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A330 - 200 CMD 2020 > 330 T > Flashcards

330 T Flashcards

1
Q

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

A

The crew will be notfied with an ECAM message

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2
Q

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

A

25000

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3
Q

If there is an APU fire in flight, the APU

A

must be shutdown and the agent manually discharged

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4
Q

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

A

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

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5
Q

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

A

The FWD or AFT agent PB is pressed

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6
Q

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

A

The fuel quantity indication is inaccurate

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7
Q

The pneumatic system supplies high pressure air for

A
  • Hydraulic reservoir pressurization and pack bay ventilation turbofan actuation
  • Wing anti ice and water pressurization
  • Air conditoning and eng starting
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8
Q

When can managed vertical navigation be engaged

A

Only after managed lateral navigation has been engaged

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9
Q

The audio managment system includes how many audio control panels

A

3

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10
Q

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

A

Engines, External Power, APU

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11
Q

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

A

Independent bleed air source from HP compressors

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12
Q

The cabin pressure controllers receive signals from

A

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

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13
Q

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

A

Rudders elevators ailerons spoilers and braking

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14
Q

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

A

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

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15
Q

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

A

One or two

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16
Q

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

A

HP valve opens, IP stage remains open

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17
Q

Cabin interphone system permits you to speak to

A

The cabin attendants

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18
Q

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

A

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

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19
Q

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

A

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

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20
Q

How are the FMAs displayed on the PFD

A

There are 5 columns and 3 rows

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21
Q

At what power levels does window heat operate when airborne?

A

Normal power while inflight

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22
Q

Autobrakes if selected will be only activated by

A

The ground spoiler extension command

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23
Q

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

A

A white warning light warns that the slide is armed

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24
Q

During engine start up when is the BLUE hydraulic sys pressurized

A

Automatically after first engine start (ENG1)

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25
Q

Ground dependent position determining systems such as VOR DME or ILS

A

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

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26
Q

Each passenger door has one CABIN Pressure warning light that

A

Warns of residual pressure in the cabin

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27
Q

What are the AP functions

A

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

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28
Q

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

A

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

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29
Q

Hot air from the pneumatic system provides wing anti ice to

A

The four outboard slats

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30
Q

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

A

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

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31
Q

Alpha floor protection is avbl

A

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

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32
Q

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

A

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

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33
Q

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

A

3500kg 7700lbs

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34
Q

Automatic control of CG

A

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

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35
Q

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

A

Disarm the door

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36
Q

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

A

Normal function in ELEC EMER config

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37
Q

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

A

DMC failure

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38
Q

Engine fire detection loops are installed in the

A

Pylone, nacelle and engine core sections

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39
Q

For engine start HP air supplied from the ground air source

A

is not regulated

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40
Q

How does the FMGC derive Vapp

A

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

41
Q

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

A

Two nozzles / one nozzle each

42
Q

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

A

4 TL positions - TOGA FLX/MCT CL IDLE

43
Q

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

A

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

44
Q

The APU master SW Fault light will illuminate

A

When an automatic shutdown of the APU occurs

45
Q

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

A

The slide is still armed

46
Q

What are the correct positions for the PFD and ND

A

PFD should be outboard and the ND should be inboard

47
Q

How longs does an alignment take

A

app 10´

48
Q

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

A

The overhead emergency lights will illuminate automatically

49
Q

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

A

inner

50
Q

The APU generator has priority over ….for AC Bus2

A

External Power B

51
Q

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

A

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

52
Q

Both independent cabin px controllers receive signals from

A

LGCIU ADIRS FMGEC PSCU EIU and flow control valves

53
Q

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

A

Yes TL pos is disregarded

54
Q

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

A

2

55
Q

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

A

True

56
Q

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

A

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

57
Q

What is required to arm the Autobrakes?

A

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

58
Q

Illumination of the SEL indicator on a Radio Managment Panel indicates

A

A transceiver normally asociated with one RMP is tuned by another

59
Q

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

A

overhead panel

60
Q

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

A

True

61
Q

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

A

The respective IR is lost

62
Q

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

A

True

63
Q

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

A

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

64
Q

Which situation will automatically illuminate the escape path lighting

A

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

65
Q

Which one of the following statements is true

A

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

66
Q

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

A

Direct

67
Q

TAT probes are heated on the ground

A

False

68
Q

Which of the following have automatic fire extinguishing systems

A

APU and lavatory waste bins

69
Q

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

A

You have to verify both batteries are off

70
Q

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

A

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

71
Q

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

A

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

72
Q

Air bleed from the engines is

A

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

73
Q

How many FADEC are installed

A

2 - 1 per eng

74
Q

If the VHF3 transmisison key illuminated amber showing the word CALL

A

indicates a SELCAL

75
Q

Automatic cranking is provided

A

by the FADEC following an automatic start abort

76
Q

What does HORN shutoff on the EVAC panel do

A

Silences horn in the cockpit

77
Q

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

A

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

78
Q

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

A

ECAM control panel

79
Q

Wht happens to the cockpit door with electrical power failure

A

it automatically unlocks

80
Q

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

A

Yes only using TOGA

81
Q

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

A

Warning level

82
Q

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?

A

APU

83
Q

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

A

95%

84
Q

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

A

Yes select ECAM HYD page

85
Q

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

A

Window heating comes on automatically after first engine start

86
Q

What does the Low Accuracy message mean

A

The estimated position uncertainty EPU exceeds the RNP

87
Q

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

A

Close the HYD cutoff valve, disengage doors and gear unlocks

88
Q

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

A

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

89
Q

What does the AMBER speed brakes mean on the lower ECAM

A

Speed brakes are extened and eng are not idle

90
Q

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

A

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

91
Q

Which hyd system supply presure to the landing gear system

A

Green

92
Q

When is the SRS active

A

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

93
Q

If battery voltage is below minimum how do you charge them

A

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

94
Q

The landing gear consists of

A

two inb retracting main gears a forward retrating nose gear

95
Q

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

A 
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
96
Q

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

A

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

97
Q

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

A

VLS

98
Q

What are the different types of Flight guidance

A

Managed and selected

A330 - 200 CMD 2020 (10 decks)

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