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Airbus Stuff > System Questions 2 > Flashcards

System Questions 2 Flashcards

1
Q

The ECAM HYD page display shows that:

A

The ENG 2 FIRE pb has been pressed.

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2
Q

In the Yellow system, hydraulic fluid is currently prevented from flowing to the engine driven pump. Based on the ECAM, the Yellow hydraulic system is being pressurized via the ELEC Pump.

A

False

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3
Q

The Green hydraulic system can be pressurized by:

A

The #1 engine-driven pump or the PTU.

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4
Q

The Yellow hydraulic system can be pressurized by:

A

The #2 engine-driven pump, the PTU, an electric pump or a hand pump.

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5
Q

The Blue hydraulic system can be pressurized by:

A

An electric pump or a RAT-driven pump.

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6
Q

When there is a hydraulic system non-normal, the ______will also alert the pilots.

A

E/WD

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7
Q

When the PTU is operating:

A

Pressure transfers between the Green and Yellow systems.

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8
Q

Once deployed, how can the RAT be stowed?

A

Only on the ground by maintenance personnel.

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9
Q

What cockpit lighting is available in EMERG ELEC CONFIG?

A

Dome light over the FO’s seat CA instrument flood lights

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10
Q

What does the highlighted switch control?

A

Dome lights above the Captain’’s and FO’s seats.

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11
Q

Where are the EXT LT switches located?

A

Overhead panel

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12
Q

The airspeed limitation for the retractable landing lights is 290kts.

A

False

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13
Q

With the EMER EXIT LT switch set to ARM, which cabin light(s) is/are armed to illuminate automatically if AC BUS 1 is unpowered?

A

Overhead emergency lights

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14
Q

With AC BUS 1 unpowered, what is the normal source of power for the Emergency lights?

A

DC ESS SHED BUS

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15
Q

With DC ESS SHED BUS shed, all three sets of emergency lights are powered by self-contained battery packs.

A

True

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16
Q

In this EXT LT configuration, the Strobe lights are:

A

OFF

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17
Q

5b. In this EXT LT configuration, the Strobe lights are:

A

AUTO

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18
Q

The smaller light on the nose landing gear is the:

A

Taxi Light

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19
Q

The larger light on the nose landing gear is the:

A

Takeoff light

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20
Q

When the NOSE light switch is placed in the Taxi position:

A

Only the smaller taxi light illuminates

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21
Q

When the NOSE light switch is in the T.O. position:

A

Both lights on the nose gear are illuminated

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22
Q

The nose gear lights remain on when the nose gear retracts.

A

False

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23
Q

What are the arrows pointing toward on the nose gear?

A

Runway turnoff lights

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24
Q

With the Strobe lights in AUTO:

A

Strobe lights only operate when the aircraft is in flight

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25
Q

The smaller light on the nose landing gear is the:

A

Taxi Light

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26
Q

The larger light on the nose landing gear is the:

A

Takeoff light

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27
Q

When is the GND symbol displayed on the SD ECAM BLEED Page?

A

Whenever the aircraft is on the ground

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28
Q

The Bleed Monitoring Computers (BMCs) command the engine bleed valves to close whenever:

A

One or more bleed leaks are detected.
Excessive pressure or temperature is detected.
Reverse airflow is detected.

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29
Q

Engine and APU bleed air are the only air sources for the pneumatic system.

A

False

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30
Q

Which pb would you press to manually close this valve?

A

ENG 1 BLEED pb

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31
Q

The pneumatic system is displayed on which SD ECAM page?

A

BLEED

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32
Q

When engines are running, their bleed sources have priority over the APU bleed source and the APU bleed valve automatically closes.

A

False

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33
Q

With the X BLEED knob in the AUTO position, the crossbleed valve opens and closes in response to the:

A

APU bleed valve

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34
Q

While in AUTO, the crossbleed valve will also automatically close in response to a bleed leak.

A

True

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35
Q

Above what altitude must the APU bleed valve be closed?

A

20,000ft

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36
Q

The APU bleed valve is spring-loaded to the closed position in the absence of air flow.

A

True

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37
Q

With this GPWS panel configured as shown, which statement below is true?

A

All five of the GPWS basic mode warnings are inhibited.

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38
Q

Select the correct alerting priority order.

A
  1. Stall warnings,
  2. Windshear warnings,
  3. GPWS warnings,
  4. TCAS warnings.
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39
Q

You must make sure the loudspeakers are turned up loud enough so that you can hear the aural GPWS warnings.

A

False

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40
Q

If the TERR ON ND pb is selected to OFF:

A

Terrain alerting will still be available for predictive warning of High Terrain ahead of the aircraft.

41
Q

As the aircraft approaches within 750ft of the selected FCU altitude with the A/P off:

A

The aural alert sounds and the PFD`s altitude window pulses yellow.

42
Q

Reactive windshear warnings function during takeoff and landings:

A

Below 1300ft AGL and at configuration Flaps 1 or greater.

43
Q

The Terrain Clearance Floor is:

A

Not predictive. The aircraft must actually penetrate the TCF to trigger a warning.

44
Q

Pressing the T.O. Config. key on the ECAM control panel:

A

Simulates the application of Takeoff Thrust.

45
Q

Which item causes a takeoff configuration warning when the thrust levers are placed to a takeoff thrust setting while on the ground but does not cause a warning when the T.O. CONFIG key is pressed after engine start?

A

Parking brake set to ON.

46
Q

The T.O. CONFIG warning system is activated automatically when you bring the thrust levers to a takeoff thrust setting while on the ground.

A

True

47
Q

To use the PA handset to make a PA announcement:

A

You press the PTT switch on the handset and hold while talking.

48
Q

Which radio is normally dedicated to ACARS communications?

A

VHF 3 is dedicated to ACARS but can be used for voice communications if needed.

49
Q

VHF 3 can also be used as an additional radio for voice communications if necessary.

A

True

50
Q

The transfer key is used to transfer the frequency displayed in the STBY window to the ACTIVE frequency window.

A

True

51
Q

For HF radios, the HF radio antenna must be tuned by pressing a PTT selector. A tone is briefly heard, confirming the antenna tuning.

A

True

52
Q

The CVR operates automatically:

A

For the first 5 minutes after AC power is applied to the aircraft.
When the first engine is started.
Anytime the aircraft is airborne

53
Q

Which transmission key alerting light does NOT extinguish automatically after a short period of time if the RESET pb is not used?

A

CALL

54
Q

The ACP is the:

A

Audio Control Panel

55
Q

The Radio Management Panels, RMPs, are used:

A

Exclusively to tune frequencies for various radios, including navaids if necessary

56
Q

The RMP is the:

A

Radio Management Panel

57
Q

The selection of a transmission key does not select that communications device for reception.

A

True

58
Q

The SEL light illuminates on both RMPs when:

A

RMP is selected to a non-dedicated radio

59
Q

An amber CALL light flashing on VHF means:

A

A SELCAL from a ground radio station has been received.

60
Q

Which of the following does NOT have a fire extinguishing system installed?

A

Avionics compartment

61
Q

Which statement is true regarding cargo compartment fire extinguishing, except the A321H?

A

There is only one halon fire bottle. It can be discharged into either compartment, but not both.

62
Q

Which statement accurately describes each engine’s dedicated fire detection system?

A

The Fire Detection Unit will alert you to an engine fire if both fire detection loops detect a heat rise.
The Fire Detection Unit will alert you to an engine fire if both fire detection loops fail with a few seconds of each other.
The Fire Detection Unit will alert you to an engine fire if one fire detection loop detects a heat rise and the other is determined to be faulted.

63
Q

Which indications appear in the flight deck after an APU fire has been extinguished on the ground?

A

The APU FIRE pushbutton light is not illuminated, while the AGENT DISCH light is illuminated .

64
Q

All of these areas on the A319 have fire detection. Which of these has fire detection but no fire protection?

A

Avionics bay

65
Q

What section of the engine does not have Fire Detection Loops?

A

Exhaust

66
Q

The APU automatically shuts down and discharges a fire bottle when a fire is detected on the ground.

A

True

67
Q

If Avionics Smoke is detected, what system page comes up automatically on the lower ECAM?

A

ELEC

68
Q

Cargo compartment smoke detection is provided by:

A

Particulate sensing smoke detectors, located in both cargo compartments.

69
Q

Why does the Smoke Light continue to illuminate after the Cargo Agent has been discharged?

A

Particulates are still present and have not settled.

70
Q

The lavatory smoke detection system:

A

Provides indications in both the flight deck and cabin that smoke has been detected in a lavatory, with the specific lavatory identified in the cabin.

71
Q

The DISCH amber light on the ENG 1 Fire panel indicates:

A

The halon bottle is discharged.

72
Q

When icing conditions exist, when should engine anti-ice be selected on?

A

During all ground and flight operations.

73
Q

The Airfoil anti-ice system provides protection for the following?

A

The three outboard slats

74
Q

Under what ECAM page would you get information about the anti-ice system?

A

BLEED

75
Q

Which statement is correct regarding rain repellent?

A

It can be used in moderate to heavy rain conditions.

76
Q

When will the window and the probe heat come on with the PROBE/WINDOW HEAT pushbutton in the AUTO position?

A

After the first engine is started

77
Q

Probe heat can be activated prior to engine start by:

A

Pressing the PROBE/WINDOW HEAT pushbutton.

78
Q

If an APU Fire is detected on the ground:

A

The APU automatically shuts down and the halon extinguisher is automatically discharged.

79
Q

The APU may be started and operated in flight. Which of the following is also true?

A

The APU may be operated up to the maximum certified pressure altitude of 39,000 feet.

80
Q

You have just selected the APU MASTER SW pb to ON. You now select the APU START pb to ON. Which statement is correct?

A

The ECB will not engage the electric starter until the power-up self test is completed satisfactorily and the air intake flap is fully open.

81
Q

How do you start the APU?

A

Press the APU MASTER SW pushbutton, followed 5 seconds later, by the APU START pushbutton.

82
Q

Normally, how do you shut down the APU?

A

Press the APU MASTER SW pushbutton only.

83
Q

The APU generator has the same power output as an engine generator.

A

True

84
Q

Fuel for APU operation is normally supplied from:

A

The left fuel feed line, through the engine 1 feed line.

85
Q

Automatic control of the avionics ventilation system is provided by:

A

A single Avionics Equipment Ventilation Computer (AEVC).

86
Q

You can monitor the operation of the avionics ventilation system inlet and extract valves:

A

On the CAB PRESS page.

87
Q

To cool avionics ventilation air, the skin heat exchanger:

A

Uses the temperature of the exterior of the aircraft’s fuselage in certain modes of operation.

88
Q

The open configuration of the avionics ventilation system:

A

Uses outside air to ventilate the avionics equipment.

89
Q

Status of the Avionics Ventilation System may be monitored on the:

A

CAB PRESS page.

90
Q

The fwd cargo compartment on some aircraft:

A

Is heated and ventilated.

91
Q

Heating, if installed, for the fwd cargo compartment:

A

Is provided by a trim air system.
Is controlled automatically by a cargo heat controller.
Can be adjusted from the flight deck.

92
Q

In the open configuration, the skin heat exchanger isolation valve is ____ and the heat exchanger is ____

A

Closed / bypassed.

93
Q

If the AEVC senses smoke in the avionics compartment, an Avionics Smoke Caution is generated and after placing the Blower pb and Extract pb to override, the following is accomplished:

A

The blower fan stops.
The inlet valve remains closed, or closes if open.
The air conditioning inlet valve opens.

94
Q

Unlike the normal operating configurations, the Avionics Smoke Configuration doesn’t occur automatically, and the crew must manually set the Avionics Smoke Configuration by:

A

Using the Blower pb and Extract pb.

95
Q

In the event of a forward cargo compartment overheat condition, or if the Hot Air pb is selected to OFF, the Trim Air Valve closes and airflow to the forward cargo compartment is shut off.

A

True

96
Q

The closed configuration of the avionics ventilation system:

A

Is used on the ground during cold ambient conditions.
Is used during flight.
Utilizes the skin heat exchanger.

97
Q

Once engine bleed air is available to the packs, if pack flow selector is selected to Low, what percentage of normal flow is provided?

A

80%

98
Q

HI flow rates are automatically commanded regardless of Pack Flow selector position when:

A

D. Both A and B
A. Operating on a single pack
B. The APU is the sole source of bleed air

Airbus Stuff (5 decks)

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