Aircraft ECAM Advisory Mode Quiz
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Questions and Answers

What is the purpose of the EICAS display system?

  • To provide a wide variety of information relevant to engine operation and other automated systems.
  • To provide a maintenance mode for ground use only.
  • To categorize displays and alerts according to function and usage. (correct)
  • To display primary engine parameters such as N1 speed and EGT.

    • What is the purpose of the upper display unit on the EICAS?

  • To display the status of non-engine systems such as flight control surface position and hydraulic system.
  • To display primary engine parameters such as N1 speed, EGT, and warning and caution messages. (correct)
  • To display secondary parameters such as N2 speed, fuel flow, oil quantity, pressure, and temperature.
  • To display a row of Vs when secondary information is being displayed on the lower unit.

    • What is the purpose of the lower display unit on the EICAS?

  • To display primary engine parameters such as N1 speed and EGT.
  • To display secondary parameters such as N2 speed, fuel flow, oil quantity, pressure, and temperature. (correct)
  • To display warning and caution messages.
  • To display the status of non-engine systems such as flight control surface position and hydraulic system.

    • What is the purpose of the Operational mode in the EICAS display system?

    <p>To display the engine operating information and any alerts required to be actioned by the crew in flight.</p> Signup and view all the answers

    What is the purpose of the Status mode in the EICAS display system?

    <p>To display the status of non-engine systems such as flight control surface position and hydraulic system.</p> Signup and view all the answers

    What is the purpose of the Maintenance mode in the EICAS display system?

    <p>To display maintenance information for ground use only.</p> Signup and view all the answers

    What type of warning is associated with Level 3 failures?

    <p>Master Warning</p> Signup and view all the answers

    In the ECAM Failure Mode, what is the primary requirement for Level 3 failures?

    <p>Immediate corrective action</p> Signup and view all the answers

    What is the primary difference between Level 1 and Level 2 failures?

    <p>Action requirement</p> Signup and view all the answers

    Which type of failure corresponds to an abnormal aircraft configuration?

    <p>Level 2</p> Signup and view all the answers

    What is the distinguishing feature of a Level 3 failure compared to other levels?

    <p>Urgent corrective action requirement</p> Signup and view all the answers

    Which level of failure classification requires the flight crew to decide on whether an action should be taken?

    <p>Level 2 (Caution)</p> Signup and view all the answers

    What is the primary function of the Event Record Switch?

    <p>To enable manual recording of suspected malfunctions in non-volatile memory</p> Signup and view all the answers

    In what position does the Computer Select Switch automatically switch between the left and right computers?

    <p>In the 'AUTO' position</p> Signup and view all the answers

    Which of the following functions is controlled by the inner knob of the Display Brightness control?

    <p>Display intensity</p> Signup and view all the answers

    What is the purpose of the Thrust Reference Set Switch?

    <p>Both B and C</p> Signup and view all the answers

    What is the purpose of the Max Indicator Reset button?

    <p>To clear alerts from the display when measured parameters no longer exceed limits</p> Signup and view all the answers

    Which of the following systems can the Event Record Switch be used to activate the recording of fault data for?

    <p>Environmental Control system, Electrical Power system, Hydraulic system, and APU</p> Signup and view all the answers

    What is the primary purpose of the alert messages in the system?

    <p>To continuously monitor and detect malfunctions in various engine and airframe systems</p> Signup and view all the answers

    Which of the following best describes a Level A - Warning alert message?

    <p>Displayed in red, requires immediate corrective action, activates master warning lights and aural warnings</p> Signup and view all the answers

    How are Level B - Caution alert messages presented to the crew?

    <p>Displayed in amber, accompanied by an aural tone repeated twice</p> Signup and view all the answers

    What is the maximum number of alert messages that can be displayed simultaneously?

    <p>11</p> Signup and view all the answers

    Which statement best describes the purpose of the Maintenance Control Panel?

    <p>To allow maintenance engineers to access and display maintenance data stored in the system's computer memories</p> Signup and view all the answers

    What is the primary difference between Level B - Caution and Level C - Advisory alert messages?

    <p>Level B alerts are accompanied by aural tones, while Level C alerts have no aural tones or caution lights</p> Signup and view all the answers

    What is the primary function of the STS (System Test Switch) on the EICAS (Engine Indicating and Crew Alerting System) control panel?

    <p>To manually select an aircraft's status message when no warning is displayed</p> Signup and view all the answers

    What is the primary function of the RCL (Recall) switch on the EICAS control panel?

    <p>To recall previously cleared warning messages if the failure conditions still exist</p> Signup and view all the answers

    What happens when the CLR (Clear) switch is pressed on the EICAS control panel?

    <p>It suppresses status messages</p> Signup and view all the answers

    How many main components make up the basic EICAS system?

    <p>4</p> Signup and view all the answers

    What are the three types of information the EICAS system provides the flight crew?

    <p>Primary engine parameters, secondary engine parameters, and advisory/caution/warning alert messages</p> Signup and view all the answers

    Study Notes

    Display Units

    • Two display units provide a wide variety of information relevant to engine operation and other automated systems
    • Upper unit displays primary engine parameters:
      • N1 speed
      • EGT
      • Warning and caution messages
    • Lower unit displays secondary parameters:
      • N2 speed
      • Fuel flow
      • Oil quantity
      • Pressure
      • Temperature
    • Status of non-engine systems can also be displayed, including:
      • Flight control surface position
      • Hydraulic system
      • APU

    Display Modes

    • EICAS has three modes of displaying information:
      • Operational mode (selected by flight crew)
      • Status mode (selected by flight crew)
      • Maintenance mode (ground use only, selected via maintenance panel)

    Operational Mode

    • Displays engine operating information and alerts required to be actioned by the crew in flight
    • Normally only the upper display unit presents information

    Advisory Mode

    • Provides a summary of the aircraft's condition following a failure and possible downgrading of systems

    Failure Mode

    • Classifies failures into three levels:
      • Level 3: Warning (emergency configuration, requires immediate corrective action)
      • Level 2: Caution (abnormal configuration, requires crew awareness)
      • Level 1: Advisory (information on aircraft configuration requiring monitoring)

    Event Record Switch

    • Normally auto-records any malfunctions as they occur
    • Manual switch enables manual event marking for storage in non-volatile memory
    • Data can be retrieved and displayed by ground engineers via ground maintenance panel

    Computer Select Switch

    • In "AUTO" position, selects primary computer and automatically switches to secondary computer in case of failure
    • Manual selection of either computer is possible

    Display Brightness

    • Controlled by inner knob for display intensity and outer knob for display brightness

    Thrust Reference Set Switch

    • Allows selection of reference cursor on thrust indicator display (EPR or N1) for engines

    Alert Messages

    • System continually monitors over 400 inputs from engine and airframe systems
    • Up to 11 alert messages can be displayed on the upper display unit
    • Three levels of alert messages:
      • LEVEL A: Warning (red, immediate corrective action required)
      • LEVEL B: Caution (amber, immediate crew awareness required)
      • LEVEL C: Advisory (amber, crew awareness required)

    Maintenance Control Panel

    • Used by maintenance engineers to display maintenance data stored in system's computer memories
    • STS switch permits manual selection of status message if no warning is displayed
    • RCL switch enables recall of previously cleared warning messages

    Engine Indicating & Crew Alerting System

    • Basic system comprises two display units, a control panel, and two computers
    • Computers are designated "Left" and "Right" and only one is in control of the system at any one time
    • System provides flight crew with information on primary engine parameters, secondary engine parameters, and advisory/caution/warning alert messages as required

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    Description

    Test your knowledge of the ECAM Advisory Mode in aircraft systems. Learn about the different failure modes, classification levels, and crew actions in response to warnings and emergencies.

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