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Question 1

How many electric booster pumps are there in total for the center and inner cell tanks for A321?

Answer 1

4

Question 2

What type of slide (pertaining to lane) is mounted for the overwing emergency exit?

Answer 2

Dual lane

Question 3

The A320 family structure is composed of

Answer 3

Answer. Aluminum Alloy and Carbon Fiber Reinforced Plastic

Question 4

Potable water & lavatory servicing is disallowed in order to avoid

Answer 4

Answer. Cross Contamination

Question 5

Emergency lights can be controlled from

Answer 5

Answer. From the cockpit and From the Cabin

Question 6

The Integrated Stand by Instrument System (ISIS) replaces the Standby:

Answer 6

Answer. Altimeter, the standby horizon and standby airspeed

Question 7

Z=0 is located

Answer 7

Vertical stbilizer

Question 8

Both pneumatic system is connected by:

Answer 8

Cross bleed valve

Question 9

Where does re-circulated air from the cabin go?

Answer 9

Mixer unit

Question 10

Cabin systems are controlled, tested & monitored by:

Answer 10

CIDS

Question 11

Which of the following conditions could cause automatic relight of the igniters?

Answer 11

Answer. Engine Anti-Ice On

Question 12

Which DMC serves as a back-up for ECAM?

Answer 12

Answer. DMC 2 and 3

Question 13

A19 is equipped with_ _ _ _ _ overwing exits. (Ceb Fleet).

Answer 13

2

Question 14

Light located in the underside of the wings

Answer 14

Landing light

Question 15

In the pushbutton color philosophy, green is used to indicate

Answer 15

Answer. Normal operation of the back-up system

Question 16

Where is the engine fire detectors locate

Answer 16

Answer. On the pylon, fan & the core

Question 17

What among the APU functions are only available during aircraft ON GROUND situation?

Answer 17

Answer. Auto-extinguishing & Auto shutdown

Question 18

The fire protection system includes;

Answer 18

Answer. 2 fire agent bottles for each engine- 1 fire agent
bottle for the APU

Question 19

The APU provides:

Answer 19

Answer. Electrical power for aircraft electrical system & bleed starting & air conditioning

Question 20

Manual radio navigation tuning is done by means of _ _ _ _ _ _,

Answer 20

Answer. Multipurpose Control Display Unit

Question 21

Starter drives what during starting?

Answer 21

N2

Question 22

Which among of the following flight control mechanical back-up?

Answer 22

Answer. THS and Rudder

Question 23

What information is given by the electrical clock?

Answer 23

Answer. Universal Time Coordinated, Elapsed Time, Chronometer

Question 24

WHC 1 control what?

Answer 24

Answer. Left windshield and left side windows

Question 25

What components are electrically-heated to prevent ice formation on their surfaces?

Answer 25

Answer. AOA sensors, pitot tubes, static ports TAT probes, windshield & cockpit side windows, drain masts.

Question 26

Where are the smoke detectors located?

Answer 26

Answer. Lavatories, cargo compartments, avionics bay

Question 27

This is used to transmit and receive audio signals from different communication transceivers and radio navigation and audio reception.

Answer 27

Answer. ACP

Question 28

A flashing amber on the Area Call Panel indicates _ _ _ _ _.

Answer 28

lavoratory smoke

Question 29

Air bleed can be supplied from:

Answer 29

Answer. The engine bleed system and APU, An external HP ground power unit

Question 30

Cabin oxygen system:

Answer 30

Answer. Can be deployed auto in case of rapid decompression, Can be mechanically opened using MRT

Question 31

Which of the following statements is true for the 56-5B engine?

Answer 31

Answer. Has 5 LP compressor stages, 9 HP compressor stages, 4 stages LP turbine, single stage

Question 32

Which of the following statements is true for the 56-5B engine?

Answer 32

Answer. Has 5 LP compressor stages, 9 HP compressor stages, 4 stages LP turbine, single stage

Question 33

All braking functions (NB, A/Skid, AutoB, B temp Indication) are controlled by 2:

Answer 33

BSCU

Question 34

How many spoiler for roll?

Answer 34

Answer. Spoilers 2,3,4,5

Question 35

Yellow hydraulic system is pressurized by:

Answer 35

Answer. EDP/Elec pump and PTU

Question 36

Pre-FANS functions includes

Answer 36

Answer. Communication and AOC functions

Question 37

ECAM DOOR green indications when

Answer 37

Answer. Door is CLOSED and LOCKED

Question 38

On the enhanced version of A320, vacuum system is controlled & monitored by

Answer 38

Answer. CIDS

Question 39

What is the purpose of the Bypass valve?

Answer 39

Answer. Modulate output temperature of the pack & prevent ice formation

Question 40

Electronic Instrument System(EIS) consists of

Answer 40

Answer. 6 display units

Question 41

Auto thrust can be disengaged by:

Answer 41

Answer. Pressing the instinctive disconnect at the thrust control lever

Question 42

Windows is

Answer 42

Answer. ATA 56

Question 43

RAT can be deployed auto/man

Answer 43

Answer. Pressurizes the blue system at 2500psi and Can be retracted on ground only

Question 44

If there are several power suppliers able to deliver correct voltage simultaneously, the AC BUS 1 (2) are supplied in which highest priority.

Answer 44

Answer. By the corresponding generator, GEN 1(2)

Question 45

In AFS, the FG part has 3 functions

Answer 45

Answer. Autopilot, Flight Director, A/THR

Question 46

A319/A320 aircraft is equipped with the following:

Answer 46

Answer. Anti-Skid system, Auto-braking system, brake fans, Tire pressure indicating system

Question 47

Which of the following happens when the fuel in the inner cell reaches the low level?

Answer 47

Answer. Inter-cell transfer valve opens

Question 48

Which of the following statements is true for Pilot oxygen system:

Answer 48

Answer. Enables selection of pure oxygen or mixture of cabin air & pure oxygen, Enables the oxy flow to be tested

Question 49

In emergency configuration with emergency generator not available, BAT 2 supplies the AC ESS BUS via:

Answer 49

Answer. It is not possible BAT 2 supplies DC ESS BUS

Question 50

It gives full time accessibility and readability of messages exchanged with the ATC and both CREW.

Answer 50

Answer. Datalink Control and Display Unit.