Airbus A320 Performance Test

5/27/2018 Airbus A320 Performance Test

1/100

QuestionA320 CFM metric Test 1 / 100

For the Normal Operation of the CARGO CON

!"!T#M $

The pilot ensures that there are no li%hts

illuminate& on the p' s( an& that the

temperature is set as re)uire&*

A

The s+stem &ispla+ (ill 'e foun& on the#CAM ,-## pa%e*

,

The pilot has no control of the s+stem

temperature*

C

The s+stem &ispla+ (ill 'e foun& on the

#CAM .R#!! pa%e*

AftCargo

Ventilation

Controller

ForwardCargo

Ventilation

Controller

1


2/100


The t(o pacs are lost an& there is no

more air con&itionin%*

All the ales are close& an& the RAM AR

must 'e use& for the ca'in air

con&itionin%*

ae a loo at the #CAM CON4 pa%e $ .AC5

R#G4 is &ispla+e&*

6hat &oes it mean7

A

,C

The 8ON# CONTRO--#R has faile&9

temperature re%ulation is &one ia the

OT AR ale*

The 8ON# CONTRO--#R has faile& an&

the t(o pacs &elier a fi:e& temperature

2


3/100


;00 ft*

;000 ft*

On the CA,N .R#!! panel9 the -G #-#< has

'een set manuall+*

6hat is the appro:imate alue 7

A

,

C

; ft*

;0 ft*

3


4/100


=>00 ft*

;=00 ft*

On the #CAM !TAT?! pa%e9 as +ou can see ca'in

pressure control is manual* "ou (ant &escen& from

F- 3>0 to F- 330* 6hat is +our tar%et CA,N AT-7

A

,

C

0 ft*

=000 ft*

@


5/100


.lease in&icate the position of the


6/100


6hat happens if the G selector no' is pulle&7

The aircraft reerts to the ori%inal F.-N*

A

The G tar%et chan%es to TR5*

,

The aircraft follo(s the selecte& G

until interceptin% the lateral F.-N*

C

Nothin%9 the aircraft continues on G

1@0 in&efinitel+*

;


7/100


-oo at the FMA* NA< in %reen is***

The actie lateral mo&e (hich is a

constraint*

A

The arme& lateral mo&e*

,

The arme& lateral mo&e (hich is a

constraint*

C

The actie lateral mo&e*

B


8/100


ATC cleare& +ou to F- 1=0* The .F sets the ne(

altitu&e on the FC?* 6hat (ill happen if he pulls the

A-T selection no'7

The aircraft (ill stop the clim' at F- ;0

until passin% the constraint then continue

clim' to F- 1=0*

A

The aircraft (ill &isre%ar& the constraintan& clim' to F- 1=0*

,

As soon as the aircraft passes F- ;09 the

tar%et altitu&e on the .F (ill chan%e to

F- 1=0 an& the aircraft continues to clim'*

C

The aircraft (ill leel off at F- ;0* The .F

must pull the A-T selection no' a

secon& time to clim' to F- 1=0*


9/100


The autothrust s+stem has t(o channels* 6hich

FMGC controls the A/TR D'oth FMGCs 'ein%

operatieE7

The FMGC1*

A

The FMGC2*

,

The ran&oml+ chosen FMGC*

C

>


10/100


The +a( 'ar9 (hen &ispla+e& on the .F instea& of

the fli%ht &irector roll 'ar9 is use& to $

.roi&e %ui&ance9 if a localier is

aaila'le for taeoff an& rollout phases*

A

.roi&e %ui&ance after taeoff up to 1000

feat AG- to maintain the run(a+ center

line*

,

Confirm that the aircraft is (ell

esta'lishe& in the %li&e slope on -! final

approach*

C

Chan%e oer automaticall+ in case of

localier failure on -! final approach*

10


11/100


As soon as a CO RT# or a CT" .AR is entere& in

the NT .AG# A9 the &ispla+e& coor&inates are$

The run(a+ threshol& position*

A

The aircraft present position*

,

The airport reference point position*

C

The alternate airport position

11


12/100


The F.-N pa%e sho(n in the MC? is $

The F.-N pa%e A*

A

The F.-N pa%e ,*

,

12


13/100


The stan&ar& instrument &eparture is sho(n on the

nai%ation &ispla+9 ho(eer an am'er line can 'e

seen$

t is the secon&ar+ F.-N*

A

t is a temporar+ F.-N*

,

t is the en%ine out stan&ar& instrument

&eparture*

C

t is the stan&ar& &eparture for li%ht

airplanes*

13


14/100


ae a loo at the MC?9 the -! 23R is a currentl+

selecte& approach9 the %reen color means$

This approach is inserte& into the actie

F.-N*

A

This approach is &ispla+e& in %reen'efore insertion in the F.-N*

,

This approach can not 'e selecte&*

C

1@


15/100


On the clim' fli%ht path9 2 en%ines runnin%9 the !R!

Dspee& reference s+stemE proi&es a pitch attitu&e

to maintain$


16/100


6hat is the meanin% of the small ma%enta &ot

&ispla+e& '+ the altitu&e scale7

t (arns the pilot a'out a possi'le (ron%

altitu&e settin% on the FC?*

A

t (arns the pilot that the spee& must 'e

re&uce& to re%ain the compute& &escent

profile*

C

t in&icates that the e:pe&ite mo&e must

'e en%a%e&*

t hi%hli%hts an+ ertical &eiation of the

aircraft from the compute& &escent

profile*

,

1;


17/100


6h+ must the pilot press the tae oer push'utton

on the si&e stic t(ice to &isconnect the autopilot7

A first time to &isconnect the autopilot

an& a secon& time to confirm the

&isconnection*

A

A the first time to &isconnect the autopilot

an& a secon& time to %et a &efinite priorit+

on his si&e*

,


an& a secon& time to reset all the relate&

(arnin%s*

C


an& a secon& time to reset the master

FMGC*

1B


18/100


F1 2 are ON9 no A. is en%a%e&9 (hich FMGC is

master7

The s(itchin% occurs at eer+ FMGC

po(er up*

A

t &epen&s on (hich ATR channel isen%a%e&*

,

FMGC2*

C

FMGC1*

FMGC 2FMGC 1

1


19/100


6hat is the meanin% of OPP FMGC IN PROCESS49

the messa%e &ispla+e& here in the scratchpa& of

MC?17

MC?1 is &rien '+ FMGC2*

A

The FMGC2 is no( master*

,

The FMGC2 performance 'ecame 'etter

than the FMGC1*

C

1>


20/100


"ou are in TR -#/#!4 mo&es (ith autopilot 1

en%a%e& an& the FC? 1 fails*

6hat is the action re)uire&7

As the autopilot 1 &isen%a%es9 en%a%e

autopilot 2*

A

The .F 'arometric reference is no( onl+

aaila'le on stan&ar& an& the pilot mustset the current 'aro settin% on the

stan&'+ altimeter*

,

The FC?2 has taen oer automaticall+

an& the 'aro reference must 'e cross

chece&*

C

20


21/100


The aircraft must 'e on the %roun& (ithat least one en%ine runnin%*

,

The aircraft must 'e off the %roun&*

C

The en%ines must 'e shut &o(n for at

least = minutes*

After lan&in%9 to erase the C


22/100


False*

,

On the


23/100


False*

,

6ith the A?O !6TCNG no' in the CA.T 3

position9 the captain su'stitutes AC. 3 for AC. 1*

True*

A

23


24/100


"ou (ant to rechar%e the 'atteries*

o( &o +ou procee&7

#:ternal po(er is aaila'le* onl+ hae to

s(itch the 'atteries to on an& the+ (ill 'e

char%e&*

A

hae to s(itch the e:ternal po(er an&

the 'atteries to on an& the 'atteries (ill'e char%e&*

,

hae to s(itch the e:ternal po(er to ON

an& the 'atteries (ill 'e char%e&*

C

hae to call a mechanic 'ecause the

'atteries can onl+ 'e char%e& '+

maintenance*

2@


25/100


,oth 'atteries are no( 'ein% char%e& '+ the

e:ternal po(er unit* Appro:imatel+ ho( lon% &oes

the char%in% process tae 7

10 minutes

A

One hour

,

20 minutes

C

!eeral hours

2=


26/100


-ooin% at the #CAM #-#C .a%e9 to connect A.?

G#N$

.ush A.? G#N p' s( locate& oerhea&

panel*

A

6ait until 1st #n%ine is !tarte&*

,

eselect #HT .6R*

C

!6TC OFF ,AT 12*

2;


27/100


On #HT .6R p' s(9 the illuminate& c+an li%ht

means that$

The %roun& cart is suppl+in% the aircraft

electrical net(or*

A

#:ternal po(er is plu%%e& in 'ut notsuppl+in% the net(or*

,

#:ternal po(er is plu%%e& in an& &eliers

'lee& air onl+*

C

2B


28/100


On #HT .6R p' s(9 the illuminate& c+an li%ht

means that$

The %roun& cart is suppl+in% the aircraft

electrical net(or*

A

#:ternal po(er is plu%%e& in 'ut notsuppl+in% the net(or*

,

#:ternal po(er is plu%%e& in an& &eliers

'lee& air onl+*

C

2BQuestionA320 CFM metric Test 1 / 100

After startin% en%ine nI29 is the present #CAM #-#C

pa%e a correct confi%uration7

No* #NG G#N nI2 shoul& po(er all

aircraft net(or*

A

No* The A.? G#N shoul& continuepo(erin% all aircraft net(or*

,

"es* #NG G#N nI2 is no( po(erin% its

o(n si&e*

C

2


29/100


Follo(in% an AC ,?! 1 fault9 pushin% the AC #!!

F## p' s( on #-#C oerhea& panel allo(s +ou$

To recoer the AC #!! ,?! po(er onl+*

A

To recoer the C #!! ,?! po(er onl+*

,

To recoer AC an& C #!! 'uses*

C

To recoer AC ,?! 1 po(er*

2>


30/100


n case of #-#C #M#R CONF9 -AN A!A. in re& is

&ispla+e& on the #/6*

This messa%e (ill sta+$

As lon% as the Re& (arnin% #-#C #M#R

CONF persists*

A

#en after hain% reset one %eneratorsuccessfull+*

,

#en if ,?! T# p' s( is pushe&*

C

#en if A.? is starte&*

30


31/100


n case of an #-#C #M#R CONFG situation9 ho(

can the t(o si&es of the electrical s+stem 'e

se%re%ate& e*% to isolate a short circuit 7

.ush ,?! T# p' !6 locate& on #-#C

s+stem oerhea& panel*

A

Reset each AC %enerator*

,

Manuall+ lo(er RAT '+ pushin% its p' !6

C

Nothin% has to 'e &one 'ecause the

se%re%ation is &one automaticall+*

31


32/100


n #M#R #-#C CONF9 (hen the RAT stalls &ue to

A/C spee& &ecreasin%9 the static inerter (ill

'ecome actie in or&er to suppl+$

The C #!!*

A

The complete C net(or*

,

The AC #!!*

C

The AC an& C #!!*

32


33/100


6hich of those area9 has NO fire e:tin%uishin%

s+stem installe&7

Aionic 'a+*

A

Car%o compartments*

,

#n%ine / A.?*

Ca'in*

C

33


34/100


Accor&in% to this #CAM #/6 pa%e9 the associate&

proce&ure is

An in&ication presentin% the F6 CARGO

!MO5# con&ition onl+*

A

To press the illuminate& re& F6 !MO5#!C p'*

,

To lift the re& %uar& an& press the !C

p'*

C

This is an automatic fonction an& +ouhae to press F6 !MO5# p' to confirm*

3@


35/100


Accor&in% to these in&ications9 (hich fli%ht control

la( is actie 7

A

,

C

Normal -a(*

Alternate -a(*

irect -a(*

Mechanical ,ac ?p*

3=


36/100


Accor&in% to these in&ications9 (hich fli%ht control

la( is actie 7

A

,

C

Normal -a(

Alternate -a(

irect -a(

Mechanical ,ac ?p

3;


37/100


O'sere the .F*

6ithout an+ si&estic inputs***

A

,

C

The aircraftJs attitu&e (ill sta+ constant*

The pitch (ill sta+ constant9 the'an an%le (ill slo(l+ &ecrease*

The 'an an%le (ill sta+ constant9 the

pitch (ill slo(l+ &ecrease*

The aircraftJs attitu&e (ill slo(l+ ten&

to(ar&s (in%s leel4 an& pitch 04*

3B


38/100


The Alpha Floor protection has 'eentri%%ere&*

The -oa& Factor -imitation has 'een

tri%%ere&*

There is no protection tri%%ere& +et*

The i%h An%le Of Attac protection has

'een tri%%ere&*

Accor&in% to the follo(in% in&ications***

A

,

C

3


39/100


To fl+ a coor&inate& turn***

No ru&&er inputs are re)uire&*

A

"ou hae to center the si&eslip in&icator(ith the ru&&er pe&als*

,

Onl+ small ru&&er inputs are re)uire&*

C

3>


40/100


n Normal -a(9 is there a ma:imum 'an an%le 7

A

,

C

No*

"es9 in&icate& '+ the %reen &ashes D'E*

"es9 in&icate& '+ the (hite &ashes DaE*

"es9 'an is limite& to 0K*

a

'

@0


41/100


o( &o +ou interpret the am'er crosses on the

.F 7

The autotrim is lost* "ou hae to use

manual pitch trim*

A

The ailerons are controlle& &irectl+ '+ thesi&estics*

,

The 'an an%le limit protection is lost*

C

The 'an an%le protection is actie*

@1


42/100


The C.TJs si&estic is &eflecte& full+ left an& the

FOJs si&estic is simultaneousl+ &eflecte& full+

ri%ht*

6hich in&ications &o +ou e:pect 7

A

,

C

@2


43/100


6ith either A. en%a%e&9 (hich statement is true 7

,oth si&estics are loce& in neutral

position* The loc can not 'e oerri&&en

A

,oth si&estics are &eactiate& untilthe A. is &isen%a%e&*

,

,oth si&estics are loce& in neutral

position* ,+ appl+in% a certain force9 the

loc can 'e oerri&&en 'ut the A.

remains en%a%e&*

C

,oth si&estics are loce& in neutralposition* ,+ appl+in% a certain force9 the

loc can 'e oerri&&en an& the A. is

&isen%a%e&*

@3


44/100


6hat (ill happen Lust 'efore the spee& reaches


45/100


Accor&in% to this F?#- ! pa%e in&ications9 (hich

pumps are fee&in% the en%ines7

The Center Tan .umps alone*

A

The Center Tan .umps an& the innertan pumps*

,

The inner Tan .umps alone*

C

@=


46/100


On the #CAM9 the messa%e O?T#R T5 F?#- HFR

appears in the M#MO* 6hat &oes it mean7

Fuel is transferre& from the inner tan to

the outer tan*

A

Fuel is transferre& from the outer tan to

the inner tan*

,

Fuel is transferre& from the inner tan to

the center tan*

C

Fuel is transferre& from the center tan to

the inner tan*

@;


47/100


"ou are in cruise an& accor&in% to those

in&ications9 a failure occurre& in the fuel s+stem*

6h+ &i&nt +ou %et a master caution or a chime7

The fuel s+stem is not connecte& to the

Fli%ht 6arnin% Computer*

A

nner tan pump failures neer tri%%er a

(arnin% 'ecause the fuel can 'e use& '+

%rait+ fee&in%*

C

ue to re&un&anc+9 loss of one pump is

onl+ leel 1 caution*

,

@B


48/100


The normal pressure for the h+&raulic s+stem is

2000 psi

A

,

True*

False*

@


49/100


2000 psi

3000 psi

6hat is the normal pressure in the h+&raulic

s+stem7

A

,

C

=00 psi

1000 psi

@>


50/100


The .T?*

,oth the GR##N an& "#--O6 s+stems*

Accor&in% to this in&ication9 the ,-?# s+stem is

po(ere& '+***

A

,

C

The #-#C pump*

The RAT*

=0


51/100


?sers connecte& to the "#--O6 s+stem

are no lon%er supplie& (ith h+&raulic

pressure*

6e hae complete& the proce&ure for " " R!


52/100


"ou (ant to increase the air pressure '+

isolatin% the "#--O6 s+stem*

"ou (ant to aoi& the pressuriation of

the +ello( s+stem '+ the .T? after +ou

s(itch the #NG 2 pump off*

"ou %et a " R!


53/100


The ,-?# an& the "#--O6 s+stems are

suppl+in% the GR##N s+stem*

The "#--O6 s+stem is suppl+in% the

GR##N s+stem*

6hich statement is true7

A

,

C

The GR##N s+stem is supplie& '+ the

,-?# s+stem*

The "#--O6 s+stem is suppl+in% the

,-?# an& the GR##N s+stem*

=3


54/100


The RAT is pressuriin% the ,-?#

s+stem*

6hat is the meanin% of the RAT in&ication9 as

&ispla+e& on this " #CAM pa%e7

A

,

C

The RAT is fault+*

The RAT is &eplo+e&*

=@


55/100


6hat is the correct .T? in&ication if it is &elierin%

po(er to the GR##N s+stem7

A

,

C

==


56/100


On the #CAM ,-## ! pa%e9 (hat is the normal

in&ication in fli%ht (ith 6NG ANTC# on7

A

,

C

=;


57/100


.lease in&icate the #CAM #/6 screen*

A

,

C

C

=B


58/100


.lease in&icate the N 2*

,

A

C

=


59/100


Re&*

A

Am'er*

,

Green*

C

6hite*

Color co&in% on the #CAM screens$ (hich color

in&icates that cre( a(areness is re)uire&7

A

,

C

=>


60/100


Re&*

A

Am'er*

,

Green*

C

6hite*

Color co&in% on the #CAM screens$ (hich color

in&icates a normal con&ition7

A

,

C

;0


61/100


On the #CAM ! pa%e9 (hat &oes an a&isor+

messa%e mean7

The parameter is a'out to reach a limit*

A

The parameter is out of limits*

,

The parameter has a fault+ in&ication*

C

1.1 5.1

;1


62/100


.ress an& hol& the correspon&in% 'utton

on the #C.*

A

!(itch the ! to one of the NJs*

,

!(itch the ! to one of the .FJs*

C

The upper #CAM ? faile&* To see the &ifferent

s+stem pa%es on the lo(er ?9 +ou hae to$

;2


63/100


The #/6 is automaticall+ transferre& to

one of the NJs*

A

The #/6 is automaticall+ transferre& to

one of the .FJs*

,

To %et #/6 information9 it must 'e

manuall+ transferre& to one of the NJs*

C

To %et #/6 information9 it must 'e

manuall+ transferre& to one of the .FJs*

,oth #CAM screens faile&* 6hat happens to the

#/6 in&ication7

;3


64/100


The failure messa%e has 'een preiousl+

cancelle& (ith the #M#R CANC p'*

A

The failure messa%e ha& occurre& &urin%

the preious fli%ht*

,

The F6C is (orin% in a &e%ra&e& mo&e

an& is not a'le an+more to &etect this

failure*

C

,ecause it (as a false (arnin%9

maintenance inhi'ite& it*

On the #CAM !TAT?! pa%e 9 (hat &oes a

CANC#--# CA?TON mean7

;@


65/100


The location of the FR Di%ital Fli%ht ata

Recor&erE is $

nsi&e the Cocpit*A

nstalle& in the tail !ection of the aircraft9

an& the &ata is store& on a tapeContaine& in fire an& shoc proof 'o:*

,

n the passen%er Ca'in for protection

reason*

C

;=


66/100


6hen is the FR automaticall+ ener%ie&7

The FR (ill 'e onl+ ener%ie& after the

first en%ine start*

A

The FR is ener%ie& &urin% = minutes

an& then after the first en%ine start*

,

The FR (ill 'e ener%ie& at lift off*

C

;;


67/100


6hen a FR fault occurs9 it (ill 'e si%nale& '+ $

A fault li%ht illuminatin% am'er on

oerhea& panel*

A

An #CAM caution messa%e*

,

A lo( fre)uenc+ si%nal soun&s throu%h

the cocpit lou& speaer*

C

A MANT#NANC# messa%e in the status

pa%e*

;B


68/100


On the .F9 (hat is the actual spee&7

1=0 t*A

1;0 t*

,

1;> t*

C

1= t*

140

160

180

200

F

120

;


69/100


On the .F9 (hat is the ma:imum spee& to select

the ne:t flap settin%7

1@0 t*A

1== t*

,

1B= t*

C

1= t*

140

160

180

200

F

120

;>


70/100


On the .F9 (hat is the meanin% of the 'lue ri''on

on the altitu&e scale7

t mars the lan&in% eleation*A

t mars the selecte& altitu&e*

,

t mars the preselecte& altitu&e*

C

t mars the &ecision hei%ht*

STD

FL 70

30.08

QNH

7000

B0


71/100


On the .F9 (hat is the actual ertical spee&7

0 ft/min in clim'*A

00 ft/min in &escent*

,

0 ft/min in &escent*

C

00 ft/min in clim'*

STD

FL 70

30.08

QNH

7000

B1


72/100


On the .F9 (hat is the selecte& hea&in%7

0;>*A

00*

,

0@*

C

B2


73/100


On the .F9 (hat is the actual aircraft trac7

0;>*A

00*

,

0@*

C

B3

O h N hi h f h f ll i i


74/100


On the N9 (hich of the follo(in% statements is

true7

The hea&in% to the ne:t (a+point .A! is

109 it is at 2 NM9 time left to the

(a+point is > minutes an& secon&s*

A

The hea&in% to the ne:t (a+point .A! is

109 it is at 2 NM9 time to the &estinationis > hours an& minutes*

,

The trac to the ne:t (a+point .A! is

109 it is at 2 NM9 elapse& time of this

fli%ht is > minutes an& secon&s*

C

The trac to the ne:t (a+point .A! is109 it is at 2 NM9 it (ill 'e oerflo(n at

>$0*

B@

O th .F th t ' l th &


75/100


On the .F9 the ma%enta s+m'ols on the spee&

scale represent$

The #CON spee& ran%e &urin% mana%e&

&escent*

A

The mana%e& spee& '+ the FMG! &urin%

mana%e& clim'*

,

The upper ma%enta for hi%h spee&

protection9 the lo(er for tur'ulence

operatin% spee&*

C

The lo(er ma%enta s+m'ol represents


76/100


p % p +

from ecto .ascals to inches of mercur+ an& ice

ersa7

No9 it is not possi'le 'ecause each airline

has its o(n confi%uration*

A

"es9 '+ rotatin% the outer scale of 'aro

reference selector on the #F! panel*

,

No9 the cre( shoul& refer to a conersion

ta'le*

C

"es9 'ut onl+ the Captain si&e is e)uippe&

(ith this conersion*

1020

B;

O th .F lti t l hi h t t t i


77/100


On the .F altimeter scale9 (hich statement is

correct 7

The cre( is pushin% the 'aro reference

selector to chan%e from !T settin% to

local QN*

A

Cre( is pushin% the 'aro reference

selector to chan%e from local QN to the!T settin%*

,

The rate of &escent is 2@0 F.M*

C

Aircraft passin% altitu&e is =00 ft*

STD

FL 70

BB

urin% push 'ac9 en%ine nI 2 is starte&9 lea&in% to


78/100


The nose (heel steerin% has 'een re

connecte& '+ %roun& personnel*

The am'er in&ication (ill &isappear as

soon as +ou start ta:i*

The nose (heel steerin% is still

&isconnecte&* The memo has 'ecome

am'er 'ecause one en%ine is runnin%*

% p 9 % 9 %

the NW STRG DISC4 memo*

6hat is the correct statement7

A

,

C

The N6 !TRG &isconnect mechanism

has

faile&*

The +ello( h+&raulic s+stem has 'uil& up

pressure (hich mi%ht &ama%e the N6

!TRG s+stem (hen set to to(in%position*

NW STRG DISC

APU BLEED

B

6hat is the meanin% of the %reen arc appearin%


79/100


The ANT/!5 s+stem is automaticall+

releasin% the pressure of that 'rae*

The -/G control s+stem has &etecte& a

lo( tire profile*

6hat is the meanin% of the %reen arc appearin%

oer (heel 27

A

,

C

t mars the hottest 'rae (ith a

temperature of more than 100 K Celsius*

t in&icates an a'normal hi%h

temperature*

B>

"ou perform a lan&in% (ith A?TO/,R5 selecte& to

M# After touch &o(n +ou o'sere the follo(in%


80/100


The ANT/!5 s+stem for (heels 1 an&

3 is inoperatie*

The A?TO/,R5 is appl+in% pressure to

'rae 2 an& @ onl+*

M#* After touch &o(n +ou o'sere the follo(in%

in&ications*

At this moment9 (hich statement is true 7

A

,

C

The ANT/!5 s+stem is increasin% 'rae

pressure for (heels 2 an& @*

The ANT/!5 s+stem is releasin% 'rae

pressure for (heels 2 an& @*

0

urin% +our (alaroun& +ou see that one li%ht


81/100


T/O li%ht*

Ta:i li%ht*

urin% +our (alaroun&9 +ou see that one li%ht

nee&s a ne( 'ul'* 6hat is the purpose of this li%ht7

A

,

C

-an&in% li%ht*

R6" turnoff li%ht*

1

On the #HT -T control panel9 the !TRO,# li%ht


82/100


6hen the lan&in% li%hts are s(itche& off*

6hen the last en%ine has 'een shut

&o(n*

selector is set to A?TO* n this position9 (hen &o

the+ stop flashin%7

A

,

C

6hen the aircraft touches &o(n*

6hen the first reerser is opene&*

2


83/100


6hich Naai&s are &ispla+e& on the RM7


84/100


,et(een the N an& MC? +ou are performin% a

NA< ACC?R chec* oes it satisf+ +ou7

"es9 ra( &ata an& FMG! position are the

same or the &ifference is (ithin

accepta'le limits*

A

No9 there is a maLor &iscrepanc+ 'et(een

ra( &ata an& FMG! positions*

,

No9 the accurac+ is &ispla+e& -O6 on the

MC? .ROG pa%e*

C

@

On the passen%er OH"G#N control panel9 (hich


85/100


C

On the passen%er OH"G#N control panel9 (hich

in&ication confirms the &eplo+ment of the mass7

A

,

=

The cocpit CR#6 OH"G#N 'ein% operatie9

hi h ' h t ' & t it h th t


86/100


(hich p' has to 'e presse& to s(itch the s+stemOFF7

C

;

On the #CAM control panel9 please select the

i t #CAM t t i f ti ' t th


87/100


appropriate #CAM pa%e to %et information a'out the

.N#?MATC s+stem*

A

C

,

B

,oth en%ines are runnin% an& A.? ,-## has 'een

s(itche& OFF s the #CAM ,-## pa%e &ispla+


88/100


s(itche& OFF* s the #CAM ,-## pa%e &ispla+

correct 7

No9 A.? 'lee& close&9 'ut H 'lee& ale

has to sta+ open*

A

No9 the cre( shoul& select H 'lee& ale

selector to DshutE position to close theale manuall+ after one en%ine is starte&*

,

No9 . . ales shoul& 'e close&*

C

"es9 all the in&ications are correct9 .ales open 'ecause of hi%h air &eman&

(ith en%ine at lo( R.M*

"ou hae Lust set the A.? MA!T#R !6 to OFF*

"ou notice +ou still hae A.? A


89/100


"ou notice +ou still hae A.? A

6hich #CAM A.? pa%e correspon&s to these


90/100


6hich #CAM A.? pa%e correspon&s to these

in&ications on the oerhea& panel 7

A

,

C

>0

Accor&in% to this in&ication9 the Car%o &oor is


91/100


inoperatie*

A

,

True*

False*

>1

On the #CAM ! OOR/OH" pa%e this in&ication


92/100


The left for(ar& ca'in &oor an& the

for(ar& car%o &oor are unloce&9 the

oer(in% e:its an& the ri%ht rear &oor

sli&es are not arme&*

Oer(in% e:its an& ri%ht rear &oor sli&es

are not arme&9 left for(ar& ca'in &oor an&

for(ar& car%o &oor in&icatin% a

malfunction*

means*

A

,

C

Oer(in% e:its an& ri%ht rear &oor sli&es

are arme&9 left for(ar& ca'in &oor an&

for(ar& car%o &oor in&icate a

malfunction*

The left for(ar& ca'in &oor an& the

for(ar& car%o &oor are unloce&9 the

oer(in% e:its an& the ri%ht rear &oorsli&es are arme&*

>2

"ou are a'out to perform a taeoff* "ou &onJt hae

inserte& a F-#H temperature


93/100


F-#H/MCT*

TO/GA*

inserte& a F-#H temperature*

6hich thrust leer &etent shall 'e use& for taeoff7

A

,

C

F?--*

C-M,*

>3

"ou are performin% a taeoff (ith the thrust leers


94/100


in the F-#H position* s A/TR no( actie7

A

,

"es*

No*

>@

"ou are performin% a taeoff (ith TOGA po(er*

6h & h A/TR ' i 7


95/100


As soon as +ou en%a%e the autopilot*

As soon as the thrust leers are pulle&

'ac into the C-M, position*

6hen &oes the A/TR 'ecome actie7

A

,

C

As soon as the thrust leers are pulle&

'ac into the F-#H position*

As soon as +ou push the A/TR p'

manuall+ on*

>=

6hat &oes an am'er R#< in&ication mean7


96/100


The reersers are stuc*

The reersers are unloce&*

6hat &oes an am'er R#< in&ication mean7

A

,

C

The reersers are fault+*

The reersers are full+ &eplo+e&*

>;

6hat is the meanin% of an am'er FA?-T li%ht on

th #NG l7


97/100


t in&icates a failure in the en%ine fire

e:tin%uishin% s+stem*

the #NG panel7

A

,

C

t in&icates a failure in the automatic start

se)uence*

t in&icates an en%ine failure*

>B

On the #CAM #/6 pa%e9 (hat is the meanin% of

th ' C5 i &i ti 7


98/100


t is an in&ication of a &iscrepanc+

'et(een the &i%ital #GT in&ication an&

the alue in&icate& '+ the nee&le*


'et(een the alue sho(n on the #CAM

an& the real alue*

the am'er C5 in&ication7

A

,

C

t is an in&ication that the #GT of #NG 1 is

out of the normal ran%e*


'et(een #GT of #NG1 an& #NG2*

C

H

ENG 1 EGT DISCREPANC!

>

6hich step of a manual start is taen oer '+ the

FA#C7


99/100


Fuel flo( start*

!tarter en%a%ement*

FA#C7

A

,

C

%nition start*

%nition cutout*

>>

From #CAM #/6 an& ! en%ine pa%es

&eterminate (hich step of a manual start is taen


100/100

Fuel flo( start*

%nition start*

p

oer '+ the FA#C7

A

,

C

!tarter ale closure*

!tarter ale en%a%ement*

Documents

Airbus A320 Performance Test