330 T

Question 1

If the BSCU fails, most likely a BRAKES SYS 1(2) FAULT may occur

Answer 1

The crew will be notfied with an ECAM message

Question 2

The APU bleed valve automatically closed by the ECB above …..feet climbing

Answer 2

25000

Question 3

If there is an APU fire in flight, the APU

Answer 3

must be shutdown and the agent manually discharged

Question 4

Although no busses are unpowered, illumination of emergency exit light in the cabin is desired. Which of the following answers is correct?

Answer 4

EMER lights exit signs and the escape path markings will illuminate if the cockpit EMER EXIT LT switch is ON

EMER lights exit signs and the floor path markings will illuminate if the guarded EMER EXIT LT pb on the flight attendant CIDS panel is selected on

Question 5

The fire extinguishing system for the cargo compartment discharges to either the FWD cargo or AFT&BULK cargo compartments depending on whether

Answer 5

The FWD or AFT agent PB is pressed

Question 6

What does two amber lines across the last two digits of the fuel quantity mean?

Answer 6

The fuel quantity indication is inaccurate

Question 7

The pneumatic system supplies high pressure air for

Answer 7

• Hydraulic reservoir pressurization and pack bay ventilation turbofan actuation
• Wing anti ice and water pressurization
• Air conditoning and eng starting

Question 8

When can managed vertical navigation be engaged

Answer 8

Only after managed lateral navigation has been engaged

Question 9

The audio managment system includes how many audio control panels

Answer 9

3

Question 10

The APU is supplying the elec system. What is the order of priority for the different generators?

Answer 10

Engines, External Power, APU

Question 11

When both ENG1 and 2 pushbuttons are turned ON each engine nacelle is anti-iced by

Answer 11

Independent bleed air source from HP compressors

Question 12

The cabin pressure controllers receive signals from

Answer 12

Pack flow control valve and LGCIU, ADIRS and Engine Interface Unit, FMGC and Proximity Switch Control Unit

Question 13

In the event of low pressure, heavy load users are isolated to give priority to

Answer 13

Rudders elevators ailerons spoilers and braking

Question 14

In the event of low hydraulic pressure the priority valve and pressure maintaining valve give priortiy to primary flight controls and brakes. The pilots:

Answer 14

can neither control nor monitor the priority valve (automaic operation)

Question 15

How many HP ground units can be connected to the crossbleed duct?

Answer 15

One or two

Question 16

What happens when pressure and temperature are not sufficient to supply the corresponding engine bleed valve (low engine speed)

Answer 16

HP valve opens, IP stage remains open

Question 17

Cabin interphone system permits you to speak to

Answer 17

The cabin attendants

Question 18

What is required for the FADEC to compute a reduced thrust setting

Answer 18

A flex temp must be entered on the TakeOFF PERF page on the MCDU

Question 19

With nobody in the cockpit if you have an APU fire which statement is correct

Answer 19

On the ground an APU EMER shutdown automatically occurs and the APU fire bottle will be discharged

Question 20

How are the FMAs displayed on the PFD

Answer 20

There are 5 columns and 3 rows

Question 21

At what power levels does window heat operate when airborne?

Answer 21

Normal power while inflight

Question 22

Autobrakes if selected will be only activated by

Answer 22

The ground spoiler extension command

Question 23

If a flight attendant opens the door with the escape slide armed

Answer 23

A white warning light warns that the slide is armed

Question 24

During engine start up when is the BLUE hydraulic sys pressurized

Answer 24

Automatically after first engine start (ENG1)

Question 25

Ground dependent position determining systems such as VOR DME or ILS

Answer 25

Cross check and refine the FMGS positions computed by independent systems such as ADIRS

Question 26

Each passenger door has one CABIN Pressure warning light that

Answer 26

Warns of residual pressure in the cabin

Question 27

What are the AP functions

Answer 27

Acquisition and tracking of a flight path Stabilisation of the aircraft around its centre of gravity Automatic landing and go around

Question 28

The fault light for the T.Tank.Mode pb switch on the fuel control panel comes on amber when

Answer 28

Excess aft CG has been detected FCMC is unable to carry out the forward transfer FUEL LO Temp warning is triggered

Question 29

Hot air from the pneumatic system provides wing anti ice to

Answer 29

The four outboard slats

Question 30

During normal flight, the avionics ventilation system controls the temperature by

Answer 30

Blowing air through the underfloor extract valve Extract air from the different panels and equipment racks Using cabin fans recirculated air from the cabin

Question 31

Alpha floor protection is avbl

Answer 31

From liftoff and down to 100ft radio altitude in landing configuration

Question 32

How is it determined that the cockpit sliding window is closed and locked

Answer 32

The red coloured indicator on the top of the handle should completely flush and the red colours not be visible

Question 33

Automatic transfer from the outer tanks to the inner tanks occurs when the center and trim tank have been emptied and either inner tank reaches ......kg

Answer 33

3500kg 7700lbs

Question 34

Automatic control of CG

Answer 34

begins when climbing through FL255 is terminated when descending through FL245 is terminated when FMGC time to destination is below 35min

Question 35

When the door arming lever is in the ARM position opening the door from the outside will

Answer 35

Disarm the door

Question 36

The electric standby horizon ISIS normally draws current from the DC ESS bus. In case of total electric failure the indication remains usuable for ....minutes

Answer 36

Normal function in ELEC EMER config

Question 37

What causes a DU to display a black screen with a white diagonal line

Answer 37

DMC failure

Question 38

Engine fire detection loops are installed in the

Answer 38

Pylone, nacelle and engine core sections

Question 39

For engine start HP air supplied from the ground air source

Answer 39

is not regulated

Question 40

How does the FMGC derive Vapp

Answer 40

Vapp=Vls +1/3 surface headwind component or VLS+5kts whichever is highest

Question 41

The fire ext sys for the cargo compartmend discharges through either the .... in the FWD compartment or through ...in the AFT&Bulk cargo compartment

Answer 41

Two nozzles / one nozzle each

Question 42

How many thrust lever positions are there, and how are they labeled?

Answer 42

4 TL positions - TOGA FLX/MCT CL IDLE

Question 43

Which statement is correct regarding the illumination of the amber BULK ISOL VALVE fault light?

Answer 43

Either the inet or outlet isol valve is not in the selected position

Question 44

The APU master SW Fault light will illuminate

Answer 44

When an automatic shutdown of the APU occurs

Question 45

You want to open the cabin door whilst lifting the control handle the white light illuminates. What does that mean

Answer 45

The slide is still armed

Question 46

What are the correct positions for the PFD and ND

Answer 46

PFD should be outboard and the ND should be inboard

Question 47

How longs does an alignment take

Answer 47

app 10´

Question 48

With the EMER EXIT LT selector in the ARM pos if partial loss of the normal AC power supply

Answer 48

The overhead emergency lights will illuminate automatically

Question 49

The two center tank transfer pumps transfer fuel from the center tank to the ....tanks

Answer 49

inner

Question 50

The APU generator has priority over ....for AC Bus2

Answer 50

External Power B

Question 51

What is the signification of an amber RAT indicator during flight phases 1 and 2 ECAM HYD page

Answer 51

Pressure for stowing RAT has been applied or the RAT pump is not avbl

Question 52

Both independent cabin px controllers receive signals from

Answer 52

LGCIU ADIRS FMGEC PSCU EIU and flow control valves

Question 53

If the thrust levers are set IDLE detent is Alpha floor protection still avbl?

Answer 53

Yes TL pos is disregarded

Question 54

There are .... HP ground air supply connector located on the lower center fuselage

Answer 54

2

Question 55

Opening a passenger door from the outside disarms the door and escape slides

Answer 55

True

Question 56

How can you get mechanics attention when he is outside the aircraft

Answer 56

Use the MECH pb on the CALLS panel which sounds an external horn

Question 57

What is required to arm the Autobrakes?

Answer 57

Green hydraulic pressure avbl, anti skid, no failures in the braking system

Question 58

Illumination of the SEL indicator on a Radio Managment Panel indicates

Answer 58

A transceiver normally asociated with one RMP is tuned by another

Question 59

The override switch for the service interphone switch is located on the ... and is used for maintenance purposes only

Answer 59

overhead panel

Question 60

The green hydraulic circuit drives an emergency generator that automatically supplies emergency AC power to the aircraft electrical system in case of main generators loss

Answer 60

True

Question 61

INFLIGHT a yellow IR fault light is teady ON. What does that mean?

Answer 61

The respective IR is lost

Question 62

The APU air intake and an electrically operated flap allow air to reach the compressor inlet

Answer 62

True

Question 63

The APU is fed from the engine 1 collector in the left inner tank through the APU FWD pump and the APU isol valve when

Answer 63

On Ground after two minutes when the trim tank is not refueled

Question 64

Which situation will automatically illuminate the escape path lighting

Answer 64

The loss of power to the DC ESS Bus and the loss of normal electrical power

Question 65

Which one of the following statements is true

Answer 65

When the engine anti-ice is operating continous ignition is automatically activated

Question 66

While operating on Emergency Electrical Power with the landing gear lowered which of the following control laws is in effect?

Answer 66

Direct

Question 67

TAT probes are heated on the ground

Answer 67

False

Question 68

Which of the following have automatic fire extinguishing systems

Answer 68

APU and lavatory waste bins

Question 69

You enter the dark cockpi what action is necessary before checking the main battery voltages

Answer 69

You have to verify both batteries are off

Question 70

After the engine shutdown you observe a pulsing STS message What does that mean

Answer 70

It is a remainder that the status page holds a maintenance message

Question 71

During a routine flight which of the following would result after the loss of GEN2 and the subsequent start of the APU

Answer 71

ENG GEN1 continues to power AC Bus1 and downstream systems. The APU powers AC Bus 2 and downstream systems...

Question 72

Air bleed from the engines is

Answer 72

cooled by air to air heat exchanger using air bleed from engine fan

Question 73

How many FADEC are installed

Answer 73

2 - 1 per eng

Question 74

If the VHF3 transmisison key illuminated amber showing the word CALL

Answer 74

indicates a SELCAL

Question 75

Automatic cranking is provided

Answer 75

by the FADEC following an automatic start abort

Question 76

What does HORN shutoff on the EVAC panel do

Answer 76

Silences horn in the cockpit

Question 77

When the TL are moved to the TO position the FMGS updates its position at TO using

Answer 77

The NAV databse and the TO RWY entered into the MCDU by the pilot

Question 78

The .... allows the pilot to select on the ECAM either warning and caution messages or system and system status messages displayed

Answer 78

ECAM control panel

Question 79

Wht happens to the cockpit door with electrical power failure

Answer 79

it automatically unlocks

Question 80

You are about to TO but no FLEX is inserted. Can you still take off?

Answer 80

Yes only using TOGA

Question 81

What does the AMBER level indicate on the HYD QTY indic?

Answer 81

Warning level

Question 82

With the engines off if the AVAIL LT is lilluminated on both the APU start pb and the EXT PWR pb what is the active source of ELEC pwr for the AC busses?

Answer 82

APU

Question 83

APU bleed air supplies the pneumatic system if the APU speed is above ..

Answer 83

95%

Question 84

After extending the RAT is it possible to check its position and status

Answer 84

Yes select ECAM HYD page

Question 85

With reference to the PROBE WINDOW heat pb in normal position AUTO which of the following is true

Answer 85

Window heating comes on automatically after first engine start

Question 86

What does the Low Accuracy message mean

Answer 86

The estimated position uncertainty EPU exceeds the RNP

Question 87

What does the LDG GEAR GRVYT EXTN selector handle initiate when selected DOWN

Answer 87

Close the HYD cutoff valve, disengage doors and gear unlocks

Question 88

What is the function of APU GEN pb located on the OVHD CTRL panel

Answer 88

When selected to OFF the APU generator field is de-energized

Question 89

What does the AMBER speed brakes mean on the lower ECAM

Answer 89

Speed brakes are extened and eng are not idle

Question 90

After a single DMC failure how could a crew recover the DU ?

Answer 90

Rotate the EIS DMC switch on the switching panel to replace the failed DMC with DMC3

Question 91

Which hyd system supply presure to the landing gear system

Answer 91

Green

Question 92

When is the SRS active

Answer 92

At TO when TOGA or FLX power is set SRS is displayed on the FMA and provides guidance up to the acc altitude During GA after the TL are placed to the TOGA position up to ACC ALT

Question 93

If battery voltage is below minimum how do you charge them

Answer 93

I have to check tht the BAT pb are on and switch the EXT power on

Question 94

The landing gear consists of

Answer 94

two inb retracting main gears a forward retrating nose gear

Question 95

When the APU fire pb is released out an elec signal is sent that

Answer 95

``` Shuts down the APU and silences the CRC Arms the APU ext squib closes LP fuel valve shuts off apu fuel pumps closes the apu bleed valve and deactivates apu generator ```

Question 96

The pack flow control valve are pneumatically operated and electrically controled. They close automatically in case of

Answer 96

Pack overheating, operation of the fire or ditching pb insufficent upstream air pressure engine starting and any unclosed doors at eng start

Question 97

While flying the airplane with A7THR active, the speed know is pulled and turned to a selected speed that happens to be slower than Alpha Prot. What speed will the aircraft slow to

Answer 97

VLS

Question 98

What are the different types of Flight guidance

Answer 98

Managed and selected