A320 Auto Flight System
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Questions and Answers

What is the primary function of the A320's Auto flight system?

  • To completely automate all flight operations without pilot interaction
  • To provide fully automatic managed operation with direct inputs from pilots (correct)
  • To assist pilots with navigation only
  • To monitor fuel consumption during the flight
  • Which components contribute to the position data inputs of the FMGS?

  • Flight Control Unit, FMGCs, and Autopilots
  • EFIS displays, MCDUs, and Thrust Levers
  • ADIRS, GPS, and Radio Navigation data (correct)
  • Flight Directors, GPS, and Auto thrust
  • When are inputs made to a MCDU in the context of the FMGS?

  • For short term operational changes
  • During lost communication scenarios
  • To adjust the landing gear configuration
  • When long term operations are desired (correct)
  • What characterizes 'selected' guidance in the FMGS?

    <p>It facilitates short term operational changes by direct inputs to the FCU</p> Signup and view all the answers

    Which part of the FMGS handles flight guidance?

    <p>Flight guidance</p> Signup and view all the answers

    What does the FMGS automatically tune for enhanced navigation?

    <p>Navigation radios</p> Signup and view all the answers

    How are the two FMGCs within the FMGS typically operated?

    <p>In synchronization to provide main computing support</p> Signup and view all the answers

    Which of the following statements is true regarding the functions of the FMGS?

    <p>It manages both flight guidance and augmentation processes</p> Signup and view all the answers

    What mode is engaged when the SPD/MACH selector knob is pulled out during Auto flight?

    <p>Selected Speed Mode</p> Signup and view all the answers

    Which statement is true regarding the managed mode of FMGS operation?

    <p>Dashes replace the selected value in the display.</p> Signup and view all the answers

    How does the Altitude selector knob modify the altitude settings?

    <p>The outer ring is typically set to 1000 feet increments.</p> Signup and view all the answers

    What occurs when the Altitude selector knob is pushed?

    <p>Activates the vertical profile compliance.</p> Signup and view all the answers

    During which situation would the METRIC ALT pushbutton be useful?

    <p>To change the target altitude to a metric reference.</p> Signup and view all the answers

    What does pressing the HDG-V/S/TRK-FPA pushbutton change?

    <p>From HDG-V/S to TRK-FPA mode.</p> Signup and view all the answers

    What visual indicators are displayed when the HDG/TRK knob is engaged in managed mode?

    <p>Dashes and a solid white dot.</p> Signup and view all the answers

    Which description accurately represents the function of the SPD/MACH selector knob?

    <p>It selects a target speed value for the AP or A/THR.</p> Signup and view all the answers

    What is the primary use of the EXPED pushbutton?

    <p>To expedite climb or descent to the selected altitude.</p> Signup and view all the answers

    What does pulling the V/S - FPA selector knob engage?

    <p>Selected mode for V/S or FPA operations.</p> Signup and view all the answers

    Which mode is indicated when the HDG/TRK knob is pulled?

    <p>Selected lateral mode.</p> Signup and view all the answers

    In what context does a solid white dot appear in the display?

    <p>When managed speed mode is activated.</p> Signup and view all the answers

    What happens during the automatic changeover from SPD to MACH?

    <p>Happens during climb.</p> Signup and view all the answers

    What does the Thrust Lever Angle (TLA) primarily determine?

    <p>The thrust limit of the engine</p> Signup and view all the answers

    What happens when the crew moves the thrust levers to the CL detent after takeoff?

    <p>The A/THR activates and remains armed.</p> Signup and view all the answers

    In which scenario will the A/THR remain engaged with one engine inoperative?

    <p>When thrust levers are positioned between idle and MCT detent.</p> Signup and view all the answers

    What is indicated by the display of MAN TOGA in the FMA Auto Thrust column?

    <p>Thrust is manually controlled at TOGA level.</p> Signup and view all the answers

    What occurs when the thrust levers are moved to IDLE during manual flight?

    <p>A/THR disconnects.</p> Signup and view all the answers

    What message displays when the A/THR is voluntarily disconnected?

    <p>A/THR OFF</p> Signup and view all the answers

    What activates the A/THR after it has been armed?

    <p>Pilot moving the thrust levers to the CL detent.</p> Signup and view all the answers

    What should a pilot do to re-engage the A/THR after a disconnect?

    <p>Move the thrust levers to the CLB detent and press the A/THR pushbutton.</p> Signup and view all the answers

    What occurs during the flare phase with A/THR in SPEED mode if the thrust levers are not moved to IDLE?

    <p>The A/THR will maintain target speed.</p> Signup and view all the answers

    When does the FMA A/THR indicate a transition from thrust mode to SPEED mode?

    <p>As the aircraft reaches the target altitude.</p> Signup and view all the answers

    What is the recommended method for disconnecting A/THR to prevent unexpected thrust variations?

    <p>Moving thrust levers to match current N1 and pressing the instinctive disconnect pushbutton.</p> Signup and view all the answers

    When A/THR is INACTIVE, what must the crew do for taxi and takeoff?

    <p>Manually set the required power.</p> Signup and view all the answers

    What happens immediately after an instinctive disconnect is performed?

    <p>A single aural warning occurs, Master Warning lights flash, and an AP OFF message appears.</p> Signup and view all the answers

    What type of disconnect occurs when the instinctive disconnects are used for Auto Thrust or AP?

    <p>Normal Disconnect</p> Signup and view all the answers

    What is displayed on the FMA when both autopilots and flight directors are turned off?

    <p>Only the active A/THR mode is visible.</p> Signup and view all the answers

    What occurs to the FMA modes when the FPV is displayed?

    <p>They change to reflect new targeting such as TRK.</p> Signup and view all the answers

    How should the flight directors be operated in normal conditions?

    <p>Both should be turned ON or OFF together.</p> Signup and view all the answers

    What guidance does the Yaw Bar provide during takeoff or landing?

    <p>Tracking localizer during low visibility.</p> Signup and view all the answers

    What happens to the command bars when a go-around is initiated in TRK/FPA mode?

    <p>They revert back to FD command bars.</p> Signup and view all the answers

    Which knob on the FCU is responsible for altitude adjustments?

    <p>ALTITUDE knob</p> Signup and view all the answers

    What does the FMA indicate when FD1 is selected to ON?

    <p>1FD- displayed on both PFDs.</p> Signup and view all the answers

    What is indicated if only one FD is selected ON during normal operations?

    <p>It is an abnormal condition.</p> Signup and view all the answers

    What function does pressing the HDG-V/S/TRK-FPA button serve?

    <p>Changes command bar symbol guidance.</p> Signup and view all the answers

    What occurs if a disconnect happens during a DUAL approach?

    <p>The approach capability changes to CAT 1.</p> Signup and view all the answers

    What does the vertical command bar provide during flight?

    <p>Lateral or roll guidance.</p> Signup and view all the answers

    What indicates the status of the AP when it is engaged?

    <p>The ENGAGE indicator lights up.</p> Signup and view all the answers

    What does the Flight Management part of the FMGS primarily provide for an aircraft?

    <p>Position determination and lateral navigation</p> Signup and view all the answers

    In dual autopilot operations, what determines which FMGC serves as the master?

    <p>The autopilot engaged for approach</p> Signup and view all the answers

    What function does the Flight Augmentation Computer provide regarding windshear?

    <p>Activates a windshear warning in the flight deck</p> Signup and view all the answers

    What is the primary role of the autopilot in the Flight Guidance part of FMGS?

    <p>To automatically provide guidance for pitch, roll, and yaw</p> Signup and view all the answers

    What happens when an autopilot is engaged during a dual mode CAT IIIB approach?

    <p>AP 1 is automatically the master</p> Signup and view all the answers

    Which input source is synchronized to both FMGCs for redundancy?

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

    What does the term 'Fail Operational' refer to in a CAT III DUAL system?

    <p>Failure below Alert Height still allows landing</p> Signup and view all the answers

    What indicates which autopilot is currently engaged during flight operations?

    <p>The Flight Mode Annunciator (FMA)</p> Signup and view all the answers

    How does the Flight Augmentation Part support flight control functions?

    <p>Through calculations of maneuvering speed and energy states</p> Signup and view all the answers

    What feature does the 'Instinctive Disconnect' button provide?

    <p>It allows pilots to regain manual control instantly</p> Signup and view all the answers

    What is the purpose of angle of attack protection in the FMGS?

    <p>To prevent stall conditions during maneuvers</p> Signup and view all the answers

    What is the minimum altitude above ground level (AGL) for engaging an autopilot after takeoff?

    <p>100' AGL</p> Signup and view all the answers

    Which of the following is NOT a function of the Flight Management part of the FMGS?

    <p>Providing thrust control for descent</p> Signup and view all the answers

    What does pressing the AP 1 or AP 2 pushbuttons accomplish?

    <p>Engages the selected autopilot.</p> Signup and view all the answers

    What color is displayed on the FMA for armed modes that are managed?

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

    Which columns on the FMA are synchronized to provide identical displays on both PFDs?

    <p>Vertical and Lateral Columns</p> Signup and view all the answers

    What is the effect of pressing the A/THR pushbutton?

    <p>Arms the Autothrust system.</p> Signup and view all the answers

    When are special messages displayed in the FMA?

    <p>In the third row of each column.</p> Signup and view all the answers

    What happens when the Altitude Selector Knob is pressed?

    <p>Engages selected altitude mode.</p> Signup and view all the answers

    Which mode causes the A/THR to maintain a specific target speed?

    <p>SPEED mode</p> Signup and view all the answers

    What does the white box surrounding an active FMA mode indicate?

    <p>A temporary alert for mode change.</p> Signup and view all the answers

    Which thrust detent is not available when A/THR is engaged?

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

    What color signals that the A/THR is armed but not active?

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

    What is the primary purpose of the Flight Mode Annunciator (FMA)?

    <p>To provide information on armed and active flight modes.</p> Signup and view all the answers

    In which condition do the vertical and lateral columns of the FMA combine?

    <p>During approach mode.</p> Signup and view all the answers

    How is the thrust value affected when A/THR is engaged?

    <p>Thrust values change based on FMGS inputs.</p> Signup and view all the answers

    What happens when the thrust levers are moved to the IDLE position with A/THR ON?

    <p>A/THR becomes unavailable.</p> Signup and view all the answers

    Study Notes

    A320 Auto Flight System

    • The A320 Auto flight system provides fully automatic flight management with pilot override capability
    • Automation increases safety, comfort, and reduces crew workload
    • The system utilizes two identical Flight Management Guidance Computers (FMGCs) that synchronize operations
    • Position data inputs include ADIRS, GPS, and Radio Navigation data, used to compute flight plan profiles
    • Flight deck controls include the Flight Control Unit (FCU), EFIS displays, FD Pb switches, thrust levers, and MCDUs
    • MCDU inputs are for long-term "managed" guidance, providing thrust, pitch, and lateral guidance according to the flight plan
    • FCU inputs are for short-term "selected" guidance, providing pilot direct inputs similar to conventional auto flight
    • FMGS signals operate Autopilots, Autothrust, Flight Directors, and EFIS displays, and automatically tunes navigation radios
    • FMGS comprises flight management, flight guidance, and flight augmentation
    • Flight Management determines aircraft position, navigates lateral flight plans, optimizes performance, and predicts waypoints, altitudes, and fuel requirements
    • Flight Guidance provides autopilot, autothrust, and flight director commands
    • Flight Augmentation (FAC) computes flight envelope limits (VLS, VMO, VFE, VA), windshear alerts, and angle of attack protection
    • FMGCs synchronize to maintain redundancy, with one typically acting as the master based on AP selection(s)

    Autopilot and Flight Director Engagement

    • Both Flight Directors (FDs) are typically on during flight, with an Autopilot (AP) selected after takeoff.
    • AP engagement requires an AGL of 100ft and 5 seconds of flight time
    • Only one AP can engage at any one time, except during dual autopilot Autoland approaches (CAT IIIB)
    • With CAT 3 approaches, both APs are armed in the APPR, then AP2 is selected
    • CAT 3 Dual is a fail-operational automatic landing system, which allows for an automatic approach and landing to CAT IIIB minimums.
    • A CAT 3 Single system is a fail-passive automatic landing system, where the pilot assumes control after a failure.
    • An "Instinctive Disconnect" pushbutton is available on each sidestick (also on THR LVRs) to take manual control if the Auto Thrust or Auto Pilot malfunctions.
    • Disengagement using the instinctive disconnect produces aural and visual alerts, but self-clears its alarms.
    • Other disconnections trigger ECAM actions that must be cleared, especially during a dual approach.
    • If the system disconnects during a dual approach, the approach capabilities are downgraded
    • FDs provide guidance displayed on PFDs using command bars, yaw bar for low visibility, or FPV with FPD
    • Selecting both FDs on or off is recommended.

    Flight Control Unit (FCU)

    • The FCU allows pilots to adjust short-term FMGS parameters.
    • Includes four knobs for speed, heading, altitude, and vertical modes
    • "Selected" modes allow pilots to input target values directly
    • "Managed" modes delegate target settings to the FMGS
    • SPD/MACH knob (selected vs managed): Rotation sets a target speed, while pushing sets a managed speed. Transitioning between SPD/MACH automatically happens during climb/descent.
    • HDG/TRK knob (selected vs managed): Rotation sets target heading/track; pushing engages managed mode.
    • ALT knob (selected vs managed): Rotation sets target altitude; pushing engages managed mode.
    • V/S/FPA knob (selected vs managed): Rotation sets target vertical speed/flight path angle; pushing engages managed mode to set V/S or FPA to zero.
    • FCU has 2 channels, either will activate.
    • Mode/target values are displayed in the window, as well as on the associated PFDs.

    Flight Mode Annunciator (FMA)

    • FMA displays both "managed" (long-term) and "selected" (short-term) FMGS modes
    • FMA displays modes for speed, heading, and altitude
    • Information includes Autothrust modes in the lefthand column, AP/FD vertical modes (middle column) and approach and lateral capabilities
    • FMA status of each are displayed in the righthand column
    • The FMA synchronizes the 4th and 5th columns on both PFDs
    • Mode change alerts utilize a brief white box indicator
    • Specific messages are displayed using different colors and durations (examples: "MAN PITCH TRIM ONLY", "CHECK APP SEL")

    Auto-Thrust System (A/THR)

    • A/THR handles thrust operations after takeoff (when A/THR is not engaged, the captain/first officer inputs the thrust).
    • A/THR is not available during TOGA or FLX thrust
    • A/THR utilizes Thrust Levers from idle up to climb power
    • Power is determined by thrust lever position
    • A/THR operating options include speed or thrust level adjustments according to AP/FD vertical modes and input through the Thrust Levers
    • A/THR control involves the Auto-Thrust pushbutton and thrust levers
    • On the ground, A/THR is disengaged, requiring manual thrust settings for taxi and takeoff
    • A/THR can be disconnected when manually adjusting the thrust levers
    • The correct method to disconnect the A/THR is to first match your thrust lever position based on the N1 digital reading and then press the Instinctive Disconnect button
    • Press the A/THR pushbutton to re-engage the A/THR after a disconnect.

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    Description

    Test your knowledge on the A320 Auto Flight System, which combines safety and automation to enhance pilot operations. This quiz covers the functionalities of the Flight Management Guidance Computers (FMGCs), flight deck controls, and the integration of various navigation data. Prepare to explore the intricacies of flight management, guidance, and augmentation systems.

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