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CAAV QUESTION BANK A320/321- LEVEL A

ATA06 DIMENSION AND AREAS

1. The A320/A321 aircraft is divided into ones as fo!!o"s#

A. The major zones, the major sub-zones, the zones.

B. The zones and sub-zones.

C. The zones and the station.

D. The major zones, the major sub-zones

3. Each $a%or one is identified &'#

A. Three digit number and two letters

B. Three digit number

C. The first digit of three digit number

(. Access doors and )ane!s are identified &'#

A. The number of the zone in which the panel is located followed by a two-letter

suffi.

B. The number of the zone in which the panel is located followed by one letter suffi.

C. a two-letter followed by the number of the zone in which the panel is located suffi.

*. There are ho" $an' $a%or ones in the aircraft+

A. !

B. "

C. #

D. $%

ATA 0, - ITIN SORIN

6. The Tai! Safet' sta' is sed to#

A. &hare load with the main jac's during jac'ing process

B. (eep the aircraft more stable during landing gear retraction) etension tests

C. (eep the aircraft stable on jac's

,. o" $an' )oints on the strctre are desi4nated for the )r)ose of !iftin4 the

aircraft+

A. *

B. !

C. +

5. hat is )er$issi&!e drin4 %ac7in4 for $ain D "hee! chan4e+A. Cargo, A loading.

B. ate doc'ing.

C. /nstallation of the wheel choc's on the wheels of the other main 0D.

ATA05 E8EIN AND EIIN

9. The $ain )r)ose of "ei4hin4 aircraft is#

A. Calculate the position of the center of gra1ity

B. Calculate of aircraft weight

C. (now the aircraft weight for passenger loading

10. hen iftin4 the AIR:RAT for !eve!in4

A. 2ou must not lift the aircraft with the safety stay.

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B. The weight of fuel is applied e3ually on the two side of the aircraft centerline

C. 4a'e sure that the aircraft is stable before you lift it with jac's

D. All abo1e

11. hen iftin4 the aircraft

A. All the doors must be closed and loc'ed.

B. assenger)crew door may be fully opened and loc'ed but the cargo doors must beclosed and loc'ed.

C. The passenger)crew doors, the emergency eits and the cargo doors are closed and

loc'ed or fully open and loc'ed.

D. 5o re3uirement.

ATA 09 ; TOIN TAence+

A. /nstall the tow bar on the tow fitting then install the tow le1er safety pin

B. /nstall the tow le1er safety pin then install the tow bar on the tow fitting.

C. There is no specific se3uence

19. :o$$nication s'ste$?s@ to &e sed drin4 to"in4 is ?are@+A. and >0T /5T.

B. or => with >0T /5T.

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C. only.

20. hat indication on E:AM do 'o have to chec7 )rior to start to"in4+

A. 5 ?=660 &T66@ D/&C

B. 5 ?=660 &T66@ /5

C. 5 ?=660 &T66@ >>

21. ro$ coc7)it ho" can 'o 7no" that the &ra7e are re!ease )rior to to"in4 the

aircraft+

A. Chec' ar'ing bra'e selector in >>, bra'e pressure indication on 6CA4 is at %

and confirm with 5D personnel.

B. Chec' ar'ing bra'e selector in >> chec' all the %* pointes are at green range

and confirm with 5D personnel.

C. Chec' ar'ing bra'e selector in >> bra'e pressure pointes at % and confirm

with 5D personnel.

22. Mini$$ se)aration fro$ the nose "hee!s and the tractor "hi!e to"in4 the

aircraft is#A.+ m

B.* m.

C.! m.

23. In to"in4 confi4rations the safet' )in !oc7s the contro! !ever on the inter)hone

&o= in#

A. Disengaged position.

B. 6ngaged position.

C. 5ormal position.

2(. hen to"in4 the aircraft#

A. All the doors must be closed and loc'ed.

B. assenger)crew door may be fully opened and loc'ed the cargo doors open in

1ertical position

C. assenger)crew door may be fully opened and loc'ed but the cargo doors must be

closed and loc'ed

ATA12 SER8I:IN

2*. hen 'o do the Aircraft rondin4 for the Refe!/Defe! O)erations

A. Connect the ground cable to par'ing ground point before you connect it to theaircraft

B. Attach the cable to aircraft first then connect to par'ing ground point

C. rounding is not necessary

26. To e!ectrostatica!!' &a!ance the aircraft for the refe!/defe! o)erations

A. Connect a ground cable to the aircraft grounding point on the landing gears

B. Connect a bonding cable between the fuel tan'er and a grounding point on one of

the 40 0egs

C. A is essential, B is recommended

D. B is essential, A is recommended

2,. Safet' re>ire$ents for aircraft Refe!!in4 and defe!!in4 are#

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A. Do not operate the cell phones or mobile phones inside distances for "m from

aircraft.

B. Do not connect electrical e3uipment to a power source less than $: m away from

aircraft, unless the power source has spar'-proof connectors

C. Do not operate the fuel tan'er)pump unit until you stop operation of the weather

radar

D. All abo1e

25. Drin4 aircraft Refe!!in4 or defe!!in4

A. A starts or shutdowns are permitted.

B. An A start is not permitted during if the A has failed to start or an automatic

shutdown has occurred.

C. A B

29. Drin4 the refe!!in4

A. The 50 tires roll aft

B. The 50 tires roll fwd

C. The 50 tires roll does not mo1e

30. Drin4 the refe!!in4 'o $st#

A. 4o1e the aft 50 choc's away from the tires

B. 4a'e sure that the choc's do not touch the 40 tires

C. A B

31. hen 'o do the Refe!!in4 and/or defe!!in4 in the an4ar

A. The hangar doors must be closed until you ha1e completed the refuel)defuel

procedure

B. The hangar doors must not be closed until you ha1e completed the refuel)defuel

procedure

C. There is no re3uirement for hangar door

32. hen 'o do the aircraft )ressre Ato$atic refe!in4 "ith &atter' )o"er

A. /t is not always possible to refuel to full capacity. This is because the intercell

transfer 1al1e are not always in the correct position

B. /t is always possible to refuel to full capacity.

C. 2ou can not refuel in the outer cell.

33. The $a=i$$ safet' )ressre for refe!in4 is#

A. !:psiB. :%psi

C. ::psi

D. "%psi

3(. hen 'o do the aircraft refe!in4 "ith &atter' )o"er

A. The =T B&& is energized for ten minutes only after you put the BATT

?6@ switch to the 5 position.

B. =T B&& is always energized after you put the BATT ?6@ switch to the

5 position.

C. 2ou must put the BATT ?6@ switch to the 5 position and hold it during

refueling process

3*. hen 'o do the aircraft )ressre refe!in4 "ith $ana! contro!

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A. ut the 4D6 &606CT switch to the @6>60 position

B. ut the @6>60 60 ?D, A>T cargo-compartment doors and the landing gear doors are closed

B. The >?D, A>T cargo-compartment doors and the landing gear doors are opened

C. The >?D, A>T cargo-compartment doors are closed and the landing gear doors

are opened

D. The >?D, A>T cargo-compartment doors are opened and the landing gear doors

are closed

3,. hen doin4 the 'dra!ic !id Reservoir i!!in4

A. The hydraulic system operating normallyB. The reser1oirs air pressurize system must be depressurized

C. Do not depressurize the system reser1oirs

D. reen hydraulic system must be depressurized

35. hat ha))en if 'o fi!! to $ch h'dra!ic f!id in the reservoir+

A. =ydraulic system can not operate

B. A message Ereser1oir o1erfullE appear on 6CA4

C. 2ou cannot pressurize it the reser1oir sufficiently and may cause the message

E@&

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(2. In the AMM tas7s ARNIN is $eant#

A. Calls attention to use of materials, processes, methods, procedures or limits which

must be followed precisely to a1oid injury of death to persons

B. Calls attention to methods and procedures which be followed to a1oid damage to

e3uipment

C. Calls attention to methods which ma'e the job easier or pro1ide supplementary or

eplanatory information

(3. In the AMM tas7s :ACTION is $eant#

A. Calls attention to use of materials, processes, methods, procedures or limits which

must be followed precisely to a1oid injury of death to persons


e3uipment



((. In the AMM tas7s NOTE is $eant#

A. Calls attention to use of materials, processes, methods, procedures or limits whichmust be followed precisely to a1oid injury of death to persons


e3uipment



(*. AMM 4ives#

A. The status of the item of e3uipment, semi-e3uipment and related wiring

B. /nformation re3uired for trouble shooting is contained in the manual

C. The information re3uired to ser1ice, repair, replace, adjust, inspect and chec'

e3uipments and systems of the A)C normally performed on the ramp or in the

maintenance hangar

D. &chematic diagrams of the electrical installation with sufficient data for A)C fault

isolation

ATA 21 - AIR :ONDITIONIN

(6. hat is the $ain )r)ose of the )ac7 anti ice va!ve+

A. To stop the ice formation across the primary heat echanger.

B. To stop the ice formation across the main heat echanger.

C. To stop the ice formation across pac' condenser.

(,. hat is the )r)ose of the )ac7 RAM AIR f!a)s+

a. To ensure cabin 1entilation in case both pac's fail.

b. To pro1ide air to the pac' compressor.

c. To modulate the main air flow through the heat echangers.

(5. hat f!o" is de!ivered &' )ac7 "ith Bac7 !o" se!ector on O and &!eed air

s))!ied &' the ABC+

a. 0ow

b. 5ormal

c. =igh

(9. The )r)ose of the safet' va!ves is to avoid #

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A. 6cessi1e positi1e pressure differential

B. 6cessi1e negati1e pressure differential

C. 6cessi1e cabin altitude.

D. A and B

*0. hen does the avionics venti!ation air co$e fro$ "hen an' O8RD se!ected+

A. >rom the a1ionics bayB. >rom outside the aircraft

C. >rom the air conditioning duct

D. 5o 1entilation. &ystem is inoperati1e.

*1. hat is the )r)ose of the avionic venti!ation s7in heat e=chan4er+

A. To cool the air coming from the a1ionics e3uipment when /solation 1al1e is open.

B. To reheat air coming from a1ionics 1entilation system

C. To cool air before it is ducted under the cargo compartment.

ATA-22# ACTO IT SFSTEM

(2.Aircraft on 4rond in order to co$$nicate fro$ the coc7)it to the ABC )osition

'o $st#

A. &elect the /5T on the audio control panel, and press the G&6@< /5TH pushbutton

B. press GCABH transmission 'ey

C. press the G&6@< /5TH pushbutton

D. press GCABH recei1ing 'nob

(3.The !ods)ea7er vo!$e 7no&s a!!o"#

A. Controls the loudness of aural alerts and 1oice messages

B. Controls the loudness of 1oice messages only

C. Adjusts the 1olume of the loudspea'er for radio communication

D. Adjusts the 1olume of the loudspea'er for radio communication , aural alerts and

1oice messages

ATA-2(# EE:TRI:A SFSTEM

((. Maintenance &ses on!' are s))!ied "hen#

A. 6ternal power is connected and blue 5 light on 6T ?@ pushbutton

illuminated 4A/5 B& switch in 5 position

B. 6ternal power is connected and the green A

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A. An immediate A shut down is commanded and the A enerator is denergized

B. The A enerator is disconnected only

C. The A enerator >ault 0ight illuminates only

D. A ?arning 4essage is displayed on 6CA4 only

(,. hat does the Eolding type and has no adjustment

*(. :a)tain and irst Officer Seats e!ectrica! contro! s'ste$ )er$its

A. Control the seats in 1ertical and horizontal direction

B. Control the seats in 1ertical and horizontal direction and adjust the bac'rest

C. Control the seats in 1ertical and horizontal direction and adjust the lumbar restD. All abo1e

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**. The A320 aircraft is fitted "ith e$er4enc' evacation s!ide at#

A. The ! entry doors.

B. The o1erwing eits

C. The ! entry doors and the o1erwing eits

*6.Third Occ)ant seat in the coc7)it

A. Can slide along the 2-ais to ta'e up a position on the aircraft centerlineB. =a1e longitudinal adjustment

C. Can mo1es longitudinally and 1ertically

D. Attached to the left rear panel in the coc'pit

*,.The )assen4er seats

A. &eat pans are upholstered and not foldable or adjustable

B. Can fold the inner armrests between the bac'rests

C. pholstered bac'rest assembly of each seat may be adjusted

D. All abo1e

*5.The Bassen4er Service/Infor$ation Cnits ?BSICs@A. =as two primary unitsI assenger &er1ice nit 7&8 and assenger /nformation

nit 7/8

B. The assenger &er1ice nit 7&8, installed abo1e each seat row

C. The assenger /nformation nit 7/8, installed abo1e each second seat row

D. All abo1e

ATA 26 - IRE BROTE:TION

*9. here are the En4ine fire detectors !ocated+

A. n the >an and the Turbine and ylon

B. n the ylon, the >an and the Core

C. n the Core, earbo and the 5ozzle

60. Is the e=tin4ishin4 s'ste$ contro!!ed &' the DC#

A. 2es, continuously

B. 2es, whene1er engine fire is detected

C. 5o

61. o" is an ABC fire on 4rond nor$a!!' e=tin4ished#

A. >rom A fire panel.

B. >rom A compartmentC. Automatically.

D. >rom eternal power panel.

62. Fo )ress the ABC sht off )sh &tton at 1058C )ane! to+

A. /nitiate the shut down the A with cooling down se3uence.

B. /nitiate the emergency shut down of A without cooling down se3uence.

C. /nitiate the emergency shut down of A and discharge the A fire bottle.

63.To test the ABC ato e=tin4ishin4 fnction 'o $st #

A. &elect A master switch 5.

B. ress the A fire T6&T push button.C. &elect A master switch 5 and press the A fire T6&T push button.

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6(. hat additiona! e=terna! "arnin4 is/ are activated in case of ABC fire on

ROCND+

A. A fire light eternal horn warning.

B. A fire bell warning.

C. An eternal horn warning only.

D. An eternal horn warning @ed dis' indicator disappears.

6*.o" $an' fire e=tin4ishin4 &ott!e?s@ is?are@ )rovided for the car4o

co$)art$ents+

A. ThereJs one for >?D and one for A>T cargo compartment.

B. ThereJs one for both >?D and A>T cargo compartments.

C. 5one.

ATA 25 ; CE SFSTEM

66.A )ressre s"itch for each )$) $onitors a#

A. ressure differential

B. >eed pipe pressurizationC. ressure increase

D. 0oss of pressure

6,.hat ha))en if a hi4h !eve! is detected+

A. A warning is triggeredI too much fuel

B. Booster pumps are not operating correctly

C. The corresponding @6>60 1al1e closes

D. All the refueling operating is stopped

65.Are "in4 )$)s rnnin4 "hi!e center tan7 is s))!'in4+

A. 2es, wing tan' pumps run continuously

B. 5o, only when center tan' is empty

C. 5o, because of center tan' pump priority

D. ne of the two pumps is running in stand-by

69.hen the center tan7 is e$)t' in ato $ode center tan7 )$)s#

A. 4ust be manually switched >>

B. &top and wing tan' pumps start running

C. &top automatically

D. @un for + minutes

,0.Refe! va!ves $a' &e contro!!ed#

A. By refuel pressure

B. 6lectrically only

C. 4anually only

D. 6lectrically or manually

,1.The ABC fe! feed is assred &'#

A. >uel booster pumps only

B. A fuel pump only

C. All pumps together

D. A or B

,2.hat is the $a=i$$ tota! fe! ca)acit' for 8NAHs A320 aircraft+

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A. $+ !;% (

B. $: :## (

C. $# 9*+ (

D. +% #+9 (

,3.In nor$a! o)eration each en4ine is s))!ied &'#

A. ne wing tan' pump and) or one center tan' pumpB. Two wing tan's pumps and) or one center tan' pump

C.Two wing tan's pumps and) or two center tan' pumps

D.ne wing tan' pump and) or two center tan' pumps

,(.Drin4 refe!in4 the "in4 tan7 fi!!s in the fo!!o"in4 order#

A. The uter cell and /nner cell at the same time

B. The /nner cell first, then the uter cell

D. The uter cell first, then the /nner cell

,*.The inner ce!! is refe!ed on!' "hen+

A. Center tan' is full.B. uter cell is full.

C. uter cell is empty.

,6.The $a=i$$ refe! )ressre is+

A. $$ psi

B. !: psi

C. :% psi

,,.The END !i4ht in the refe!/defe! )ane! i!!$inate $eans+

A. re-selected fuel is e3ual to actual fuel.

B. All fuel tan's are full, refuel process stopped automatically.

C. Any high le1el sensor detected fuel.

,5.hen )erfor$in4 the refe! defe! rond transfer the R/D e!ectrica! circit is

ena&!e &'+

A. ower from the aircraft electrical net wor' only.

B. Carrying out =/ 0

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A. The blue system

B. The yellow system

C. The green and yellow systems

D. The blue and yellow systems

52.hat ha))ens if h'dra!ic )ressre dro)s+

A. The priority 1al1es gi1e priority to the hea1y loads users.B. The priority 1al1es gi1e priority to the essential systems

C. The priority 1al1es modulate the pressure to the users

53.A G!e s'ste$ )i)e!ine is identified &'#

A. A blue band and number $.

B. A blue band and number +.

C. A blue band and number *.

5(.hen is the en4ine fire sht off va!ve c!osed+

A. ?hen the engine is shut down

B. Automatically as soon as an engine fire is detected.C. /f the engine fire pushbutton is release out.

5*.hat can the hand )$) &e sed for+

A. To pressurized the reser1oir.

B. To chec' the flight controls

C. To operate the cargo doors

56.Drin4 "hich o)eration is the !ea7 $easre$ent va!ve c!osed ato$atica!!'

A. T operation.

B. Cargo door operation.

C. =and pump operation.

5,.hat are the $ana! de)ressriation va!ves )rovided for+

A. /ndi1idual reser1oir depressurization

B. Depressurization of related hydraulic circuit

C. =ydraulic system depressurization

ATA 30 ; I:E AND RAIN BROTE:TION

55.ot air sed for "in4 anti-iced is ta7en fro$+

A. Aircraft pneumatic system.B. Bleed from either engine $ or +.

C. Directly from the main engine compressors.

59.In the event of an en4ine anti-ice va!ve fai!re+

A. 6ach 1al1e can be deacti1ated in open position.

B. 6ach 1al1e can be deacti1ated in close position.

C. 6ach 1al1e can be deacti1ated either in close or open position.

ATA-32# ANDIN EAR

90.hen does the CN !i4ht co$e on+A. ?hen the gear and the related doors are not loc'ed up.

B. ?hen the gear is not loc'ed down.


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C. ?hen the gear is not loc'ed in the selected position.

91.hat is the nor$a! retraction se>ence+

A. Door open, gear up, door close, cancel gear up signal.

B. Door open, gear up, door close, maintain gear up signal.

C. Door open, gear up, door close, cancel door close signal.

92.o" can the )ar7in4 &ra7e &e h'dra!ica!!' )o"ered+

A. nly by yellow high pressure

B. nly by the bra'e accumulator

C. 6ither by yellow high pressure or by the bra'e accumulator

93.hat is the )r)ose of the h'dra!ic fses+

A. To stop the flow in case of lea'age

B. To shut off the return lines

C. To separate the 5ormal from the Alternate &er1o1al1e.

ATA - 33# ITIN SFSTEM

9(.hich !i4htin4 inc!des f!orescent !a$)s and inte4ra! &a!!ast nits#

A. assenger reading lights and wor' attendant light

B. Cabin light, entrance light and la1atory lights

C. 0a1atory lights sign

D. 6mergency lights sign

9*.The navi4ation !i4hts inc!de#

A. @6D light on the left hand, @665 light on the right hand and ?=/T6 light on the

A tail.

B. @665 light on the left hand, @6D light on the right hand and ?=/T6 light on the

A tail.

C. ?=/T6 light on the left hand, @665 light on the right hand and @6D light on the

A tail.

D. @6D light on the left hand, ?=/T6 light on the right hand and @665 light on the

A tail.

ATA3*# O

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C. A fied cylinder with mas's and a breathing hood system

99.:an the cre" o='4en c'!inder )ressre &e chec7ed "hen there is no e!ectrica!

)o"er+

A. 2es

B. 5o

100.hat indicates an over&oard dischar4e+

A. A warning on the oygen control panel +$ully closed

C. >ully openD. @egulating a temperature

102.here the air is ta7en fro$ drin4 en4ine hi4h )o"er settin4+

A. / stage.

B. = stage.

C. / and = at the same time.

103.hat is the )r)ose of IB/B s"itchin4+

A. To regulate the output pressure depending on the >an Air

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A. By waiting for the system pressure to dissipate

B. By operating a wash basin faucet

C. By operating the fill)o1er flow 1al1e

D. By a push button the ser1icing panel

105.:an an' toi!et &e sed drin4 servicin4+

A. 2es, because toilet use and ser1icing is independentB. 2es, but only the front toilet

C. 2es, but electric power is re3uired to supply the toilet control system

D. 5o, the door limit switch on the toilet ser1icing panel deacti1ates the toilet control

system.

109.Is it )ossi&!e to drain the "ho!e "ater s'ste$ "ithot e!ectrica! )o"er+

A. 5o, electrical power is always re3uired

B. 2es, all the drain 1al1es can be operated manually

C. 5o, only the water tan's can be drained by using the aft drain 1al1e

D. 5o, only the forward drain 1al1e can be operated manually.

(10.h' is "ater tan7 )ressried+

A. To ease draining operation.

B. To warm up water.

C. To allow water distribution.

111.hat is sed for A320 aircraft "ater tan7 fi!!in4 o)eration+

A. ne handle, one 1al1e.

B. Two handles, one 1al1e.

C. ne handle, two 1al1es.

112.o" $an' va!ves are sed drin4 drainin4 o)eration of A320 aircraft "ater tan7

A. Two

B. Three

C. >our

113.o" $an' )ota&!e "ater service and drain )ane!s are fitted to the A320 aircraft+

A. ne

B. Two

C. Three

11(.here is the $ain drain )ort of the A320 aircraft )ota&!e "ater s'ste$+A. n the portable water ser1ice panel.

B. n the fwd ser1ice panel.

C. Both

11*.o" $an' )ota&!e "ater >antit' indicators are there+

A. ne

B. Two

C. Three

116.o" $an' >antit' TRANSMITTER is in the )ota&!e "ater tan7+

A. neB. Two

C. Three


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11,.The "aste "ater drain va!ve.

A. 6lectrically operated.

B. /s held closed in flight by cabin air pressure and open when waste water enters the

1al1e has build up enough.

C. pen on ground and close in flight

D. 4anually operated only by lifting the seal assembly.

115.here does the toi!et &o"! rinsin4 "ater co$e fro$+

A. ?aste holding tan'.

B. ?aste water tan'.

C. otable water tan'.

119.o" is the "aste trans)orted to the "aste ho!din4 tan7+

A. By the 1acuum created in the waste holding tan'.

B. By the water flushing and gra1ity.

C. By the water pressure

120.o" $an' toi!et service )ane!s are fitted on the aircraft+

A. ne

B. Two

C. Three

121.o" $an' )ota&!e "ater service and drain )ane!s are fitted to the aircraft+

A. ne

B. Two

C. Three

122.here is the "aste >antit' dis)!a'ed+

A. n the toilet ser1ice panel

B. n the >orward Attendant anel

C. n both panels.

ATA (9 - ABC.

123.The E.:.G has+

A. @estricted authority o1er A operation.

B. 4onitoring function o1er A operation.

C. >ull authority o1er A operation.

12(.ro$ "here the ABC e$er4enc' sht do"n can &e initiated+

A. @efuel)Defuel panel 6ternal power panel and Coc'pit.

B. 6ternal power panel and Coc'pit only.

C. 6ternal power panel only, if the aircraft is on ground.

12*.hat indication can &e dis)!a'ed on the ABC )a4e+

A. >0A 65.

B. >60 0 @ 0? /0 00A 65 >60 0 @ 0? /0 0

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B. ower section, 0oad Compressor, Turbine.

C. ower section, 0oad Compressor, earbo.

12,.The ABC fe! !o" )ressre circit can &e activated fro$+

A. Coc'pit and 6ternal ower anel.

B. Coc'pit and >uel antit'+

A. n A page, on sight glass located on the gear bo and interrogate the C>D&.

B. n A page, on sight glass located on the gear bo.

C. n A page, on sight glass located on the oil cooler and interrogate the C>D&.

130.The hi4h oi! te$)eratre or !o" oi! )ressre detected drin4 ABC o)eration the

E:G "i!! case the ABC to sht do"n#

A. nly if the 4A&T6@ switch is released

B. nly if the &TA@T pushbutton is released

C. nly after the cool down period has elapsed

D. /mmediately

131.Drin4 coo!in4 do"n se>ence at ,*J N the ABC is#

A. &till running without electrical and pneumatic load.

B. &till running with electrical load.

C. ?ind milling without electrical and pneumatic load.

D. &till running with electrical and pneumatic load.

132.The ABC se!f test is )erfor$ed fro$ the M:DC. this fnction is avai!a&!e on!'#

A. /f the A is running

B. /f the A is not running

C. Doing the A start se3uence

D. /f the &TA@T pushbutton is pressed in

ATA *2# DOOR

133.hat indicates the red f!ashin4 !i4ht on the ca&in door+

A. The escape slide will not deploy after automatic opening

B. The first bar has failed to engage into the floor fittings

C. The slide system is armed a1oid the interior loc'ing handle is partly lifted

D. Both engine shut down, door disarmed, the cabin pressure is greater than +,: mb

13(.o" is the )assen4er door c!osed and !oc7ed infor$ation &e $onitored+

A. By a single microswitch 7loc' position8 on the E6CA4 D@E page

B. By two proimity detection on the E6CA4 D@E page

C. 5o indication at all

D. 0anding gear control interface unit nK $ 70C/ $8 on the E6CA4 D@E page

13*.hat indicates the 4reen !i4ht in the car4o door access+


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A. The cargo door is closed and loc'ed

B. The cargo door is not closed

C. The cargo door is unloc'ed

D. The cargo door is open and loc'ed

136.hat ha))en "hen the )assen4er door is o)ened fro$ the otside and the s!ide

s'ste$ is ar$ed+A. The loc'ing mechanism is bloc'ed

B. The escape slide will deploy

C. The slide system is disarmed

D. There is no possibility to open the door from the outside

13,.hat ha))en "hen the e$er4enc' e=it door of A320 aircraft is o)ened fro$ the

otside and the s!ide s'ste$ is ar$ed+

A. The loc'ing mechanism is bloc'ed




135.The BA< door is $aintained )ara!!e! to the fse!a4e &'#

A. The guide arms.

B. The support arms

C. The upper and lower connection lin's.

139.o" the o)erator is "arned "hen there is a resida! )ressre in the ca&in+

A. By a white flushing light.

B. By a red flushing light.

C. By an ember flushing light.

1(0.hat does the 4reen !i4ht fitted near the $ana! se!ector va!ve of the car4o door

indicate+

A. The yellow hydraulic pressure is a1ailable to operate the door.

B. The door is fully opened and loc'ed.

C. The door is correctly unlatched and unloc'ed

1(1.hen can the car4o door &e o)ened+

A. ?hen the cam and the hoo's are in the loc'ed position.

B. ?hen the cam is in the unloc'ed position and the hoo's are in the loc'ed position

C. ?hen the cam and the hoo's are in the unloc'ed position

1(2.The car4o doors h'dra!ic s'ste$ is )ressried &' the#

A. reen electric pump

G. Blue electric pump

:. 2ellow electric pump

1(3.hen does the resida! ca&in )ressre red !i4ht co$e on+

A. ?hen all the engines are not running, the par'ing bra'e is applied and the residual

cabin pressure eceeds +.: mbars

B. ?hen the engines are not running, the slide is disarmed and the residual cabin

pressure eceeds +.: mbarsC. ?hen the engines are not running, the par'ing bra'e is applied, the slide is disarmed

and the residual cabin pressure eceeds +.: mbars


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1((.The sea! of )a= door#

A. /s installed around the door on the inner side and when the door is closed, the it is

pushed against the frame of the fuselage

B. /s installed around the door on the outer side and when the door is closed, the it is

pushed against the frame of the fuselage

C. /s deflated when the door is closed and the passenger cabin is pressurized.

1(*.The air sto))ers are insta!!ed &et"een the BA< door and the door fra$e

A. re1ent the cold air from penetrating into the cabin

B. re1ent the water comes into the cabin

C. rotect the door structure during operation.

1(6.E$er4enc' e=it door of a320 aircraft#

A. Can be opened from outside or)and inside and the door fall outside of aircraft.

B. Can be opened from outside or)and inside and the door fall into the cabin.

C. Can be opened from outside and the door fall outside of aircraft

D. Can be opened from inside and the door fall into the cabin,

1(,.The )ressriation of the car4o door h'dra!ic s'ste$ does not occr "hen#

A. The loc'ing mechanism is in the loc'ed condition.

B. The door not in fully close or)and open position.

C. The door not in fully open position.

D. The door is operated with hand pump

1(5.GC :ar4o-:o$)art$ent Door is o)ened#

A. utward and upward.

B. utward and downward.

C. /nward and upward.

D. /nward and downward.

1(9.The D and AT car4o doors#

A. ossible to open)close at the same time

B. ossible to open at the same time when using the electric pump only

C. ossible to open one by one only

D. ossible to close at the same time only

1*0.The e=terna! )o"er rece)tac!e

A. /s installed in the lower and is a 3uic'-opening type door and opens outwardstowards the front of the aircraft

B. /s installed in the lower and is a 3uic'-opening type door and opens outwards

downwards the front of the aircraft

C. /s installed in the lower and is a 3uic'-opening type door and opens outwards

upwards the front of the aircraft

1*1.The esca)e s!ide "i!! &e ato$atica!!' de)!o'ed if#

A. irt bar attached with escape slide pac' and the door is opened.

B. irt bar is still engaged into floor brac'et and the door is opened.

C. irt bar is still engaged into floor brac'et and the door is opened by outside handle

1*2.The fnction of the safet' )in on the )a= door is#

A. To hold the door when it is closed during whole flight.


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B. To hold the door in the closed position until it is loc'ed.

C. To hold the door in the closed position until it is unloc'ed.

1*3.andin4 4ear doors can &e o)ened.

A. =ydraulically on ground only with landing gear selector set to down.

B. =ydraulically or manually if aircraft is on jac'.

C. 4anually on ground only with landing gear selector set to down

1*(.Avionics co$)art$ent can &e accessed thro4h#

A. A1ionics lower side of the fuselage.

B. A1ionics door on the fwd cargo compartment.

C. Access door in the coc'pit.

1**.E$er4enc' e=it door of a320 aircraft is e>i))ed.

A. &lide, which is automatically disarmed when the door is opened from inside.

B. &lide, which is automatically disarmed when the door is opened from outside.

C. &lide, which can only be disarmed by release the latch pin from inside.

A320 TO A321 DIEREN:ES

1*6.The )ota&!e "ater is !ocated at#

A. 0)= behind the rear cargo compartment.

B. @)= behind the forward cargo compartment.

C. @)= behind the rear cargo compartment.

1*,.If the ca&in e$er4enc' door is o)ened fro$ oter side "ith the esca)e s!ide in

ARMED $ode.

A. The A@46D mode of the escape slide changes to D/&A@46D mode as well as

passenger door.

B. The escape slide will deploy.

C. The door can not be opened.

1*5. here the esca)e s!ide )ac7 of ca&in e$er4enc' door !ocated+

A. =olds on the door.

B. =olds in a container underneath the door.

C. =olds on the o1erhead stowage compartment.

1*9.here the inf!ation reservoir of the e$er4enc' e=its door !ocated+

A. At the bottom of the door.B. /n the o1erhead stowage compartment.

C. /n the A>T cargo compartment.

160.The ABC can nor$a!!' &e s))!ied "ith fe! &'#

A. nly the A pump.

B. nly the 0= main pumps.

C. 0= main pumps or A fuel pump.

161.hat ha))en if a hi4h !eve! is detected+

A. A warning is triggeredI too much fuel.

B. The corresponding @6>60 1al1e closes.C. All refueling operations are stopped.


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162.hich tan7s are the $ain s))!' tan7s+

A. ?ing tan's.

B. Center 7transfer8 tan'.

C. uter cells.

163.o" $an' va!ves are sed drin4 the drainin4 o)eration of "ater s'ste$+

A. ne.B. Two.

C. Three.

16(.hich ca&in e$er4enc' e=its door can &e sed as )assen4er door+

A. All emergency eits doors

B. Two >?D emergency eits doors

C. Two A>T emergency eits doors

D. >?D 0)= emergency eits doors

16*.hat ha))en "hen the e$er4enc' e=it door of A321 aircraft is o)ened fro$ the

otside and s!ide s'ste$ is ar$ed+A. The loc'ing mechanism is bloc'ed




166.Is it )ossi&!e to fi!! the A321 aircraft "ater tan7 "ithot e!ectrica! s))!ied+

A. 2es, fill)o1erflow drain 1al1e can operate manually

B. 2es, but when finished you must manually return the control handle to the

5@4A0 position to close the fill)o1erflow drain 1al1e

C. 5o, because le1el transmitter can not send signal to close the fill)o1erflow drain

1al1e

D. 5o, because the fill)o1erflow drain 1al1e operate electrically

16,.The ABC of A321 aircraft can nor$a!!' &e s))!ied "ith the fe! &'#

A. nly the A pump

B. nly the 0= main pumps

C. 0= main pumps or A fuel pump

165.The en4ine anti-ice air over&oard dischar4e 4ri!! is !ocated+

A. n the outboard side of the inlet cowl.

B. n the right side fan cowl door.C. n the lower right side of the inlet cowl.

D. At the bottom 7: oJcloc' position8 of fan cowling

169.The en4ine oi! servicin4 )ane! is !ocated+

A. n the outboard side of the inlet cowl.

B. n the left side fan cowl door.

C. n the left side of the inlet cowl.

D. n the left side of the re1erser cowl.

1,0.Each reverser co"!#

A. /s hold closed by " single latches.B. /s held open by a single hold open rod.

C. /s held open by two hold open rods.


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1,1.hen the en4ine is rnnin4 #

A. 5o personnel is allowed to get access to the engine.

B. Access to the engine is permitted within the 6ntry)6it corridor if power do not

eceed min idle.

C. Access to the engine is permitted within the 6ntry)6it corridor at all power rating.

1,2.The en4ine rn ) at Min id!e can &e carried ot "ith #

A. >an cowls opened and secured.

B. Both @e1erser and >an cowls opened and secured.

C. Thrust @e1erser cowls opened and secured.

D. 5on engine cowl opened.

ATA ,2 ; ENINE :M *6-*&

1,3.eatres of :M-*6-*G( en4ine are#

A. Two spools, aial flow, high fan bypass ratio and mied ehaust.

B. Two spools, radial flow, high fan bypass ratio and mied ehaust.

C. Two spools, aial flow, high fan bypass ratio and separated ehaust.

D. Two spools, aial flow, high fan bypass ratio and mied ehaust.

1,(.Se!ect the correct t')e of co$&stion cha$&er for :M-*6-*G( en4ine+

A. Annular combustor.

B. Tubular combustor.

C. @e1erse flow combustor.

1,*.The .B. :o$)ressor has ho" $an' sta4es+

A.Twel1e.B. Ten.

C. 5ine

1,6.The B Tr&ine has ho" $an' sta4es+

A. nly one stage.

B. >our stages

C. Two stages.

1,,. Identif' the n$&er of &!ades in one en4ine fan set+

A. Thirty si 7*"8

B. Twenty two 7++8C. Thirty two 7*+8

1,5.The en4ine 4ear &o=es are driven &' "hich shaft+

A. 5$ rotor.

B. 5+ rotor 1ia the transfer gear bo.

C. 5+ rotor.

1,9.The hand cran7in4 drive connects to+

A. 0 rotor.

B. = rotor.

C. Both 0 and = rotors.

ATA ,( ; INITION SFSTEM.


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150.Of "hich t')e is the i4nition s'ste$+

A. 0ow 1oltage, high energy.

B. =igh 1oltage, low energy.

C. =igh 1oltage, high energy.

151.hat )rovide the se!ection of i4nition A/G+A. The 6C.

B. The engine control panel.

C. The 6CA4 control panel.

152.hen the i4nition is inhi&ited+

A. During automatic start when 5+ is abo1e $"L.

B. During dry cran' se3uence.

C. During wet cran' se3uence.

D. During wet and dry cran' se3uences.

153.Each en4ine e>i))ed "ith+A. ne ignition system with two igniters.

B. Two ignition systems, each has two igniters.

C. Two ignition systems with two igniters.

15(.I4nition s'ste$ )o"er s))!' is+

A. $$: < from the aircraft.

B. $$: < from engine generator.

C. +# < from the >AD6C 4A.

15*.hat does :ontinos Re!i4ht $ean+

A. An acti1e ignition system will wor' continuously.

B. Both ignition systems are selected during engine start.

C. Both ignition systems are demanded to wor' continuously.

ATA -,* ; AIR SFSTEM

156.Is the )r)ose of the Active :!earance :ontro! ?A::@ s'ste$+

A. To impro1e compressor efficiency

B. To impro1e and maintain engine performanceC. To reduce o1erall engine thermal growth

15,.hat is sed to coo! the E:C+

A. @am air ta'en from dedicated air inta'e scoop.

B. >an air ta'en from dedicated air inta'e scoop.

C. >an air ta'en from nacelle cooling system.

155.hat is sed to coo! the fan and core co$)art$ents+

A. @am air for both compartments

B. >an air for both compartments.

C. @am air for fan compartment and >an air for core compartment.

ATA - ,,# ENINE INDI:ATION.


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159.The en4ine )ri$ar' )ara$eters are dis)!a'ed on+

A. The lower 6CA4 engine page.

B. The upper 6CA4.

C. Both The lower 6CA4 engine page and the upper 6CA4.

190.The en4ine )a4e is se!ected+A. 4anually or automatically depend on flight phases.

B. 4anually only.

C. Automatically only depend on flight phases.

191.The en4ine vi&ration )ara$eter is dis)!a'ed on+

A. The pper 6CA4.

B. The 0ower 6CA4 engine page.

C. The 0ower 6CA4 engine page or Cruise page.

192.The en4ine oi! >antit' )ara$eters are dis)!a'ed on+

A. The pper 6CA4.B. The 0ower 6CA4 engine page.


193.The en4ine oi! )ressre )ara$eters are dis)!a'ed on+

A. The pper 6CA4.

B. The 0ower 6CA4 engine page.


19(.The fe! sed indication is reset to Kero #

A. >i1e minutes after engine shut down

B. After a new ta'e-off

C. Through the 4CD

D. At each engine start

19*.The en4ine thrst indicated on E:AM via "hat )ara$eter+

A. 5$ speed.

B. 5+ speed

C. 6T

ATA ,5 ; ENINE TRCST RE8ERSER.

196.hich i$)ortant safet' )rocedre sho!d &e )erfor$ed &efore an' $aintenance

"or7 on or near the L:H dcts or reverser s'ste$+

A. nloc' and pin the actuators.

B. 0oc' out the translating slee1es.

C. Deacti1ate and pin the le1er on the =C.

D. Deacti1ate and pin the le1er on the =C and loc' out translating slee1es.

ATA -,9 # ENINE OI SFSTEM

19,.The oi! tan7 content can &e chec7ed &'+

A. pening a dedicated ser1icing access panel in the 0= fan cowl.B. pening an access panel on the 0= GCJ duct.

C. pening the @= fan cowl


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195.o" is the $ain coo!in4 of the oi! s'ste$ achieved+

A. By an air-cooled oil cooler.

B. By a fuel cooled oil cooler in the = fuel system.

C. By a fuel cooled oil cooler in the 0 fuel system.

199.En4ine oi! M:D is on+A. The oil supply circuit.

B. The oil sca1enge circuit.

C. The oil 1entilation circuit.

200.En4ine oi! te$)eratre indication is $easred on+

A. The oil supply circuit.

B. The oil sca1enge circuit.

C. The oil 1entilation circuit.

ATA - 50 ; ENINE STARTIN.

201.o" can 'o assre that the oi! servicin4 of starter is acco$)!ished+

A. Chec'ing the engine oil sign glass.

B. Chec' 6CA4 indication.

C. Chec' the oil flows though the o1erflow port.

202.hat is the &est "ind direction for en4ine STARTIN+

A. &ide wind.

B. Tail wind.

C. >ront wind.

ATA ,1-50# 82*00 ENINE ; DIEREN:E.

203.eatres of 82*30-A* en4ine are#

A. Two spools, aial flow, annular combustor and mied ehaust.

B. Two spools, radial flow, annular combustor and mied ehaust.

C. Two spools, aial flow, annular combustor and separated ehaust.

D. Two spools, aial flow, tubular combustor and mied ehaust.

20(.82*30-A* $eans#

A. 6ngine is rated at ma thrust of +:*%% lbs to install in the Airbus A)C.

B. 6ngine is rated at ma thrust of *%%%% lbs to install in the Airbus A)C.C. 6ngine is rated at ma thrust of +:%%% lbs to install in the Airbus A)C.

20*.The en4ine e=hast directs rear"ards+

A. >an air discharge.

B. 6ngine core ehaust.

C. Both fan air discharge and the engine core ehaust.

206.Reverser co"!in4#

A. /s attached to the engine core by " hinges each half.

B. /s hold closed by : single latches.

C. &hould be opened)closed using the Auiliary latch assembly.

20,.Each ha!f of reverser co"! c dct#


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A. /s held closed by ! latches.

B. /s held open by a single hold open rod.

C. /s held open by two hold open rods.

205.an co"!s#

A. 4ust be held open by both struts each when the wind is more than +" 'nots 7*%

mph8.B. &hould be opened by releasing " latches in se3uence from the front to the rear.

C. 4ust always be held open by both struts each.

209.The .B. :o$)ressor has ho" $an' sta4es+

A. Twel1e.

B. Ten.

C. >ourteen.

210.Identif' the n$&er of &!ades in one en4ine fan set+

A. Thirty three 7**8

B. Twenty two 7++8C. Thirty two 7*+8

211.hat state$ent is NOT correct+

A. >an stage has ++ fan blades.

B. >an stage has +! fan blades.

C. 6ngine is constructed by %: modules.

D. earboes are dri1en by = shaft.

212.The air starter va!ve access )ane! is on+

A. @= fan cowl.

B. 0= fan cowl

C. @= re1erser cowl.

D. ut board fan cowl.

213.as the oi! )ressre fi!ter a )o) ot indicator fitted+

A. 2es.

B. 5o.

C. There is no pressure filter in the system.

21(.hich fi!ters in the oi! s'ste$ have associated fi!ter c!o4 $essa4es on the

E:AM+A. ressure &ca1enge and &ca1enge strainers.

B. ressure only.

C. &ca1enge only.

21*.hich nor$a! indications are dis)!a'ed on the E:AM for the oi! s'ste$+

A. il differential pressure, oil temperature, oil tan' 3uantity.

B. il temperature, oil pressure.

C. il differential pressure, oil 3uantity,

216.hat does the MS heat and coo!+

A. >uel, engine oil and /D oil.B. 6ngine oil and /D oil.

C. >uel only.


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D. >uel and engine oil.

21,.o" the Nose :one ?S)inner@ is anti-iced+

A. 6lectrically.

B. neumatically.

C. 5either electrically nor pneumatically.

D. 5ot re3uired.

215.In nor$a! T/R o)eration actator n!oc7ed condition is indicated &'+

A. @6< in green appears inside the 6@ gauge.

B. @6< in amber appears inside the 5$ gauge.

C. @6< in amber appears inside the 6@ gauge.

219.e! sa$)!es can &e ta7en fro$+

A. The 0 fuel filter co1er.

B. The 0 fuel pump case.

C. The = fuel pump outlet.

230.hich en4ine )ara$eters are dis)!a'ed on the E:AM ))er dis)!a'+

A. 6@, 5$ 5+.

B. 5$, 5+, 6@, oil pressure, oil temperature.

C. 5$, 5+, 6@ 6T.

Level A QB

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