test

Question 1

1) The datum (the zero reference) is?

Answer 1

2.4 Meter forward of the radum nose.

Question 2

2) Green ck/b is monitored by?and what will display?

Answer 2

flight warning computer and ECAM message will display.

Question 3

3) Red warning light on the push button required

Answer 3

an immediate action.

Question 4

4) The Navigation display (ND) cannot display on what?

Answer 4

the lower ECAM.

Question 5

5) Turning radii depending on what?

Answer 5

the effective turning angle and the steering angle.

Question 6

6) The electric instrument system (EIS) divided into how many system(s)?

Answer 6

two systems:

a) EFIS
b) ECAM.

Question 7

7) Function of (SDAC) is to:

Answer 7

convert analog data (info.) in to digital signal.

Question 8

8) What is BITE?

Answer 8

Built in Test Equipment.

Question 9

9) If the red guarded switch located on the emergency electric panel is pushed what will happen?

Answer 9

the RAT will drop W or W/O electric power.

Question 10

10) When the RAT is extended it will power what?

Answer 10

the Blue hydraulic system.

Question 11

11) On the external power panel the Blue light indicate what?

Answer 11

the flight crew trying to contact the ground personal.

Question 12

12) The (MCDU) provides ____ term flight information and the (FSU) provides the ______ term flight information.

Answer 12

LONG,SHORT

Question 13

13) Aircraft position determination is computed by what?

Answer 13

the management part of (FMGC).

Question 14

14) The automatic selection of navigation frequency is made by what?

Answer 14

the management part of the (FMGC).

Question 15

15) The flight guided functions are?

Answer 15

the autopilot, the flight direction and the auto thrust.

Question 16

16) The nose wheel can be controlled by what , where and when?

Answer 16

the autopilot on the ground during landing.

Question 17

17) On cruise with autopilot 1 is engaged and autopilot 2 selected what will happened to 1 &2?

Answer 17

1 disengages and 2 will become active.

Question 18

18) During the (ILS) approach it’s recommended to do what?

Answer 18

engage the second autopilot for backup.

Question 19

19) The YAW damper provides what 4 things?

Answer 19

the dutch roll damping, YAW guidance order execution, turn coordination and engine failure compensation.

Question 20

20) The basic functions of (FAC) are?

Answer 20

rudder control and flight envelope protection.

Question 21

21) (FMGC) controlled through what and what?

Answer 21

(MCDU) and (FCU).

Question 22

22) Pressing the reset button for the rudder trim enable what and when?

Answer 22

the rudder trim to the neutral position when the autopilot is not engaged.

Question 23

23) The YAW damper actuator does not move what?

Answer 23

the rudder puddles.

Question 24

24) (FAC) Alpha floor detection =

Answer 24

the auto thrust automatically engaged with full thrust.

Question 25

25) A blue light illuminating on the cabin area call panel indicate what?

Answer 25

passenger call.

Question 26

26) The portable is serviced from what?

Answer 26

the water service penal.

Question 27

27) Fuselage ATA code is ?

Answer 27

53

Question 28

28) Have the _____ fire extinguisher on hand when operating the APU with the APU door _____ .

Answer 28

correct , open

Question 29

29) Primary structure of the engine pylon are?

Answer 29

titanium alloy and steel.

Question 30

30) The direct law do what?

Answer 30

provides no flight protection.

Question 31

31) The normal law do what?

Answer 31

prevents aircraft from stalling.

Question 32

32) The tire pressure indicating system (TPIS) continuously monitors what?

Answer 32

the absolute pressure of each individual tire.

Question 33

33) On the walk around, the yellow oxygen discharge indicator is indicate what?and the pilot has to do what?

Answer 33

that the oxygen has discharged,notify the technician.

Question 34

34) A red cargo door indicator is indicating what?

Answer 34

that the cargo door is unlocked.

Question 35

35) APU has automatic fire extinguishing on the ____ ____.

Answer 35

ground only.

Question 36

36) APU can supply electrical power throughout the what level of flight?

Answer 36

entire flight envelope.

Question 37

37) Maximum cabin altitude allowed on commercial passenger aircraft is _____.

Answer 37

8000 ft.

Question 38

38) The passenger oxygen mask can be deployed in 3 types:

Answer 38

automatically, electrically and mechanically.

Question 39

39) Air-conditioning zones temperature are display where?

Answer 39

on ECAM air-conditioning system display (SD).

Question 40

40) Class 1 failure priority is what?

Answer 40

most serious and immediate maintenance action required.

Question 41

41) Discharge of the lavatory fire extinguisher happened from what?

Answer 41

heat that melts the eutectic solder.

Question 42

42) (CFM) 56 engine hydraulic controlled thrust reverse can be deployed where and when?

Answer 42

on the ground after the ground spoilers are deployed.

Question 43

43) The programming plug in Electronic engine control (EEC) changes what ?

Answer 43

changes the available thrust.

Question 44

44) The engine accessory gearbox is driven by what?

Answer 44

the high pressure N2.

Question 45

45) Standard visual ice indicator is located where?

Answer 45

on the fuselage between the windshields.

Question 46

46) The over pressure valve (OPV) is used for what?

Answer 46

backup if the pressure regulating valve (PRV) fails to limit the output pressure.

Question 47

47) Respective cargo heat controls what?

Answer 47

the cargo compartment trim air valve.

Question 48

48) The check valve prevents reverse flow into intermediate compressor (IP) when what?

Answer 48

the high stage (HP) valve is open.

Question 49

49) On A320 (319-318) fuel system the cross feed valve is what?

Answer 49

normally closed (NC).

Question 50

50) Engine fire detection loop A & B operate in what?

Answer 50

parallel.