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Airbus Pre Test 1 & 2
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Questions in this quiz (101)
1The APU provides
- AAC Power, bleed Air and Blue Hydraulic Pressure
- BAC Power and bleed air
- CAc power only
2APU Bleed pb sw ON. The APU valves opens if N>____% and there is no leak in the APU or in the left side bleed
- A80%
- B85%
- C95%
- D90%
3The PACK FLOW controller is set to NORM and yet the ECAM display shows PACK FLOW to be high. How is this possible?
- AAs no bleed air is available the PACK FLOW valves are spring
loaded to the fully open position - BHI flow is automatically selected regardless of PACK FLOW
selector position because air is only being supplied by the
APU. - CAs the engines are not running the PACK FLOW indicators are
at the position they were selected to at the last shut down. - DWith cold outside air conditions the PACK FLOW is
automatically increased to help increase the cabin temperature.
- AAs no bleed air is available the PACK FLOW valves are spring
4Which statement is correct?
- ADo not use HP ground unit when APU supplies bteed air to
avoid system damage. - BBoth statements are correct
- CDo not use conditioned air simultaneously from packs and LP
ground unil
- ADo not use HP ground unit when APU supplies bteed air to
5When can we have an intermediate configuration in normal operation?
- AThe skin temperature must be below a given threshold.
- BThe aircraft must be on the ground with the thrust levers not at
TIO and the skin temp above a given threshold. - CThe aircraft must be in the air with the thrust levers at TIO and
the skin temperature below a given threshold. - DThe aircraft must be in the air, or on the ground with the thrust
levers at TIO and the skin temp above a given threshold.
6Does the FMGS logic allow the crew to modify the course of an ILS when its frequency is identical to the ILS selected in the F-PLN ?
- Aallows
- Bdoes not allow.
7The pilot arms A/THR on the ground by pushing the A/THR pushbutton on the FCU when the engines are not running or by setting the thrust levers at
the FLX or TOGA detent when the engines are running.- AFalse
- BTrue
8What does the autothrust system do, if it is active:
- AMaintains a specific thrust in THRUST mode
- BControls the aircraft speed or MACH in SPEED/MACH mode.
- CAll answers are correct
- DUses ALPHA FLOOR mode to set maximum thrust when the
aircraft angle of attack exceeds a specific threshold.
9CVR: The last __ of recording are retained.
- A24 hours
- B60 minutes
- C30 minutes
- D2 hours
10What is the purpose of the AUDIO SWITCHING rotary switch?
- AIt enables the crew to change audio reception from headset to
loud speaker and vice-versa. - BIt transfers the audio reception from the ACP 1 to the ACP 2
and vice-versa. - CIf ACP 1 or 2 fails, the crew can switch to the third ACP. On
CAPT 3 position, the captain uses his acoustic equipment and
the third occupanrs ACP. - DIf ACP 1 or 2 fails, the crew can switch to the third ACP. On
F/O 3 position. the copilot uses his acoustic equipment and the
RMP 3.
- AIt enables the crew to change audio reception from headset to
11The SEL indicator on both RMPs comes on amber when a transceiver, normally assciated with one RMP, is tuned by another:
- AVHF3, tuned by RMP3
- BVHF1 , tuned by RMP1
- CVHF 1, tuned by RMP2
- DVHF2, tuned by RMP2
12May you charge the aircraft mobile at all times?
- AYes
- BNo, only on ground.
- CYes, but not during TIO and landing.
13The emergency generation network transfers automatically to the batteries and static inverter, and the system automatically sheds the AC SHED ESS
and DC SHED ESS buses.- ANo
- BYes
14The aircraft has two types of C/Bs:
- AMoni1ored (green), non-monitored (red).
- BMonitored (green), non-monitored (black).
15If you have an APU FIRE which statement is correct?
- AIn the air, an APU EMER shut down will occur and the APU fire
bottle will be discharged automatically. - BOn the ground you have to perform the ECAM actions to shut
down the APU and extinguish the fire from the cockpil - COn the ground an APU AUTO shut down will occur but you
have to discharge the APU fire bottle manually. - DOn the ground, an APU AUTO shut down will occur and the
APU fire bottle will be discharged automatically.
- AIn the air, an APU EMER shut down will occur and the APU fire
16The engine 1 (2) fire is triggered when:
- Aa fire is detected by on loop, followed by the second loop within
maximum 10 seconds - Ba temperature of more than 725 degrees C is detected in the
turbine hot section - Ca fire is detected by both loops or by one loop, the other one
being faulty, or when there is a break in both loops within 5
seconds - Dall three loops detect a fire (fan. pylon and hot section area)
- Aa fire is detected by on loop, followed by the second loop within
17When the engine fire push button is released out which aircraft systems are isolated:
- AFuel Hydraulic and Air Systems
- BFuel, Electricity and Air Systems
- CFuel, Air, Electricity and Hydraulic Systems
18What are the limits for manoeuvre protection:
- A+ 2.5 G to 0 G clean and
+ 1 G to 0 G other configurations - B+ 2.5 G to -1 G clean and
+ 2 G to 0 G other oonftgurations - C- 2.5 G to 2.5 G clean and
+ 2 G to 0 G other configurations
- A+ 2.5 G to 0 G clean and
19Rudder control is electrical for yaw damping and trim.
- ANo
- BYes
20With hydraulic blue system remaining and before landing gear extension, the flight control law in pitch is:
- ADirect
- BAlternate
- CNormal
21The fuel storage is organized as follows:
- AOne center tank, two inner tanks, two outer tanks, two vent
tanks - BTwo center tanks. two inner tanks. two outer tanks. two vent
tanks - CTwo wing tanks, two external tanks, two deaerating tanks, one
fuselage tank - DOne center wing spar tank, two outer tanks, two vent tanks, two
wing bending tanks
- AOne center tank, two inner tanks, two outer tanks, two vent
22The fuel feeding system consists of, among others, the following components:
- AA DC BUS 2 powered APU pump supplied by the right fuel
feed line, two center gravity feed only pumps, one refuel valve - BA DC BUS 1 powered APU pump supplied by the left fuel feed
line, two transfer valves between the inner tanks and the center
tank - CAn AC ESS SHED powered APU pump supplied by the left
fuel feed line, four transfer valves between the outer and inner
wing tanks and one X-FEED valve - DAn AC STAT INV BUS powered APU pump supplied by the
right fuel feed line, four center tank pumps. four wing tank
pumps
- AA DC BUS 2 powered APU pump supplied by the right fuel
23The ECAM FUEL page displays the fuel temperature value for:
- AThe outer tank only
- BThe outer & inner tanks
- CThe inner & center tanks
- DThe center tank only
24If blue system is lost, the slats operation is:
- AHalf speed.
- BLost.
- CNormal.
25What is powered by the green hydraulic system?
- ANormal brakes, Slats and Flaps, Wing tip brakes and Stabilizer
- BNWS, Alternate brake system, Reverser ENG 2 and Stabilizer
- CCargo Doors, Ram Air Turbine, Copilot's seat and the Landing
gear - DRudder, Emergency generator, Slats . Land R Elevator
26On ground, with the blue elecbic pump PB in AUTO, the circuit is energized if:
- AOne battery is on auto.
- BOne engine is running or BLUE PUMP OVRD PB has been
pressed. - CGround electrical power is on.
27The electric wipers are controlled by two individual rotary selectors:
- AFalse
- BTrue
28The maximum speed to use the windshield wipers is:
- A230 kts
- B250 kts
- C200 kts
29The ON light illuminates on the wing anti-ice pushbutton:
- AWhen the fault light goes out.
- BWhen the push button switch is set to on.
- CWhen the anti-ice valves open and pneumatic PX is available
30If a take-off is aborted just before V1 with auto brake selection MAX but spoilers not armed, the auto brake will:
- ANot be activated
- BBecome active when at least one thrust lever is set to reverse,
and the other at or near idle - CBecome active when both thrust levers are set to idle
31The landing gear can be extended by:
- Athe blue and green hydraulic system
- Bthe green and yellow hydraulic system
- Cthe green hydraulic system or gravity
32When both handwheels are operated simultaneously, the signals:
- AAre added algebraically.
- BComing from the captain have priority.
- CFrom the first pilot acting on his handwheel have priority.
33Where are the beacon lights located?
- AOne on the landing gear and one on the vertical stabilizer
- BOne on each wing tip
- COne on top of the fuselage and one below the fuselage
34Will the FLOOR PROX MARKING batteries be charged when the EMER EXIT LT switch is set to ON?
- ANo
- BYes, but only in flight
- CYes, but only on ground
35The RWY Tumoff Lights:
- Aremain on during the flight
- Bgo off automatically upon liftoff
- Care located at the nosewheel gear
- Dare installed below each wing
36The ADIRU is supplied by: ADIRU 1: CAPT probes I ADIRU 2: F/O probes I ADIRU 3: STBY probes and CAPT TAT.
- AFalse
- BTrue
37Does turning OFF the ADR also tum OFF the IR?
- AYes
- BOnly if the IR is running faulty
- CNo
- DOnly partially
38Normally the CAPT PFD displays the RA1 height and the F/O PFD displays the RA2 height. If either radio altimeter fails:
- ABoth PFDs display the height from the remaining one.
- BRA readout is lost.
- CThe RA for the serviceable side is displayed.
39The flight crew's portable oxygen system (smoke hood) is serviceable as long as the yellow indicator on the case is not broken. The hood should work
satisfactorily for at least- A15 Min
- B10 Min
- C20 Min
40If the oxygen masks fail to deploy automatically how else can they be deployed?
- AThey cannot be deployed if the automatic system fails.
- BThey can be deplored by pressing the MASK MAN ON pb on
the overhead pane . - CThey can be deployed by the flight attendants using the CIDS
panel. - DThey can be deployed by pressing the PASSENGER SYS ON
pb on the overhead panel.
41The flight crew can not override the automatic control of the cabin oxygen system.
- ATrue
- BFalse
42Each bleed valve is normally:
- APneumatically operated and controlled electrically by the
opposite BMC - BElectrically operated and controlled pneumatically by its
associated BMC - CElectrically operated and controlled pneumatically by the
opposite BMC - DPneumatically operated and controlled electrically by its
associated BMC
- APneumatically operated and controlled electrically by the
43The bleed valve function is to act as:
- AA temperature regulating valve
- BA reverse flow protection valve when the APU is not running
- CA shut off and pressure regulating valve
- DA temperature and pressure regulating valve
44With engines and APU running and APU bleed valve selected on. Select the correct statement:
- AEngine bleed valves close, X-Bleed valve opens, APU bleed
valve opens. - BEngine bleed valves close, X-Bleed valve closes, APU bleed
valve opens. - CEngine bleed valves open. X-Bleed valve opens. APU bleed
valve closes. - DEngine bleed valves open, X-Bleed valves closes, APU bleed
valve opens.
- AEngine bleed valves close, X-Bleed valve opens, APU bleed
45On ground, in case of APU fire, the following happens:
- Athe APU fire warning operate in the cokpit, the APU does not
shut down, the AVAIL light goes out - Bthe APU fire warnings only operate in the cockpit, the AVAIL
light goes out, the APU does not shut down - Ca horn in the nose gear bay sounds, the cross bteed
automatically opens, the APU does not shut down - DAPU fire warnings operate in the cockpi~ the FAULT light in the
MASTER SW lights up, the APU fire extinguisher discharges
- Athe APU fire warning operate in the cokpit, the APU does not
46Bleed air & electrical power are available up to:
- A14.500 ft
- B22500 ft
- C20000 ft
- D25000 ft
47When performing the securing the aircraft checklist and the aircraft is not handed over to Maintenance staff, the APU ...
- A... may be left on or switched off
- B... may be left on, but generator p/b must be in OFF position
- C... must be left on
- D... must be switched off
48When the slide arming lever is in the ARMED position, opening the door from the outside disarms the door and escape slide.
- ATrue
- BFalse
49When the electric pump is operating the FWD or AFT cargo doors, the only other system devices that can operate are braking and engine 2 reverse.
- ATrue
- BFalse
50Opening the door from the outside disarms the door and the escape slide.
- AFalse
- BTrue
51Starter limitations:
- Acooling periode, after 4 start attempts: 20 min
- Bpause between start attempts: 25 s
- C4 consecutive cycles: each lasts a maximum of 3 min
- Dno running engagement of the starter , when N2 is above 20°/o
52Which statement is correct?
- AThe ENG MASTER switch to OFF commands the closing of
the LP and HP fuel shut off valves. - BThe ENG MASTER switch to OFF commands the closing of
the LP fuel shut off valve only. - CThe FIRE HANDLE commands the closing of the LP and HP
fuel shut off valves
- AThe ENG MASTER switch to OFF commands the closing of
53Moving the ENG 1 (ENG2) MASTER switch to OFF directly commands the closing of _______ fuel shut off valves for that engine's fuel
system.- AThe LP and HP
- BThe LP
- CThe HP
54In which cases do you need RAM AIR?
- AFor smoke removal.
- BIf both packs fail.
- CRAM AIR is needed in both mentioned cases.
55When the A/THR is armed for takeoff or go around, the FMA displays 'MAN TOGA' (or 'MAN FLX') in __ to remind the crew that the thrust levers
have been positioned properly.- Acyan
- Bwhite
56The descent profile has a repressurization segment. When necessary, this produces a repressurization rate for the cabin during descent. It is a
function of the destination airport altitude and the selected cabin rate •- A(Defaulted to - 250 feet/min but this can be modified)
- B(Defaulted to - 350 feet/min but this can be modified)
- C(Defaulted to - 150 feet/min but this can be modified)
57If a microphone is in the transmission position for more than _____ , an interrupted tone sounds for 5 seconds, and the transmission is turned
off.- A60 seconds.
- B30 seconds.
- C45 seconds
- D25 seconds
58The vertical flight plan is divided into the following flight phases. Preflight - Takeoff - Climb - Cruise - Descent-Approach - Go Around - Done. All but
preflight and done are associated with speed and altitude profiles.- ATrue
- BFalse
59Which bus is not powerded during EMER ELEC in flight?
- Aboth AC ESS BUS & DC ESS SHED BUS
- BAC ESS BUS
- CDC ESS SHED BUS
- DDC BAT BUS
60On the ground, the CVR is stopped automatically __ after the last engine shutdown.
- A3 minute
- B1 minute
- Cimmediately
- D5 minutes
61The battery fault light illuminates if:
- Athe charging current for the corresponding battery is outside
limits. - BBattery voltage is less then 25V.
- CBattery PB set to off in flighl
- Athe charging current for the corresponding battery is outside
62When engine FIRE PB is released out, the following sequence occurs:
·Silences the aural fire warning- ATrue
- BFalse
63What happens when the GEN 1 pushbutton switch is set to off?
- AThe generator is still energized and line contactor open.
- BThe generator field is de energized and line contactor remains closed
- CThe generator field is de energized and line contactor opens.
64Does "SQUIB• light up on the ENG FIRE Panel, when an engine FIRE PB is popped by the flight crew?
- ANo
- BYes
65The pitch direct law is:
- AAchieved through the THS using manual trim control.
- BA load factor demand with no protection.
- CA direct side stick to elevator relationship with auto trim
operation. - DA direct side stick to elevator relationship.
66During the approach at 600ft AGL, smoke in the avionic bay results in ...
- A... an amber warning on the E/WD
- B... a red warning on the E/WD
- C... no warning on the E/WD
67During the approach at 600ft AGL, smoke in the avionic bay results in ...
- A... an amber warning on the E/WD
- B... a red warning on the E/WD
- C... no warning on the E/WD
68Which statement concerning wingtip brakes is correct:
- AWingtip brakes (WTBs) are activated in case of assymetry,
symmetrical runaway, or uncommanded movement of the
surfaces. They camot be released in flight - BWingtip brakes (WTBs) are activated in case of assymetry,
mechanism overspeed, symmetrical runaway, or
uncommanded movement of the surfaces. They cannot be
released in flight - CWingtip brakes (WTBs) are activated in case of assymetry,
mechanism overspeed, symmetrical runaway, or
uncommanded movement of the surfaces. They can be
released in flight
- AWingtip brakes (WTBs) are activated in case of assymetry,
69Fuel feed sequence. The tanks empty in the following sequence:
- A1. Inner tanks. 2. Center tanks. 3. Outer tanks
- B1. Outer tanks. 2. Inner tanks. 3. Center tank
- C1. Center tank. 2. Inner tanks. 3. Outer tanks
- D1. Center tank. 2. Outer tanks. 3. Inner tanks
70Flight control surfaces are all:
(multiple answers are correct)- AElectrically-controlled.
- BThe stabilizer and rudder can also be mechanically-controlled.
- CHydraulically-activated.
71What is the purpose of the pressure relief sequence valves?
- AAllows to transfer fuel in case of overflow caused by pump
failure - BWhen all pumps are running, the centre tank pumps will deliver
fuel preferentially. - CAllows the transfer from wing tanks to centre tank.
- AAllows to transfer fuel in case of overflow caused by pump
72The blue system operates:
- ASpoilers 2 and 4.
- BSpoilers 1 and 5.
- CSpoilers 3.
73What could be the reason for a half amber box appearing around the FOB value?
- AThe fuel level in the tanks is below 1500 kgs
- BOne of the pressure sensors upstream of the high pressure
fuel pump detected a low pressure condition - CThe displayed quantity is not all usable due to the failure of
both transfer valves or the failure of the center tank pumps - DAll the fuel pumps in one wing outer tank have failed
74With a single hydraulic system failure the flight control law is:
- ANormal
- BAlternate
- CDirect
75An independent air bleed from the high pressure compressor protects each engine nacelle from ice. Air is supplied through a two-position (open and
closed) valve that the flight crew controls with:- ATwo pushbuttons.
- BOne pushbutton.
- CThe valves are controlled automatically
76If blue system is lost, flap operation is:
- ALost
- BNormal
- CHalf Speed
77The windshield heating operates at:
- AHigh level in icing conditions.
Low level in other conditions. - BNormal level in flight
Low level on ground. - CHigh level when above 20,000ft.
Low level below 20,000ft.
- AHigh level in icing conditions.
78On wheel page of ECAM. AUTO BRK is flashing green:
- AAuto brake failure.
- BAuto brake is disengaged (flashing green for 10 seconds).
- CAnti-skid failure.
79Wing anti-ice switch is pushed 'ON', indications on the ECAM BLEED PAGE are:
- A"ANTI-ICE• appears in white on the ECAM BLEED PAGE when
the wing anti-ice pushbutton is depressed. - BThere is no indication on ECAM BLEED PAGE for wing anti-ice
system. - CA magenta triangle appears on the ECAM BLEED PAGE when
the wing anti-ice pushbutton is depressed.
- A"ANTI-ICE• appears in white on the ECAM BLEED PAGE when
80The nose wheel steering is powered:
- ABy electric system.
- BBy hydraulic and electric systems.
- CBy hydraulic system.
81How are the emergency lights supplied during an emergency evacuation?
- ABy DC ESS SHED BUS
- BBy DC ESS BUS
- CBy the internal batteries
- DBy HOT BAT BUS
82Automatic braking is initiated:
- AAt the command for ground spoilers extension
- BAt reverse selection
- CAt anti-skid activation
- DAt strut compression
83Which cockpit light(s) is (are) available with battery power only?
- AOnly the left dome light
- BBoth dome lights
- COnly the right dome light
- DBoth dome lights, but only in DIM position
84Pilots may create via FMGC:
- Anew runways
- Bnew waypoints
- Call answers are correct
- Dnew navaids
85The INTEG LT MAIN PNL and PED knob adjusts the brightness of integral lighting for the main panel and pedestal, and turns it on and off.
- ATrue
- BFalse
86Regarding RA, if time between two consecutive predetermined call outs exceeds a certain threshold, the present height is repeated at regular
intervals.- AThe threshold is 15 seconds above 50 feet -
5 seconds below 50 feet - BThe threshold is 10 seconds above 50 feet -
5 seconds below 50 feet - CThe threshold is 11 seconds above 50 feet -
4 seconds below 50 feet
- AThe threshold is 15 seconds above 50 feet -
87The fixed oxygen generation system for the cabin provides oxygen under positive pressure for about:
- A17 minutes.
- B15 minutes.
- C22 minutes.
88When stowing the crew oxygen mask, when will the integrated microphone be deactivated automatically?
- AAfter closing the left flap of the oxygen mask door and having
presed the RESET button - BThe microphone is not deactivated
- CAfter closing the oxygen mask doors
- DAfter pressing the test button on the mask
- AAfter closing the left flap of the oxygen mask door and having
89ND Indications: A ___ white range ring is displayed when a 10 or 20 NM range is selected.
- A7.5 NM
- B2.5 NM
- C5.0 NM
90Which system controls and monitors the operation of the pneumatic system?
- AOne Bleed Control Computer BCC
- BThe Flight Warning Computer FWC
- CTwo Cabin Pressurization Computers CPC1 and CPC 2
- DTwo Bleed Monitoring Computers BMC 1 and BMC2
91OVHD Panel: The PASSENGER SYS ON light comes on ___ when the control for the oxygen mask doors is activated.
- AWhite
- BBlue
- CAmber
92Which statement is correct concerning the APU fuel feed system?
- Aif pressure is not available (batteries only or pumps off) the
APU FUEL PUMP starts automatically - Bthe right fuel feed line supplies the APU
- Cthe autonomous DFCU (digital fuel control unit) controls the
fuel flow - Dabove FL 150, only gravity fuel feeding to the APU is available
- Aif pressure is not available (batteries only or pumps off) the
93The ENG BLEED LEAK caution comes ON at:
- AA temperature of> 165°
- BA temperature of > 204 °
- CA temperature of> 185°
- DA temperature of > 234 °
94Bleed air extraction from the APU for wing anti-icing is:
- APermitted
- Bnot permitted
95The two sliding windows in the cockpit are flight crew emergency exits. The cockpit windows can be opened from the inside or from the outside.
- AFalse
- BTrue
96APU battery start is possible up to ?
- A35.000ft
- BOn ground only
- C20.000 ft
- D25000 ft
97During engine start sequence the gray background on N2 disappears at about 50%. What does this indicate?
- AThat the start valve air pressure has dropped.
- BThat there is a start fault and a dry crank is in progress.
- CThat the start sequence has finished and all engine parameters
have stabilized. - DThat the lgniters are no longer being powered.
98The aircraft is equipped with plug-type doors that open outward and forward.
- AThere are two entry doors, one forward and one aft on the port
(left) side. The doors located on the starboard (right) side are
for emergency use only. - BThere are two on each side of the fuselage (two forward and
two aft). - CThere are three on each side of the fuselage (two forwardt two
mid and two aft}.
- AThere are two entry doors, one forward and one aft on the port
99During the automatic start sequence of ENG 2, you notice that only igniter Bis powered. Is this normal?
- AYes, igniter A is only used for engine anti Ice.
- BYes, igniters are used alternately for engine start.
- CYes, igniter B is always used for ENG 2 start.
- DNo, normally both igniters are used for all engine starts.
100To prepare for ditching, the flight crew must press the DITCHING pushbutton on the CABIN PRESS control panel to close the outflow valve. the
emergency ram air inlet, the avionics ventilation inlet and extract valves, and the pack flow control valve.- ATrue
- BFalse
101Under what conditions should the pack flow controller be set to HI ?
- AWith a low passenger load to increase cabin air flow.
- BWith a high passenger load in hot conditions in order to help
reduce the cabin temperature. - CIn cold conditions to achieve a higher cabin temperature range.
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- Quiz on Airbus Pre Test 1 & 2, created by akoenitz on 25/03/2015.
- Author
- akoenitz
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