A320 Review Flashcards: Safety & Equipment
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Questions and Answers

The potable water system is pressurized by?

  • The pneumatic system (correct)
  • The hydraulic system
  • The PTU
  • Ambient air pressure
  • FASTEN SEAT BELT and RETURN TO YOUR SEAT signs illuminate when cabin altitude exceeds ________ feet?

  • 14,000
  • 10,000
  • 11,300 (correct)
  • 13,500
  • NO SMOKING and EXIT signs illuminate when cabin altitude exceeds ________ feet?

  • 14,000
  • 13,500
  • 10,000
  • 11,300 (correct)
  • In the AUTO position, the NO SMOKING switch causes the?

    <p>NO SMOKING and EXIT signs to illuminate when landing gear is extended, and extinguish when landing gear is retracted.</p> Signup and view all the answers

    If normal electrical power is lost, the following lights remain available?

    <p>Captain's instrument panel (powered CRTs and flood lighting)</p> Signup and view all the answers

    What is the normal in-flight position of the red tab N/100% PUSH Switch on the oxygen mask?

    <p>100%.</p> Signup and view all the answers

    If the Emergency Access code is entered on the Flight Deck Access Panel and no cockpit action is taken, when will the cockpit door automatically unlock?

    <p>30 seconds.</p> Signup and view all the answers

    Galleys are powered by?

    <p>Both Main AC Busses.</p> Signup and view all the answers

    Cargo door operation is normally powered by the?

    <p>Yellow electric hydraulic pump.</p> Signup and view all the answers

    The aircraft passenger WIFI system can be powered OFF by?

    <p>GALLEY or GALLEY &amp; CAB switch.</p> Signup and view all the answers

    Air for the pneumatic system is normally bled from the ____ of the compressor?

    <p>Intermediate pressure stage</p> Signup and view all the answers

    What happens in flight if pneumatic bleed air pressure is insufficient even with the HP stage valve open?

    <p>Engines spool up automatically.</p> Signup and view all the answers

    What valve action automatically occurs when the APU supplies air to the pneumatic system?

    <p>Crossbleed valve opens and the engine bleed valves close.</p> Signup and view all the answers

    Pneumatic system operation is controlled and monitored by?

    <p>Two Bleed Monitoring Computers (BMCs).</p> Signup and view all the answers

    If BMC 1 fails, what leak detection is lost?

    <p>Engine 1 &amp; APU.</p> Signup and view all the answers

    If BMC 2 fails, what leak detection is lost?

    <p>Engine 2.</p> Signup and view all the answers

    A blue item on the takeoff memo indicates a checklist item that is _____?

    <p>faulted</p> Signup and view all the answers

    Study Notes

    Potable Water System

    • The potable water system is pressurized by the pneumatic system.

    Cabin Altitude Alerts

    • FASTEN SEAT BELT and RETURN TO YOUR SEAT signs illuminate when cabin altitude exceeds 11,300 feet.
    • NO SMOKING and EXIT signs illuminate under the same cabin altitude condition of 11,300 feet.

    NO SMOKING Switch Functionality

    • In AUTO position, the NO SMOKING switch illuminates NO SMOKING and EXIT signs when landing gear is extended and turns them off when landing gear is retracted.

    Power Loss Indicators

    • If normal electrical power is lost, Captain's instrument panel (powered CRTs and flood lighting) remains available.

    Oxygen Mask Operation

    • The red tab N/100% PUSH Switch on the oxygen mask should normally be at the 100% position.

    Cockpit Door Access

    • Entering the Emergency Access code on the Flight Deck Access Panel will result in the cockpit door automatically unlocking after 30 seconds if no further action is taken.

    Galley Power Supply

    • Galleys are powered by both Main AC Busses.

    Cargo Door Operation

    • Cargo door operation is normally powered by a yellow electric hydraulic pump.

    Passenger WIFI System

    • The aircraft passenger WIFI system can be powered OFF using the GALLEY or GALLEY & CAB switch.

    Pneumatic System Air Supply

    • Air for the pneumatic system is typically bled from the intermediate pressure stage of the compressor.

    Pneumatic Pressure Management

    • If pneumatic bleed air pressure is insufficient despite HP stage valve being open, engines will spool up automatically.

    APU Air Supply Effects

    • When the APU supplies air to the pneumatic system, the crossbleed valve opens while engine bleed valves close.

    Pneumatic System Control

    • The operation of the pneumatic system is controlled and monitored by two Bleed Monitoring Computers (BMCs).

    Leak Detection Failures

    • If BMC 1 fails, leak detection for Engine 1 and APU is lost.
    • If BMC 2 fails, leak detection for Engine 2 is lost.

    Takeoff Memo Indicators

    • A blue item on the takeoff memo signifies a checklist item that requires accomplishment.

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    Description

    Test your knowledge of the Airbus A320's emergency equipment and systems with these flashcards. Each question covers essential safety protocols and operational functionalities of the aircraft. Perfect for students or aviation enthusiasts looking to deepen their understanding of A320 operations.

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