAT which up is hydraulically driven by the RAT 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 above BUS 2 are lost and the aircraft speed is above 100kts. 100kts.
True.
False.
From From ECAM ECAM ELEC ELEC page, page, the the APU APU GEN GEN box box information information indicates indicates that: that:
The APU GEN does not have priority over the external power.
The APU GEN pb SW on overhead panel is off.
The APU is not fully available yet.
There is defect on the APU GEN out put.
Looking Looking at at the the ECAM ECAM ELEC ELEC Page, Page, to to connect connect APU APU GEN: GEN:
Push APU GEN pb sw located overhead panel.
Wait until 1st Engine is Started.
Deselect EXT PWR.
SWITCH OFF BAT 1+2.
What What does does the the APU APU GEN GEN % % indication indication mean mean ??
APU GEN shares 36% of the elec network load, the remaining 64% being taken by the external power.
APU GEN is supplying the network at 36% of its maximum load.
The external power is supplying the network.
During During preliminary preliminary procedure procedure to to check check the the battery battery voltage, voltage, the the associated associated BATT BATT pb pb sw sw should should be: be:
Switched ON.
Switched OFF.
Any position, the voltage indication being all time available.
The The minimum minimum battery battery voltage voltage for for normal normal operation operation should should be: be:
24V.
25,5V.
28V.
The The EXT EXT PWR PWR AVAIL AVAIL illuminated illuminated green green on on the the overhead overhead panel panel means means that that ::
The ground cart is supplying the aircraft network.
The external power is plugged in and delivers bleed air.
The connected ground cart voltage and frequency are normal.
On sw On EXT EXT PWR PWR pb pb sw, sw,, the the illuminated illuminated cyan cyan light light means means that: that:
The ground cart is supplying the aircraft electrical network.
External power is plugged in but not supplying the network.
External power is plugged in and delivers bleed air only.
After °2, is nn°2, After starting starting engine engine n° is the the present present ECAM ECAM ELEC ELEC page page aa correct correct configuration? configuration?
No. ENG GEN n° n°2 should power all aircraft network.
No. The APU GEN should continue powering all aircraft network.
Yes. ENG GEN n° n°2 is now powering its own side.
As As you you enter enter in in the the dark dark cockpit cockpit you you first first check check the the battery battery voltages. voltages. What What are are the the necessary necessary checks checks before before checking checking the the voltages? voltages?
You must check that the external power is available and then switch it on.
You can read the battery voltages immediately. No actions are required.
You have to switch each battery on by its associated pb sw to check the voltage.
In In flight, flight, following following an an AC AC BUS BUS 11 FAULT, FAULT, AC AC ESS ESS FEED FEED pb pb sw sw must must be be depressed depressed in in order order to: to:
Recover AC ESS FEED from AC BUS 2.
Recover AC1 bus.
Recover AC2 bus.
AC AC BUS BUS 11 FAULT FAULT will will definitively definitively lead lead to to the the DC DC and and AC AC ESS ESS buses buses loss: loss:
Yes.
No. Only AC ESS bus is recoverable.
No. DC and AC ESS buses will be recovered by pushing on the AC ESS FEED pb sw. sw.
Following Following an an AC AC BUS BUS 11 fault, fault, pushing pushing the the AC AC ESS ESS FEED FEED pb pb sw sw on on ELEC ELEC overhead overhead panel panel allows allows you: you:
To recover the AC ESS BUS power only.
To recover the DC ESS BUS power only.
To recover AC and DC ESS buses.
To recover AC BUS 1 power.
Following Following the the RAT RAT extension extension due due CONF, the RAT and EMER GEN CONF, the RAT and EMER GEN illuminated. illuminated. What What does does itit mean? mean?
to to ELEC ELEC EMER EMER FAULT light FAULT light is is
We had an ELEC EMER configuration, the RAT is extended.
The fault stays illuminated even after emergency generator connection.
The emergency generator is not connected.
In In case case of of ELEC ELEC EMER EMER CONF, CONF, LAND LAND ASAP ASAP in in red red is is displayed displayed on on the the E/WD. E/WD. This This message message will will stay: stay:
As long as the Red warning ELEC EMER CONF persists.
Even after having reset one generator successfully.
Even if BUS TIE pb sw is pushed.
Even if APU is started.
In In case case of of an an ELEC ELEC EMER EMER CONFIG CONFIG situation, situation, how how can can the the two two sides sides of of the the electrical electrical system system be be segregated e.g to isolate a short circuit ? segregated e.g to isolate a short circuit ?
Push BUS TIE pb SW located on ELEC system overhead panel.
Reset each AC generator.
Manually lower RAT by pushing its pb SW
Nothing has to be done because the segregation is done automatically.
Being Being in in an an EMER EMER ELEC ELEC configuration configuration what what is is happening ? kts happening when when A/C A/C speed speed drops drops below below 140 140 kts? kts?
AC generators are less powerful due to RAT speed decrease.
Electrical network is automatically transferred to the batteries.
You have to stop AC generator by pressing the “MAN ONON-AUTO” AUTO” pb switch.
You have to switch ON the both batteries.
In In ELEC ELEC EMER EMER CONF, CONF, you you are are in in single single display display mode mode on on the the ECAM. ECAM. Can Can you you manually manually call call an an ECAM ECAM system system page page ??
No. The upper ECAM screen is only used for E/WD display.
Yes, by pressing and holding its associated pb SW on the ECAM control panel.
In In EMER EMER ELEC ELEC CONF, CONF, when when the the RAT RAT stalls stalls due due to to A/C A/C speed speed decreasing, decreasing, the the static static inverter inverter will will become become active active in in order order to to supply: supply:
The DC ESS.
The complete DC network.
The AC ESS.
The AC and DC ESS.
In In case case of of avionics avionics bay bay smoke, smoke, GEN GEN 11 LINE LINE pb pb is is selected selected OFF. OFF. What What will will happen? happen?
All warnings will be reset.
The smoke in the avionic bay will be evacuated.
GEN1 will be disconnected from the network.
Fire extinguisher bottle will be armed.
According According to to these these indications, indications, which which statement statement is is true true ??
Both battery voltages are above the minimum of 20 V.
Both battery voltages are below the minimum of 25.5 V.
I can only check the battery voltages on the ECAM ELEC page.
I can only check the battery voltages, with batteries on.
You You want want to to recharge recharge the the batteries. batteries. How How do do you you proceed? proceed?
External power is available. I only have to switch the batteries to on and they will be charged.
I have to switch the external power and the batteries to on and the batteries will be charged.
I have to switch the external power to ON and the batteries will be charged.
I have to call a mechanic because the batteries can only be charged by maintenance.
What What is is the the meaning meaning of of the the green green AVAIL AVAIL light light ??
The external power is plugged in and the voltage and frequency parameters are normal.
The external power is plugged in.
The external power panel door has been opened.
The AVAIL light always illuminates on ground.
After After having having switched switched the the external external power power to to ON, ON, you get the following indications. How do you you get the following indications. How do you interpret interpret the the amber amber generator generator parameters parameters and and the the generator fault lights ? generator fault lights ?
You have to switch the generators to ON.
A failure has been detected. The generators will not be able to supply the electrical system after engine start
There is an internal self test in progress. The fault lights and the amber indications should disappear after 30 seconds.
On ground these indications are normal when the engines are not running.
Both Both batteries batteries are are now now being being charged charged by by the the external power unit. external power unit. Approximately Approximately how how long long does does the the charging charging process process take ? take ?
10 minutes
One hour
20 minutes
Several hours
After After 20 20 minutes minutes you you check check the the ECAM ECAM ELEC ELEC page page again. again. Which Which statement statement is is true true ??
Both battery voltages are still below the minimum voltage.
To check the battery voltages I have to switch them OFF first.
To check the battery voltages I have to disconnect external power first.
Both battery voltages are now above the minimum voltage.
You You have have started started the the APU. APU. Observe ECAM ELEC Observe ECAM ELEC page page !! Why Why is is the the electrical electrical system system still still supplied supplied by by external power only ? external power only ?
External power was connected first.
External power has priority over the APU generator.
The APU generator is still switched off.
The external power voltage is more stable.
The The APU APU generator generator is is supplying supplying the the electrical electrical system. system. By By the the way, way, do do you you know know the the order order of of priority priority for for the different generators ? the different generators ?
engines, external power, APU.
APU, engines, external power.
external power, engines, APU.
APU, external power, engines.
On On the the ELEC ELEC Panel, Panel, you you have have lifted lifted the the IDG IDG red red guard. guard. How How do do you you disconnect disconnect the the IDG IDG now now ??
I push the disconnect button and release it immediately in order to prevent the disconnect mechanism from being damaged.
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.
I push the disconnect button for at least 10 seconds to ensure the disconnection.
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.
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 ??
Yes.
No. The APU should continue powering the aircraft until crew switch it off.
No. GEN1 should supply AC1 and AC2.
No. GEN2 should supply AC1 and AC2.
At 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 ??
Yes.
No.
The crew should shut down one engine at a time to reach this configuration.
The crew should select EXT POWER ON.
You You are are at at the the gate, gate, APU APU GEN GEN is is supplying supplying the the network, the EXT POWER is plugged in. network, the EXT POWER is plugged in. What What will will happen happen when when EXT EXT POWER POWER is is selected selected ON? ON?
The APU GEN will be disconnected and will stop.
The EXT POWER will supply the A/C network.
The APU and ground power will both supply the A/C network .
The transfer between APU supply and ground power will take place only after depressing the APU/GEN pb sw to stop the APU supply.
GEN GEN 11 is is now now inoperative inoperative due due to to the the ECAM ECAM procedure application following an IDG procedure application following an IDG OIL OIL LO LO PR PR caution. caution. Is Is the the associated associated AC AC BUS BUS still still available? available?
Yes. AC ESS is supplying the AC 1.
Yes. GEN 2 has taken over.
No. GEN 2 will be disconnected from AC BUS 2 within 10 minutes.
No. APU must be started to recover AC BUS 1.
When When executing executing ECAM ECAM action action following following an an IDG IDG OIL OIL LO LO PR, PR, the the crew crew will will have have to to hold hold IDG IDG pb pb sw sw pressed for: pressed for:
Minimum 3 seconds.
Maximum 3 seconds.
Until fault amber light goes out.
No time limit.
In In case case of of GEN GEN 22 OVERLOAD OVERLOAD ECAM ECAM caution, caution, how how do do you you off off load load the the generator? generator?
By starting the APU to connect a third generator to share the load.
By switching OFF the galley.
By transferring load on GEN1 in order to keep the galley operating.
Following Following aa GEN GEN 22 OVERLOAD OVERLOAD and and the the shedding shedding of of the the galley galley is is the the ELEC ELEC page page correct? correct?
Yes.
No. The GEN overload should stay amber.
No. The GALLEY SHED message should be removed.
Which Which of of those those area, area, has has NO NO fire fire extinguishing extinguishing system system installed? installed? Cabin.
Avionic bay.
Engine / APU.
Cargo compartments.
Please Please identify identify which which of of those those area area has has aa FIRE FIRE and and OVERHEAT OVERHEAT DETECTION DETECTION system system installed. installed. Cabin.
Avionic bay.
Engine / APU.
Cargo compartments.
ItIt is is the the first first flight flight of of the the day. day. Before Before performing performing the the APU APU fire fire test, test, you you have have to to check that... check that...
The APU FIRE pb is in and guarded and AC power is supplied.
The APU FIRE pb is in and guarded and the APU is running.
The APU FIRE pb is in with the guard in the UP position and the AGENT light is extinguished.
The APU FIRE pb is in and guarded and the AGENT light is extinguished.
The The aircraft aircraft is is not not yet yet supplied supplied with with AC AC power. power. Can Can you you perform perform the the APU APU FIRE FIRE test? test?
Yes.
No.
In In this this case, case, during during the the preliminary preliminary cockpit cockpit preparation preparation the the APU APU FIRE FIRE test test will will trigger trigger the the following indications: following indications:
On the FIRE Control Panel, the APU FIRE light, the SQUIB and DISCH lights will illuminate. Additionally, APU FIRE warning will be triggered on ECAM.
On the FIRE Control Panel, the APU FIRE red light and SQUIB light will illuminate. But the APU FIRE warning will not be triggered on ECAM.
No test is possible until AC power is connected on the Electrical network.
The The APU APU FIRE FIRE test test is is successful. successful.
True.
False.
Does Does the the APU APU fire fire test test on on battery battery trigger trigger the the CRC CRC and and MASTER MASTER WARN? WARN?
Yes.
No.
With With the the following following indication indication on on ECAM, ECAM, what what is is the the FIRE FIRE DETECTION DETECTION status? status?
One fire detection loop has failed. Fire detection for both engines is still available.
Both fire detection loops of engine 1 have failed. Fire detection for engine 1 is inoperative.
One fire detection loop of engine 1 has failed. Fire detection for engine 1 is still available.
One fire detection loop of engine 1 has failed. Fire detection for engine 1 is inoperative.
FDU
According According to to this this ECAM ECAM E/WD E/WD page, page, the the associated associated procedure procedure is is
An indication presenting the FWD CARGO SMOKE condition only.
To press the illuminated red FWD SMOKE DISCH pb.
To lift the red guard and press the DISCH pb.
This is an automatic fonction and you have to press FWD SMOKE pb to confirm.
On On the the CARGO CARGO SMOKE SMOKE control control PANEL PANEL both both DISCH DISCH lights lights illuminated illuminated mean mean that: that:
There is only one fire bottle which has been discharged into both cargo compartments.
The FWD and AFT fire bottles have both been discharged into their associated compartment.
Now there is no longer any available agent which can be discharged in either the FWD or the AFT cargo compartment.
The FWD and AFT fire bottles have both been discharged into the FWD compartcompartment. ment.
According According to to these these indications, indications, which which flight flight control control law law is is active active ??
Normal Law
Alternate Law
Direct Law
Mechanical Back Up
According According to to these these indications, indications, which which flight flight control control law law is is active active ??
Normal Law
Alternate Law
Direct Law
Mechanical Back Up
Observe Observe the the PFD. PFD. Without Without any any sidestick sidestick inputs... inputs...
The aircraft’ aircraft’s attitude will stay constant.
The pitch will stay constant, the bank angle will slowly decrease.
The bank angle will stay constant, constant, the pitch will slowly decrease.
The aircraft’ aircraft’s attitude will slowly tend towards “wings level” level” and “pitch 0” 0”.
According According to to the the following following indications... indications...
The High Angle Of Attack protection has been triggered.
The Alpha Floor protection has been triggered.
The Load Factor Limitation has been triggered.
There is no protection triggered yet.
Let’ ’s assume, Let Let’s assume, you you have have set set idle idle power power and and pulled pulled the the sidestick sidestick back back to to maintain maintain altitude. altitude. Observe Observe the the PFD. If you release the sidestick now... PFD. If you release the sidestick now...
The aircraft will descend at 135 kts. kts.
The aircraft will descend at 150 kts. kts.
The aircraft will maintain altitude until 120 kts are reached .
The aircraft will maintain altitude until a stall occurs.
According According to to these these indications... indications...
The High Angle Of Attack protection has been triggered.
The Alpha Floor protection has been triggered.
The Load Factor Limitation has been triggered.
There is no triggered protection.
According According to to these these indications, indications, ifif the the sidestick sidestick is is held held in in the the full full back back position... position...
The speed will fall below 120 kts. kts. The airplane might stall.
The speed will fall below 120 kts. kts. To avoid a stall, climb power will be automatically set.
The High Angle Of Attack protection will override the sidestick input. The pitch will be lowered to maintain 120 kts. kts.
The speed will fall further. At 114 kts the pitch will be lowered to maintain 114 kts. kts.
Observe Observe the the PFD. PFD. Which Which statement statement is is true true ??
The Alpha Floor protection has automatically set CLB power.
The Alpha Floor protection has automatically set TO/GA power.
The Alpha Floor protection will override sidestick inputs. The nose will be lowered.
A stall is detected.
To To fly fly aa coordinated coordinated turn... turn...
No rudder inputs are required.
You have to center the sideslip indicator with the rudder pedals.
Only small rudder inputs are required.
In In Normal Normal Law, Law, is is there there aa maximum maximum pitch pitch attitude attitude ??
A
Yes, indicated by the green dashes (A).
B
Yes, indicated by the green dashes (B).
No.
Yes, pitch is limited to 20º 20º nose up.
In In Normal Normal Law, Law, is is there there aa maximum maximum bank bank angle angle ?? a
No. b
Yes, indicated by the green dashes (b).
Yes, indicated by the white dashes (a).
Yes, bank is limited to 80º 80º.
How How do do you you interpret interpret the the amber amber crosses crosses on on the the PFD PFD ??
The autotrim is lost. You have to use manual pitch trim.
The ailerons are controlled directly by the sidesticks. sidesticks.
The bank angle limit protection is lost.
The bank angle protection is active.
The ’s sidestick CPT The CPT’ CPT’s sidestick is is deflected deflected fully fully left left and and the the FO’ ’ s sidestick is simultaneously deflected fully FO FO’s sidestick is simultaneously deflected fully right. right. Which Which indications indications do do you you expect expect ??
IfIf both both pilots pilots deflect deflect their their sidesticks sidesticks fully fully back... back...
The “pitch up” up” order is twice as great as compared only one stick deflected.
The “pitch up” up” order is 1.5 times greater as compared to only one stick deflected.
No inputs are sent to the flight control computers unless one pilot presses the take over pb on his stick.
The “pitch up” up” order is equal to a single stick fully deflected.
IfIf the ... pb the FO FO presses presses the the take take over over pb... pb...
The CPT is unable to rere-activate his sidestick. sidestick.
The CPT’ CPT’s sidestick is still active. It will be dede-activated after 40 secs. secs.
The CPT can rere-activate his sidestick by pressing the take over pb for more than 40 secs. secs.
The CPT can rere-activate his sidestick immediately by pressing his take over pb. pb.
CPT CPT
FO FO
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
The CPT’ CPT’s sidestick is dede-activated unless he presses his take over pb. pb.
The CPT is unable to rere-activate his sidestick for the rest of the flight.
Both sidesticks are active.
CPT CPT The CPT’ CPT’s sidestick is active as long as the FO’ FO’s sidestick is in neutral position
FO FO
With With either either AP AP engaged, engaged, which which statement statement is is true true ??
Both sidesticks are locked in neutral position. The lock can not be overridden
Both sidesticks are dede-activated until the AP is disengaged.
Both sidesticks are locked in neutral position. By applying a certain force, the lock can be overridden but the AP remains engaged.
Both sidesticks are locked in neutral position. By applying a certain force, the lock can be overridden and the AP is disengaged.
What What will will happen happen next next ??
The left SPLR 3 will be retracted, the right SPLR 3 will be inhibited to prevent asymmetry.
The right SPLR 3 will be extended to prevent asymmetry.
Left SPLR 3 remains extended, spoiler operation is not possible anymore.
After After aa turn, turn, you you have have the the following following message. message. What What happened happened ??
The left SPRL 3 failed to extend.
The right SPRL 3 failed to extend.
The left SPRL 3 failed to retract.
The right SPRL 3 failed to retract.
What What will will happen happen just just before before the the speed speed reaches reaches VFE VFE Speed Speed (red (red barber barber pole)? pole)?
Auto flap retraction at 210 kts. kts.
Auto flap and slat retraction at 210 kts. kts.
High Speed protection will become active, the autopilot will increase the pitch.
High Speed protection will become active, the autothrust will reduce thrust.
The The message message WING WING TIP TIP BRK BRK ON ON appears appears on on the the E/WD. E/WD. What What does does itit mean? mean?
A hydraulic device locks the flaps in their present position.
F/CTL FLAPS LOCKED -WING TIP BRK ON MAX SPEED . . . . . . . .
To reduce structural stress, the slats movement is being slowed down through the wing tip brakes.
To avoid asymmetry, the outer slats are locked in their present position.
Because of the locked flaps, the wing tip brake also lock the slats.
Which Which control control surfaces surfaces are are used used for for the the mechanical mechanical backup? backup?
Ailerons and rudder.
THS and rudder.
Elevator and ailerons.
THS and elevator.
How How many many actuators actuators are are provided provided to to control control the the ailerons ailerons and and how how many many hydraulic hydraulic sources sources supply supply these these actuators? actuators?
2 hydraulic sources with 4 actuators
1 hydraulic source with 2 actuators
4 hydraulic sources with 4 actuators
3 hydraulic sources with 4 actuators
What What does does the the white white cross cross indicate? indicate?
It is an indicator for the sidestick deflections during the flight control check.
It is an indicator for the control surfaces deflections during the flight control check.
It is an indication for the rudder pedals deflections during the flight control check.
In In Normal Normal Law, Law, ifif one one sidestick sidestick is is rapidly rapidly pulled pulled fully ’s maximum airplane fully back, back, can can the the airplane’ airplane’s maximum allowable allowable ““G” G” load load be be exceeded exceeded ??
Yes. Rapid sidestick deflection must never be made.
Yes, until maximum pitch attitude is reached.
No. At maximum “G” load, the sidesticks are dede-activated for 5 seconds.
No. The load factor limitation overrides sidestick commands to avoid excessive “G” loads.
With With the the sidestick sidestick fully fully forward, forward, what what will will be be the the maximum maximum airspeed airspeed indication? indication?
According According to to these these indications, indications, ifif you you release release the the sidestick sidestick now... now...
The bank angle will automatically return to 33º 33º.
The bank angle will not change.
The bank angle will return to wings level, because the bank protection is active.
The bank angle will return to 20º 20º.
In 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 ??
33º 33º
There is no bank limitation.
80 º
67 º
According According to to these these indications, indications, which which flight flight control control law law is is active active ??
Normal Law.
Alternate Law.
Direct Law.
Mechanical Back Up.
According According to to these these indications, indications, which which flight flight control control law law is is active active ??
Normal Law
Alternate Law
Direct Law
Mechanical Back Up
Which Which ECAM ECAM FUEL FUEL page page corresponds corresponds to to this this E/WD? E/WD?
Which Which ECAM ECAM FUEL FUEL page page corresponds corresponds to to this this E/WD? E/WD?
You You are are in in cruise cruise and and according according to to those those indications, indications, aa failure failure occurred occurred in in the the fuel fuel system. system. Why didn't you get a master caution or a chime? Why didn't you get a master caution or a chime?
The fuel system is not connected to the Flight Warning Computer.
Due to redundancy, loss of one pump is only level 1 caution.
Inner tank pump failures never trigger a warning because the fuel can be used by gravity feeding.
You You are are in in cruise cruise and and according according to to those those indications, indications, aa failure failure occurred occurred in in the the fuel fuel system. system. Why didn't you get a master caution or a chime? Why didn't you get a master caution or a chime?
The fuel system is not connected to the Flight Warning Computer.
Due to redundancy, loss of one pump is only level 1 caution.
Inner tank pump failures never trigger a warning because the fuel can be used by gravity feeding.
In 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 fuel out out of of the the right right inner inner tank? tank?
Yes, the fuel of this tank is available by gravity feeding.
No, the fuel of this tank is lost.
Yes, the fuel flows via transfer valves to the outer tank.
Yes, the fuel flows via spill valves to the center tank.
In 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 fuel out out of of the the right right inner inner tank? tank?
Yes, the fuel of this tank is available by gravity feeding.
No, the fuel of this tank is lost.
Yes, the fuel flows via transfer valves to the outer tank.
Yes, the fuel flows via spill valves to the center tank.
According According to to this this SD SD FUEL FUEL page page indications, indications, only only the the Center Center Tank Tank Pumps Pumps are are feeding feeding the the engines. engines.
True.
False.
According According to to this this SD SD FUEL FUEL page page indications, indications, only only the the Center Center Tank Tank Pumps Pumps are are feeding feeding the the engines. engines.
True.
False.
According According to to this this FUEL FUEL SD SD page page indications, indications, which which pumps pumps are are feeding feeding the the engines? engines?
The Center Tank Pumps alone.
The Center Tank Pumps and the inner tank pumps.
The inner Tank Pumps alone.
According According to to this this FUEL FUEL SD SD page page indications, indications, which which pumps pumps are are feeding feeding the the engines? engines?
The Center Tank Pumps alone.
The Center Tank Pumps and the inner tank pumps.
The inner Tank Pumps alone.
Why Why has has the the fuel fuel been been transferred transferred from from the the outer outer to to the the inner inner tanks? tanks?
The temperature in the outer tank was too low.
The center tank quantity is 0.
The temperature in the inner tank was too low.
The quantity in the approaching low level.
inner tanks is
Why Why has has the the fuel fuel been been transferred transferred from from the the outer outer to to the the inner inner tanks? tanks?
The temperature in the outer tank was too low.
The center tank quantity is 0.
The temperature in the inner tank was too low.
The quantity in the approaching low level.
inner tanks is
On On the the ECAM ECAM E/WD E/WD page page the the message message REFUELG REFUELG appears appears in in the the MEMO. MEMO. What What does does itit mean? mean?
The aircraft systems are ready to start refueling.
The refueling control panel door is not closed.
Refueling is completed, the required amount of fuel has been pumped into the tanks.
A reminder that you still have to refuel.
On On the the ECAM ECAM E/WD E/WD page page the the message message REFUELG REFUELG appears appears in in the the MEMO. MEMO. What What does does itit mean? mean?
The aircraft systems are ready to start refueling.
The refueling control panel door is not closed.
Refueling is completed, the required amount of fuel has been pumped into the tanks.
A reminder that you still have to refuel.
On amber On this this ECAM ECAM FUEL FUEL SD SD page page what what does does an an amberamber-boxed boxed FOB FOB indication indication mean? mean?
Not all the fuel on board is useable anymore.
The fuel temperature exceeds a limit.
A fuel imbalance has been detected.
A disagreement between fuel measured and fuel entered on the MCDU has been detected.
On amber On this this ECAM ECAM FUEL FUEL SD SD page page what what does does an an amberamber-boxed boxed FOB FOB indication indication mean? mean?
Not all the fuel on board is useable anymore.
The fuel temperature exceeds a limit.
A fuel imbalance has been detected.
A disagreement between fuel measured and fuel entered on the MCDU has been detected.
On On the the ECAM ECAM FUEL FUEL SD SD page page what what does does this this indication indication of of aa Center Center Tank Tank Pump Pump mean? mean?
It is switched on with the Mode SEL pb in MAN and CTR TK pump not supplying fuel.
It is switched on with the Mode SEL pb in AUTO and supplying fuel
It is switched on with the Mode SEL pb in MAN and supplying fuel.
It is switched on with the Mode SEL pb in AUTO but not supplying fuel.
On On the the ECAM ECAM FUEL FUEL SD SD page page what what does does this this indication indication of of aa Center Center Tank Tank Pump Pump mean? mean?
It is switched on with the Mode SEL pb in MAN and CTR TK pump not supplying fuel.
It is switched on with the Mode SEL pb in AUTO and supplying fuel
It is switched on with the Mode SEL pb in MAN and supplying fuel.
It is switched on with the Mode SEL pb in AUTO but not supplying fuel.
This This is is your your ECAM ECAM FUEL FUEL page page after after engine engine shutdown. shutdown. You You notice notice the the transfer transfer valves valves are are open. open. What are your actions to close them? What are your actions to close them?
You have to switch the inner tank pumps off.
You have to push the MODE SEL pb sw to manual.
You have to open and then close the crossfeed valve again.
There are no actions required. The valves will close automatically during the next refueling.
This This is is your your ECAM ECAM FUEL FUEL page page after after engine engine shutdown. shutdown. You You notice notice the the transfer transfer valves valves are are open. open. What are your actions to close them? What are your actions to close them?
You have to switch the inner tank pumps off.
You have to push the MODE SEL pb sw to manual.
You have to open and then close the crossfeed valve again.
There are no actions required. The valves will close automatically during the next refueling.
On On the the ECAM, ECAM, the the message message OUTER OUTER TK TK FUEL FUEL XFRD XFRD appears appears in in the the MEMO. MEMO. What What does does itit mean? mean?
Fuel is transferred from the inner tank to the outer tank.
Fuel is transferred from the outer tank to the inner tank.
Fuel is transferred from the inner tank to the center tank.
Fuel is transferred from the center tank to the inner tank.
On On the the ECAM, ECAM, the the message message OUTER OUTER TK TK FUEL FUEL XFRD XFRD appears appears in in the the MEMO. MEMO. What What does does itit mean? mean?
Fuel is transferred from the inner tank to the outer tank.
Fuel is transferred from the outer tank to the inner tank.
Fuel is transferred from the inner tank to the center tank.
Fuel is transferred from the center tank to the inner tank.
What What is is the the reason reason the the center center tank tank pumps pumps switch switch automatically automatically off off when when the the slats slats are are extended extended for for takeoff? take take-off?
To keep the center of gravity as low as possible.
During taketake-off, the center tank fuel is pumped to the rear to trim the aircraft.
To feed the 2 engines from 2 different sources ( the inner tanks ).
What What is is the the reason reason the the center center tank tank pumps pumps switch switch automatically automatically off off when when the the slats slats are are extended extended for for takeoff? take take-off?
To keep the center of gravity as low as possible.
During taketake-off, the center tank fuel is pumped to the rear to trim the aircraft.
To feed the 2 engines from 2 different sources ( the inner tanks ).
What -off? take What is is the the minimum minimum fuel fuel quantity quantity for for taketake-off?
1000 kg.
1500 kg.
2000 kg.
2500 kg.
What -off? take What is is the the minimum minimum fuel fuel quantity quantity for for taketake-off?
2400 lbs.
3300 lbs.
4700 lbs.
5300 lbs.
The The normal normal pressure pressure for for the the hydraulic hydraulic system system is is 2000 2000 psi psi
True.
False.
What What is is the the normal normal pressure pressure in in the the hydraulic hydraulic system? system?
500 psi
1000 psi
2000 psi
3000 psi
According According to to this this indication, indication, the the BLUE BLUE system system is is powered powered by... by...
The ELEC pump.
The RAT.
The PTU.
Both the GREEN and YELLOW systems. systems.
We We have have completed completed the the procedure procedure for for HYD HYD Y Y RSVR RSVR LO LO AIR AIR PR, PR, what what does does the the YELLOW YELLOW indication indication in in amber mean? amber mean?
YELLOW is amber because ENG 2 is not running.
The ELEC pump has been switched off.
Users connected to the YELLOW system are no longer supplied with hydraulic pressure.
You You get get aa Y Y RSVR RSVR LO LO AIR AIR PR PR message. message. The The first first step step of of the the procedure procedure asks asks you you to to switch switch the PTU off. Why? the PTU off. Why?
Because it is faulty.
You want to unpressurize the BLUE system.
You want to increase the air pressure by isolating the YELLOW system.
You want to avoid the pressurization of the yellow system by the PTU after you switch the ENG 2 pump off.
Which Which statement statement is is true? true?
The GREEN system is supplied by the BLUE system.
The YELLOW system is supplying the BLUE and the GREEN system.
The BLUE and the YELLOW systems are supplying the GREEN system.
The YELLOW system is supplying the GREEN system.
As As part part of of the the cockpit cockpit preparation, preparation, you you must must check check the the hydraulic hydraulic fluid fluid level. level. What What should should the the indication indication look look like? like?
What What is is the the meaning meaning of of the the RAT RAT indication, indication, as as displayed displayed on on this this HYD HYD ECAM ECAM page? page?
The RAT is faulty.
The RAT is deployed.
The RAT is pressurizing the BLUE system.
What What is is the the correct correct PTU PTU indication indication ifif itit is is delivering delivering power power to to the the GREEN GREEN system? system?
On On the the ECAM ECAM BLEED BLEED SD SD page, page, what what is is the the normal normal indication -ICE on? ANTI indication in in flight flight with with WING WING ANTIANTI-ICE on?
You …. indications You are are in in flight. flight. According According to to these these indications… indications….
The right wing antianti-ice valve failed to open.
The left wing antianti-ice valve failed to close.
Both wing antianti-ice valves failed to open.
Both wing antianti-ice valves failed to close.
In In flight flight the the ECAM ECAM SD SD page page displays displays the the following following indications. indications. What What does does itit mean? mean?
The right wing antianti-ice valve failed to open.
The left wing antianti-ice valve failed to close.
Both wing antianti-ice valves failed to open.
Both wing antianti-ice valves failed to close.
Concerning Concerning the the PROBE/WINDOW PROBE/WINDOW HEAT HEAT pb, pb, which which one one of of the the following following statements statements is is true? true?
When pushed on after taketake-off, the windows are heated only when necessary.
When in AUTO mode, the windows are only heated on ground.
When pushed on, window heating will perform a 30 seconds test on ground and then switch off until taketake-off.
When pushed prior to engine start, the windows are manually heated.
Which Which sources sources are are used used for for ice ice and and rain rain protection? protection?
Electrical heating only.
Hot air only.
Electrical heating and warm air from the cabin.
Electrical heating and hot air.
IfIf one -ice system anti one engine engine antianti-ice system fails, fails, the the second second one one takes -icing for anti takes over over and and provides provides antianti-icing for both both engines. engines.
True.
False.
When When flying flying in in icing icing conditions, conditions, what what will will be be the the correct correct ECAM ECAM BLEED BLEED system system page page indication indication with with both -ice systems anti both WING WING and and ENG ENG antianti-ice systems ON? ON?
In In flight, flight, after after switching switching wing wing Anti Anti Icing Icing System System ON, ON, the WING A.ICE the ECAM ECAM E/WD E/WD page page displays displays ““WING A.ICE SYS SYS FAULT” ”. What FAULT FAULT”. What does does itit mean? mean?
The right wing Anti Ice failed to open.
Both wing Anti Ice failed to open.
Both wing Anti Ice failed to closed.
The left wing Anti Ice failed to OPEN.
In -Ice Anti In case case of of Icing Icing condition, condition, the the engine engine AntiAnti-Ice system... system...
Operates only in flight and is fully automatic in case of icing conditions.
Operates automatically after engine start, the pilots can have manual control through the ENG1 and ENG2 antianti-ice pb. pb.
Cannot be used simultaneously with the wing antianti-ice system due to engine limitations.
Is controlled manually by the pilot through the ENG1 and ENG2 antianti-ice pb. pb.
According According to to the the ECAM ECAM Memo Memo Page Page these these indications indications mean: mean:
The ENG A.ICE system is inoperative.
The ENG A.ICE has automatically started without any crew action.
Because of ice detection, the system asks the pilot to switch the A.ICE system on.
At least one ENG A.ICE switch is in the ON position.
After After aa disagreement disagreement on on landing landing gear gear position, position, you you have recycled the L/G but there are still indications have recycled the L/G but there are still indications as as shown. shown. How How do do you you perform perform the the next next ECAM ECAM action? action?
According to the procedure L/G GRAVITY EXTENSION which is found in the Quick Reference Hand book (QRH).
Recycle the L/G a second time. This time the gear will free fall automatically.
Pull the GRAVITY GEAR EXTN handcrank and turn it clockwise 3 turns.
Pull the GRAVITY GEAR EXTN handcrank and turn it counterclockwise 3 turns.
After After aa disagreement disagreement on on landing landing gear gear position, position, you you have performed the L/G GRAVITY EXTENSION have performed the L/G GRAVITY EXTENSION procedure. procedure. According According to to these these indications, indications, which which statement statement is is true true ??
The gear is in the downlock position.
The gear is down but not locked.
After GRAVITY EXTENSION the gear indications on the ECAM WHEEL page are not reliable.
You You perform perform aa landing landing with with AUTO/BRK AUTO/BRK selected selected to to MED. MED. After After touch touch down down you you observe observe the the following following indications. indications. At At this this moment, moment, which which statement statement is is true true ??
The ANTI/SKID system is increasing brake pressure for wheels 2 and 4.
The ANTI/SKID system is releasing brake pressure for wheels 2 and 4.
The ANTI/SKID system for wheels 1 and 3 is inoperative.
The AUTO/BRK is applying pressure to brake 2 and 4 only.
You You have have just just set set the the parking parking brake brake handle handle to to ON. ON. Which Which indication indication CONFIRMS CONFIRMS that that the the parking parking brake brake is is actually actually set set ??
PARK PARK BRK BRK
On NW STRG ” DISC On this this E/WD, E/WD, what what does does the the ““NW STRG DISC” DISC” memo memo mean? mean?
The nose wheel steering has been disconnected by ground personnel.
A failure in the nose wheel steering system has been detected.
One of the pilots has pushed the PEDALS DISC pushbutton located on the steering handwheel. handwheel.
The nose wheel steering computer has finished it’ it’s self test. Nose wheel steering is now available.
PARK BRK NW STRG DISC
During ° 22 is nn° During push push back, back, engine engine n° is started, started, leading leading to to the NW STRG ” memo. DISC the ““NW STRG DISC” DISC” memo. What What is is the the correct correct statement? statement?
The NW STRG disconnect mechanism has failed.
The yellow hydraulic system has build up pressure which might damage the NW STRG system when set to towing position.
The nose wheel steering has been rereconnected by ground personnel. The amber indication will disappear as soon as you start taxi.
The nose wheel steering is still disconnected. The memo has become amber because one engine is running.
NW STRG DISC APU BLEED
After After starting starting to to taxi taxi you you perform perform the the brake brake check. check. While pressing on top of the rudder pedals you While pressing on top of the rudder pedals you feel feel the the airplane airplane decelerating decelerating but but the the BRAKES BRAKES pressure pressure indication indication remains remains 0. 0. Which Which statement statement is is true true ??
The BRAKES pressure indicator has failed.
The indication is normal because the “BRAKES” BRAKES” press indicator is active on brake system alternate mode (yellow supply).
You must perform the check again and press harder on the brakes until you get an indication.
The indication is normal because with manual braking you are not able to apply enough pressure to be displayed on the BRAKES indicator.
According According to to these these indications, indications, the the AUTO/BRAKE AUTO/BRAKE is is active. active.
True.
False.
What What is is the the meaning meaning of of the the 22 triangles, triangles, appearing appearing below below each each landing landing gear, gear, on on the the WHEEL WHEEL ECAM ECAM page? page?
Each triangle represents one tire.
There are two computers providing information on the gear position. Each triangle represents the position detected by its associated computer.
Each triangle represents one braking system (normal/alternate) available for the associated gear.
The front triangle indicates that AUTO/BRK is available and the one in the back means that ANTI/SKID is available for that gear.
You You have have just just set set the the L/G L/G selector selector to to the the DOWN DOWN position. position. According According to to these these indications... indications...
The L/G is locked. The L/G doors are jammed open.
The computers providing gear position information have failed.
The L/G is up and not locked in the selected position. The L/G doors are open
The L/G computer has failed. The gear will not extend.
How How do do you you interpret interpret the the following following indications? indications?
The nose gear is in transit.
All gears are down and locked.
One L/G control system is inoperative. The nose landing gear is not downlocked. downlocked.
The nose gear is down and locked. The nose gear doors are open.
What What is is the the meaning meaning of of the the green green arc arc appearing appearing over over wheel wheel #2? #2?
It marks the hottest brake with a temperature of more than 100 º Celsius.
It indicates an abnormal high temperature.
The ANTI/SKID system is automatically releasing the pressure of that brake.
The L/G control system has detected a low tire profile.
The The pilot pilot flying flying asks asks you you to to perform perform ECAM ECAM actions. actions. What What are are your your actions actions according according to to the the first first line line of of the ECAM procedure ? the ECAM procedure ?
I must put the L/G selector to the UP position.
The system is trying to recycle the gear automatically. I must wait until the first line disappears.
I must put the L/G selector to the UP position and immediately to the DOWN position again.
I must put the L/G selector to the UP position, wait until the gear has retracted, and then to the DOWN position again.
During -around, you walk During your your walkwalk-around, you see see that that one one light light needs needs aa new new bulb. bulb. What What is is the the purpose purpose of of this this light? light?
Landing light.
RWY turnoff light.
T/O light.
Taxi light.
Where Where is is the the location location of of the the exterior exterior light light panel? panel?
Where Where are are the the controls controls for for the the seat seat belts belts and and no no smoking smoking signs signs located? located?
On On the the EXT EXT LT LT control control panel, panel, the the STROBE STROBE light light selector selector is is set set to to AUTO. AUTO. In In this this position, position, when when do do they stop flashing? they stop flashing?
When the aircraft touches down.
When the first reverser is opened.
When the landing lights are switched off.
When the last engine has been shut down.
According According to to these these panels, panels, which which lights lights are are actually actually illuminated? illuminated?
STROBE, BEACON, NAV, LAND, T.O. and RWY TURN OFF lights.
NAV, BEACON, T.O. and LAND lights.
BEACON,LAND, STROBE, T.O. and NAV lights.
STROBE, BEACON, NAV and LAND lights.
Which Which of of these these buttons buttons control control IR IR and and ADR? ADR?
On On the the ND. ND. What What does does the the MAN MAN indication indication mean? mean?
It is an indication that at least one navaid has been manually tuned.
It is an indication that the WX RADAR Tilt has been manually adjusted.
It is an indication that the WX RADAR Gain has been manually adjusted. MAN
What What is is the the meaning meaning of of the the magenta magenta color color of of some some radar radar returns? returns?
Mountains.
Turbulences.
Water.
What What is is the the meaning meaning of of the the black black color color on on the the radar radar image? image?
Mountains.
Turbulences.
No precipitations or water.
On On the the GNADIRS GNADIRS control control panel, panel, during during the the IRS IRS alignment, alignment, the the ALIGN ALIGN lights lights start start flashing. flashing. What What is is wrong? wrong?
System discovered a discrepancy between the position in the database and the position entered on the MCDU.
At least one of the IR lost the NAV capability.
The system is performing a test before the final alignment.
The alignment process stopped at 1 minute of the end and is waiting for the coordinates to be inserted.
Between Between the the ND ND and and MCDU MCDU you you are are performing performing aa NAV NAV ACCUR ACCUR check. check. Does Does itit satisfy satisfy you? you?
Yes, raw data and FMGS position are the same or the difference is within acceptable limits.
No, there is a major discrepancy between raw data and FMGS positions.
No, the accuracy is displayed LOW on the MCDU PROG page.
One One of of the the IR IR has has an an attitude attitude problem. problem. Please Please perform perform the the correct correct action. action.
On On the the GNADIRS GNADIRS control control panel, panel, what what is is the the position position for for the the DATA DATA selector selector to to see see the the remaining remaining time time for for alignment? alignment?
PPOS.
HDG.
ALIGN
STS.
TEST.
ALIGN
ALIGN
What What does does the the indication indication TTN TTN 10 10 on on the the GNADIRS GNADIRS panel panel mean? mean?
It is an indication that IR3 has calculated a heading of 10 degrees to True North.
It is an indication that it will take 10 minutes to complete the alignment.
ALIGN
It is an indication that the heading calculated by IR3 differs by 10 degrees from the average.
It is an indication that the time to the next waypoint is 10 minutes.
ALIGN
ALIGN
An 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 2. 2.
PFD 1 and ND 1.
PFD 2 and ND 2.
PFD 1 and ND 2.
PFD 2 and ND 1.
Is Is itit possible possible to to get get information information about about ILS ILS 22 on on the the CAPT CAPT side? side?
Yes, on the PFD 1.
Yes, on the ND 1.
No, it is not possible.
Which -aids are Nav Which NavNav-aids are displayed displayed on on the the DDRMI? DDRMI?
VOR 1 and VOR 2.
ADF 1 and ADF 2.
VOR 1 and ADF 2.
VOR 2 and ADF 1.
Please Please indicate indicate the the location location of of the the GPWS GPWS panel. panel.
Please Please indicate indicate the the location location of of the the ATC ATC and and TCAS TCAS panel. panel.
Which Which situation situation corresponds corresponds to to the the WX WX RADAR RADAR settings? settings?
What What is is the the appropriate appropriate ECAM ECAM page page to to get get information information about about the the oxygen oxygen system? system?
In In case case of of an an ECAM ECAM procedure procedure calling calling for for aa Manual Manual deployment deployment of of the the masks, masks, indicate indicate which which control control pb pb has to be pressed. has to be pressed.
On On the the passenger passenger OXYGEN OXYGEN control control panel, panel, which which indication indication confirms confirms the the deployment deployment of of the the masks? masks?
On On the the crew crew OXYGEN OXYGEN MASK MASK Regulator Regulator Panel, Panel, which which statement statement best best reflects reflects the the function function of of the the N/100% N/100% supply supply selector? selector?
The 100% position provides the maximum pressure, N provides the normal pressure, which is lower.
The N position provides an air/oxygen mixture, 100% delivers pure oxygen.
N position cuts the oxygen supply, 100% position enables normal oxygen supply.
The N/100% selector is to be used during the preflight check to check the oxygen supply to the mask.
The The cockpit cockpit CREW CREW OXYGEN OXYGEN being being operative, operative, which which pb pb has has to to be be pressed pressed to to switch switch the the system system OFF? OFF?
After After switching switching the the cockpit cockpit CREW CREW OXYGEN OXYGEN OFF, OFF, which which ECAM ECAM indication indication would would you you see? see?
On On the the ECAM ECAM control control panel, panel, please please select select the the appropriate appropriate ECAM ECAM page page to to get get information information about about the PNEUMATIC system. the PNEUMATIC system.
Both Both engines engines are are running running and and APU APU BLEED BLEED has has been been switched switched OFF. OFF. Is Is the the ECAM ECAM BLEED BLEED page page display display correct correct ??
No, APU bleed closed, but X bleed valve has to stay open.
No, the crew should select X bleed valve selector to (shut) position to close the valve manually after one engine is started.
No, IP HP valves should be closed.
Yes, all the indications are correct, HP valves open because of high air demand with engine at low RPM.
An An ENG ENG 11 BLEED BLEED fault fault has has occurred occurred and and is is indicated indicated by by the the related related ECAM ECAM E/WD E/WD failure failure message. message.
The ENG 1 BLEED valve has been automatically closed.
The left hand Bleed can’ can’t be recovered.
APU bleed can never supply the left side.
On BLEED” BLEED” page On ground, ground, on on the the ECAM ECAM SD SD ““BLEED” page the the GND GND symbol symbol is is always always displayed. displayed.
True.
False.
According According to to the the ECAM ECAM BLEED BLEED page page message message and and ““AIR AIR COND” ” control COND COND” control panel panel indications. indications.
The engines are running and supplying bleed air.
The engines are not running, the APU is supplying bleed air.
The engines are running, the APU is supplying bleed air.
The engines are not running, a GND HP air unit is supplying bleed air.
After After starting starting both both engines engines and and according according to to those those AIR AIR COND COND panel panel and and ECAM ECAM BLEED BLEED page page indications, indications, which which source(s) source(s) provide provide the the bleed bleed air? air?
The engines.
The APU.
The engines and the APU together.
What What is is the the engine engine power power according according to to this this ECAM ECAM indication? indication?
At or close to taketake-off power.
The engines are not running.
At or slightly above idle power.
According According to to the the present present AIR AIR COND COND control control panel panel switch positions and ECAM BLEED page switch positions and ECAM BLEED page indications, indications, which which source(s) source(s) will will supply supply bleed bleed air air when the APU BLEED pb is pressed. when the APU BLEED pb is pressed.
The APU supplies both sides of the system.
The APU supplies the left side of the system only.
The APU supplies left side and engine 2 the right side of the system.
There will be no bleed air supplied.
The The APU APU BLEED BLEED pb pb has has just just been been switched switched ON. ON. On On the the ECAM ECAM BLEED BLEED page page what what do do the the related related indications mean? indications mean?
The X BLEED valve has failed to open.
The X BLEED valve has failed to close.
The X BLEED valve is in transit.
The X BLEED valve is open.
Following Following an an ENG ENG 11 BLEED BLEED fault, fault, the the ECAM ECAM E/WD E/WD procedure has been applied; on the ECAM status procedure has been applied; on the ECAM status page page how how do do we we interpret interpret the the STATUS STATUS information information message in green? message in green?
One pack has been automatically switched off because one ENG BLEED system cannot supply WAI and 2 packs.
One pack has to be switched OFF if WING ANTI ICE (WAI) is used because one ENG BLEED system cannot supply WAI and 2 packs together.
If WAI, has to be used, the X BLEED valve is automatically closed. Therefore, pack 1 will no longer be supplied.
What What is is the the normal normal APU APU Fire Fire extinguisher extinguisher overpressure overpressure indication, indication, and and how how do do you you interpret interpret it? it?
A red disc, which means the APU FIRE EXTING BOTTLE has been discharged due to an APU fire.
A pressure gage visible from outside which indicates the bottle pressure.
A green disc, which means the bottle pressure is normal.
A red disc, which means the APU FIRE EXTING BOTTLE has not been discharged overboard.
To To use use the the APU APU bleed bleed system, system, the the crew crew will will select: select:
The APU BLEED pb on AIR COND overhead panel.
The bleed rotary selector on AIR COND overhead panel.
The ENG1 and ENG2 BLEED pbs. pbs.
This is an automatic sequence initiated when second or Eng starting is selected.
The The APU APU provides: provides:
On ground and in flight, electric power for the aircraft electric system and bleed air for engine start.
Bleed air for engine start on ground and air conditioning in flight only.
Electric Power only for electric system on ground and in flight.
- On ground: bleed air for engine start - On ground and in flight: electric power and bleed air for air conditioning.
The The Electric Electric Power Power supplied supplied from from the the APU APU generator generator is is
Available as soon as APU is running, even if APU GEN is not selected ON.
Only available if the ground External Power is already connected to the a/c Electric network .
Available as soon as engines are shut down.
Available when APU is running, APU GEN is ON and EXT PWR is not ON.
You You have have just just set set the the APU APU MASTER MASTER SW SW to to OFF. OFF. You You notice notice you you still still have have APU APU AVAIL AVAIL indications. indications. What What is is the the reason reason for for that that ??
The APU has shut down but the AIR INLET FLAP is not fully closed yet.
The APU is still running. It is in the cool down period because you have used APU bleed before.
The APU is still running because it always needs a cool down period after the APU MASTER SW has been switched off.
The APU is still running. You have to push the START SW to initiate the shut down sequence.
After After the the engines engines have have been been switched switched off, off, you you realize that there is no external power available. realize that there is no external power available. According According to to the the indications indications can can you you still still interrupt interrupt the APU shut down sequence? the APU shut down sequence?
No, I have to wait until the APU AIR INLET FLAP is fully closed and then start the APU again.
Yes, I simply push the APU MASTER SW back to ON.
Yes, I simply push the APU START switch to ON.
No, I have to wait until the AVAIL indications disappear and then start the APU again.
Which Which ECAM ECAM APU APU page page corresponds corresponds to to these these indications indications on on the the overhead overhead panel panel ??
You You are are attempting attempting to to start start the the APU. APU. After 20 seconds you get the following After 20 seconds you get the following indications indications that ’t get didn that you you didn’ didn’t get during during the the last last APU APU start. start. Can Can you you continue continue the the APU APU start? start?
No. A low oil level has been detected and any start attempt will damage the APU.
Yes, you simple have to wait 20 sec until the LOW OIL LEVEL advisory disappears and then go ahead with the APU start.
Any start attempt with a detected LOW OIL LEVEL will lead to an AUTO SHUTDOWN to prevent the APU to be damaged.
Yes. The APU will run for another 60 hours after the LOW OIL LEVEL has been detected.
After After engine engine shut shut down, down, APU APU running running but but APU APU bleed bleed has has not not been been used, used, when when you you select select APU APU MASTER MASTER SW SW pb pb off. off.
The APU will keep on running to cool down and then shutdown.
The APU will shutdown right away.
APU will shutdown only if external power is connected.
Nothing happen because air conditioning is selected on.
In In flight flight APU APU starting starting limitation limitation is is
15 000 ft
39 000 ft
20 000 ft
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) 39 000 39 000
25 25 000 000
15 000 ft
20 000 ft
25 000 ft
39 000 ft
20 20 000 000 15 15 000 000
According According to to the the ECAM ECAM APU APU page page indications indications ::
The APU is running and available. It is providing bleed air and electrical power.
The APU is running and available. It is providing bleed air only.
The APU is running and available. It is providing electrical power only.
The APU is running and available . It is providing neither electrical power nor bleed air.
On On the the ground, ground, during during APU APU start, start, the the master master caution and single chime come ON and caution and single chime come ON and you you notice notice on ’t exceed won on the the ECAM, ECAM, that that the the APU APU won’ won’t exceed 53% 53% N1. N1. Which statement is true? Which statement is true?
An APU AUTO SHUT DOWN will occur because of APU failure to reach 90% N1.
You have to abort the start by pushing the APU MASTER SW to off.
An APU EMER SHUT DOWN will occur because APU EGT overheating may cause an APU fire.
The FLAP will remain open after APU shutdown to vent the APU compartment.
You You are are performing performing the the walk walk around around with with the the APU APU running running and and nobody nobody is is in in the the cockpit. cockpit. What What will will happen happen in in case case of of an an APU APU FIRE? FIRE?
An APU EMER shut down will occur and the APU fire bottle will be discharged automatically.
You have to perform the ECAM actions to shut down the APU and extinguish the fire from the cockpit.
An APU AUTO shut down will occur but you have to discharge the APU fire bottle from the cockpit manually.
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.
Please Please indicate indicate the the stowing stowing place place for for the the escape escape ropes. ropes.
On On the the ECAM ECAM DOOR/OXY DOOR/OXY page, page, what what does does an an amber amber door door indication indication mean? mean?
The door is fully open.
The door is fully closed.
The door is unlocked.
The door is inoperative.
According According to to this this indication, indication, the the Cargo Cargo door door is is inoperative. inoperative.
True.
False.
You You have have reached reached the the gate. gate. Somebody Somebody is is about about to to open open the the left left forward forward door door from from the the outside. outside. What What will will happen happen in in this this case? case?
The slide will be deployed.
Nothing. The door can't be open from outside as long as the slide is armed.
Nothing. Opening from outside disarms the slide.
On On the the ECAM ECAM SD SD DOOR/OXY DOOR/OXY page page this this indication indication means. means.
Overwing exits and right rear door slides are armed, left forward cabin door and forward cargo door indicate a malfunction.
The left forward cabin door and the forward cargo door are unlocked, the overwing exits and the right rear door slides are armed.
The left forward cabin door and the forward cargo door are unlocked, the overwing exits and the right rear door slides are not armed.
Overwing exits and right rear door slides are not armed, left forward cabin door and forward cargo door indicating a malfunction.
You You are are at at the the gate, gate, according according to to this this DOOR/OXY DOOR/OXY ECAM ECAM page, page, the the EMERGENCY EMERGENCY EXITs EXITs are are disarmed. disarmed.
True.
False.
Regarding Regarding engine engine THRUST THRUST LEVERS LEVERS position, position, which which detent(s) -off? detent(s take detent(s)) can can be be used used for for taketake-off?
FULL.
CLIMB and FLEX/MCT.
CLIMB and TO/GA.
FLEX/MCT and TO/GA.
What What is is the the meaning meaning of of an an amber amber FAULT FAULT light light on on the the ENG ENG panel? panel?
It indicates a failure in the automatic start sequence.
It indicates an engine failure.
It indicates a failure in the engine fire extinguishing system.
On On the the ECAM ECAM E/WD E/WD page, page, what what is is the the meaning meaning of of the the amber amber CHK CHK indication? indication?
It is an indication that the EGT of ENG 1 is out of the normal range.
It is an indication of a discrepancy between EGT of ENG1 and ENG2.
C H K
ENG 1 EGT DISCREPANCY
It is an indication of a discrepancy between the digital EGT indication and the value indicated by the needle.
It is an indication of a discrepancy between the value shown on the ECAM and the real value.
On On the the ECAM ECAM E/WD E/WD page, page, what what is is the the meaning meaning of of the the amber amber CHK CHK indication? indication?
It is an indication that the EGT of ENG 1 is out of the normal range.
It is an indication of a discrepancy between EGT of ENG1 and ENG2.
ENG 1 EGT DISCREPANCY
It is an indication of a discrepancy between the digital EGT indication and the value indicated by the needle.
It is an indication of a discrepancy between the value shown on the ECAM and the real value.
You You are are in in the the middle middle of of the the engine engine start start procedure. procedure. Is Is this this an an automatic automatic start start or or aa manual manual start? start?
Automatic.
Manual.
You You are are in in the the middle middle of of the the engine engine start start procedure. procedure. Is Is this this an an automatic automatic start start or or aa manual manual start? start?
Automatic.
Manual.
During During aa manual manual start, start, what what is is the the role role of of the the FADEC? FADEC?
It has a passive monitoring role, the crew has to monitor the start carefully to take corrective actions in case of malfunctions.
There is no difference between automatic and normal start, FADEC monitors and reacts to possible failures during the start sequence.
FADEC does not monitor the manual start at all. All steps and possible corrective actions have to be performed by the pilots.
During During aa manual manual start, start, what what is is the the role role of of the the FADEC? FADEC?
It has a passive monitoring role, the crew has to monitor the start carefully to take corrective actions in case of malfunctions.
There is no difference between automatic and normal start, FADEC monitors and reacts to possible failures during the start sequence.
FADEC does not monitor the manual start at all. All steps and possible corrective actions have to be performed by the pilots.
Which Which step step of of aa manual manual start start is is taken taken over over by by the the FADEC? FADEC?
Ignition start.
Ignition cutcut-out.
Fuel flow start.
Starter engagement.
Which Which step step of of aa manual manual start start is is taken taken over over by by the the FADEC? FADEC?
Ignition start.
Ignition cutcut-out.
Fuel flow start.
Starter engagement.
From From ECAM ECAM E/WD E/WD and and SD SD engine engine pages pages determinate determinate which which step step of of aa manual manual start start is is taken taken over by the FADEC? over by the FADEC?
Starter valve closure.
Starter valve engagement.
Fuel flow start.
Ignition start.
From From ECAM ECAM E/WD E/WD and and SD SD engine engine page page determinate determinate which which step step of of aa manual manual start start is is taken taken over over by by the the FADEC. FADEC.
Starter valve closure.
Starter valve engagement.
Fuel flow start.
Ignition start.
You -off. You ’t have take don You are are about about to to perform perform aa taketake-off. You don’ don’t have inserted inserted aa FLEX FLEX temperature. temperature. Which -off? take Which thrust thrust lever lever detent detent shall shall be be used used for for taketake-off?
FULL.
CLIMB.
FLEX/MCT.
TO/GA.
During During the the automatic automatic start start sequence sequence of of ENG ENG 2, 2, you you notice notice that that only only igniter igniter B B is is powered. powered. Is Is this this normal? normal?
No, normally igniter A is used for the engine start.
No, normally both igniters are used for engine start.
Yes, igniter B is always used for the engine start.
Yes, igniters are used alternatively for engine start, in this case B.
During During the the automatic automatic start start sequence sequence of of ENG ENG 2, 2, you you notice notice that that only only igniter igniter B B is is powered. powered. Is Is this this normal? normal?
No, normally igniter A is used for the engine start.
No, normally both igniters are used for engine start.
Yes, igniter B is always used for the engine start.
Yes, igniters are used alternatively for engine start, in this case B.
You -off with take You are are performing performing aa taketake-off with the the thrust thrust levers levers in in the the FLEX FLEX position. position. Is Is A/THR A/THR now now active? active?
Yes.
No.
You -off with take You are are performing performing aa taketake-off with the the thrust thrust levers levers in in the the FLEX FLEX position. position. Is Is A/THR A/THR now now active? active?
Yes.
No.
You You are are performing performing aa take take off off with with thrust thrust levers levers in in FLEX FLEX position. position. When When does does A/THR A/THR become become active? active?
As soon as the thrust levers are pulled back into the CLIMB position.
As soon as you pass the thrust reduction altitude.
As soon as you engage the autopilot.
As soon as you push the A/THR pb manually on.
You You are are performing performing aa take take off off with with thrust thrust levers levers in in FLEX FLEX position. position. When When does does A/THR A/THR become become active? active?
As soon as the thrust levers are pulled back into the CLIMB position.
As soon as you pass the thrust reduction altitude.
As soon as you engage the autopilot.
As soon as you push the A/THR pb manually on.
You -off with take You are are performing performing aa taketake-off with TOGA TOGA power. power. When When does does the the A/THR A/THR become become active? active?
As soon as the thrust levers are pulled back into the FLEX position.
As soon as you push the A/THR pb manually on.
As soon as you engage the autopilot.
As soon as the thrust levers are pulled back into the CLIMB position.
You -off with take You are are performing performing aa taketake-off with TOGA TOGA power. power. When When does does the the A/THR A/THR become become active? active?
As soon as the thrust levers are pulled back into the FLEX position.
As soon as you push the A/THR pb manually on.
As soon as you engage the autopilot.
As soon as the thrust levers are pulled back into the CLIMB position.
What What does does an an amber amber REV REV indication indication mean? mean?
The reversers are faulty.
The reversers are fully deployed.
The reversers are stuck.
The reversers are unlocked.
What What does does an an amber amber REV REV indication indication mean? mean?
The reversers are faulty.
The reversers are fully deployed.
The reversers are stuck.
The reversers are unlocked.
On On the the ECAM ECAM E/WD, E/WD, with with thrust thrust levers levers reverser reverser to to reverse reverse position. position. What What does does aa green green REV REV indication indication mean? mean?
The reversers are faulty.
The reversers are fully deployed.
The reversers are stuck.
The reversers are unlocked.
On On the the ECAM ECAM E/WD, E/WD, with with thrust thrust levers levers reverser reverser to to reverse reverse position. position. What What does does aa green green REV REV indication indication mean? mean?
The reversers are faulty.
The reversers are fully deployed.
The reversers are stuck.
The reversers are unlocked.
Before Before engine engine starting starting the the Eng Eng FADEC FADEC should should be be energized: energized: which which control control do do you you activate activate in in order order to to energize the FADEC prior to engine start? energize the FADEC prior to engine start?
Before Before engine engine starting starting the the Eng Eng FADEC FADEC should should be be energized: energized: which which control control do do you you activate activate in in order order to to energize the FADEC prior to engine start? energize the FADEC prior to engine start?
During During the the manual manual start start sequence sequence of of ENG ENG 2, 2, you you notice notice that that both both igniters igniters are are powered. powered. Is Is this this normal? normal?
No, normally igniter A is used for the engine start.
Yes, for manual start both igniters are always used.
No, normally igniter B is used for the engine start.
Yes, both igniters are used for every start.
During During the the manual manual start start sequence sequence of of ENG ENG 2, 2, you you notice notice that that both both igniters igniters are are powered. powered. Is Is this this normal? normal?
No, normally igniter A is used for the engine start.
Yes, for manual start both igniters are always used.
No, normally igniter B is used for the engine start.
Yes, both igniters are used for every start.
