Aircraft Systems Quiz Questions
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Questions and Answers

What does the amber CABIN PRESSURE warning light on each passenger door indicate?

  • Warns of residual pressure in the cabin
  • Shows a possible unlocked door (correct)
  • Both a and b are correct
  • None of the above

Where are the warnings generated by the Door and Slide Control System (DSCS)?

  • On ECAM (correct)
  • On the doors
  • Both a and b are correct
  • None of the above

What happens to the cockpit door in case of an electrical power failure?

  • It operates normally on HOT BAT bus
  • It automatically unlocks
  • It automatically locks from outside but stays unlock from inside (correct)
  • None of the above

Are the cockpit windows capable of being opened both from inside and outside?

<p>False (A)</p> Signup and view all the answers

What does the white slide armed light on the main cabin door indicate?

<p>The main cabin door has not been properly closed (C)</p> Signup and view all the answers

What is the purpose of the safety valve?

<p>To avoid excessive positive pressure differential (B)</p> Signup and view all the answers

Can the flight compartment sliding windows be used as emergency exits?

<p>No, they are not approved emergency exits (D)</p> Signup and view all the answers

Where is the landing elevation sent to when set to AUTO?

<p>FCU (D)</p> Signup and view all the answers

How do the air conditioning packs operate once set to 'ON'?

<p>Automatically, pack one as a master, pack two as a slave (C)</p> Signup and view all the answers

What is the mixing unit connected to?

<p>Packs, emergency ram air inlet, and LP ground connector (C)</p> Signup and view all the answers

When is the emergency ram air inlet valve activated?

<p>Diff.press &lt; 1 psi, and ditching not selected (C)</p> Signup and view all the answers

Which system is responsible for sending the landing elevation to the controller?

<p>FCU (C)</p> Signup and view all the answers

What does the message 'CTR TK FEEDG' in the MEMO indicate?

<p>At least one center tank pump is energized. (C)</p> Signup and view all the answers

From which fuel tanks will fuel gravity feed?

<p>Inner cell of the wing tanks, and center tank. (A)</p> Signup and view all the answers

Is it possible for center tank pumps to stop 5 minutes after reaching a low level?

<p>It is not possible to determine their position. (A)</p> Signup and view all the answers

When do fuel transfer valves open during normal operations?

<p>When a low level is sensed in the center tank. (D)</p> Signup and view all the answers

What does an amber line across the last two digits of the fuel quantity indicate?

<p>A disagreement between fuel measured and fuel entered on the MCDU has been detected. (C)</p> Signup and view all the answers

How does the APU fuel system obtain fuel?

<p>Obtains fuel from the left fuel manifold via the left side fuel pumps or if needed, the APU fuel pump. (A)</p> Signup and view all the answers

When will the PTU come into action automatically?

<p>At 500 psi (C)</p> Signup and view all the answers

Under what condition will the yellow system electric pump operate when AC power is available?

<p>When the yellow electric system ELEC PUMP push button is selected to ON or the ground crew activates a cargo door switch (D)</p> Signup and view all the answers

What is the normal pressure in the hydraulic system?

<p>2,000 psi (A)</p> Signup and view all the answers

Is it normal for the PTU test not to be activated after starting engine #2?

<p>Yes, the PTU will not work until the second engine has been started (C)</p> Signup and view all the answers

Why does the ECAM procedure ask you to switch off the PTU first when you get a G RSVR OVHT message?

<p>To depressurize the YELLOW and GREEN systems (C)</p> Signup and view all the answers

In hydraulic system malfunctions, when will the RAT deploy?

<p>When hydraulic pressure drops below a certain level (D)</p> Signup and view all the answers

What action is necessary before checking the battery voltages in a dark cockpit?

<p>You have to ensure that at least one battery is on. (C)</p> Signup and view all the answers

How can you get the APU generator to power the electrical system after starting the APU?

<p>By pushing the BUS TIE pushbutton. (A)</p> Signup and view all the answers

Are there any limitations associated with disconnecting an IDG?

<p>Never disconnect an IDG in flight, or push the IDG disconnect push button for more than 30 seconds. (B)</p> Signup and view all the answers

Which voltage requires recharging or replacing the batteries?

<p>24 volts or less. (D)</p> Signup and view all the answers

In what order of priority are the different generators when the APU is supplying the electrical system?

<p>APU, external power, engines. (D)</p> Signup and view all the answers

What is the significance of the green collared circuit breakers?

<p>They highlight manually resettable devices. (B)</p> Signup and view all the answers

Flashcards

Amber CABIN PRESSURE warning light

Indicates a possible unlocked passenger door.

DSCS Warning Generation

Warnings by the Door and Slide Control System appear on ECAM.

Cockpit Door Power Failure

In power failure, the cockpit door locks from outside but remains unlocked inside.

Cockpit Window Opening

Cockpit windows cannot be opened from inside or outside.

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Slide Armed Light

Indicates the main cabin door is not properly closed.

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Safety Valve Purpose

Prevents excessive positive pressure differential.

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Emergency Exit Windows

Flight compartment sliding windows are not emergency exits.

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Landing Elevation AUTO

Sent to the Flight Control Unit (FCU) when set to AUTO.

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Air Conditioning Packs Operation

Packs automatically function: pack one as master, pack two as slave when ON.

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Mixing Unit Connections

Connected to packs, emergency ram air inlet, and LP ground connector.

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Emergency Ram Air Inlet Activation

Activated when differential pressure is less than 1 psi and ditching is not selected.

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FCU Role

Sends landing elevation data to the controller.

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CTR TK FEEDG Message

Indicates at least one center tank pump is energized.

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Fuel Gravity Feed Tanks

Fuel feeds from inner wing tanks and center tank.

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Center Tank Pumps Shutdown

Cannot stop 5 minutes after reaching a low level; their position is indeterminate.

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Fuel Transfer Valves Operation

Open during normal operations when low level is sensed in the center tank.

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Amber Fuel Indication Line

Indicates a disagreement between measured and entered fuel quantities.

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APU Fuel System Source

Gets fuel from the left fuel manifold via left pumps or APU fuel pump.

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PTU Automatic Activation

Automatically activates at 500 psi.

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Yellow Electric Pump Operation

Operates when its push button is on or cargo door switch activated.

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Normal Hydraulic Pressure

The normal pressure in the hydraulic system is 2,000 psi.

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PTU Test Activation

Not activated until starting engine #2; normal behavior.

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ECAM Procedure for G RSVR OVHT

Switch off PTU first to depressurize YELLOW and GREEN systems.

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RAT Deployment Condition

Deploys when hydraulic pressure drops below a certain level.

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Battery Voltage Check

Ensure at least one battery is on before checking voltages in darkness.

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APU Generator Powering

APU generator delivers power after pushing BUS TIE button.

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IDG Disconnect Limitations

Do not disconnect an IDG in flight or hold the button longer than 30 seconds.

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Battery Voltage for Action

Requires recharging or replacing if at 24 volts or less.

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Generator Priority Order with APU

In priority: APU, external power, engines.

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Green Collared Circuit Breakers

Highlight manually resettable devices in the system.

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