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Garmin 530w Manual

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    Setup 2 Page
    Nearest Airport  Criteria
    To set the minimum runway length and runway 
    surface: 
    1.  Select “Nearest Airport Criteria” from the Setup 
    Page. 
    2.   The flashing cursor highlights the “Runway 
    Surface” field. Turn the small right knob 
    to select the desired surface. The following 
    options are available: 
    • Any surface
    • Hard surfaces Only
    • Hard / Soft surfaces
    • Water landings only
    3. Press  ENT to accept the runway surface selec-
    tion. 
    4.   The flashing cursor moves to the minimum 
    runway length field. To enter a different mini-
    mum runway length, use the small and large 
    right  knobs to enter the desired length. Press 
    ENT when finished. 
      A runway length of “0”(or a very short length) 
    will report all available runways. 
     NOTE: Exercise caution when changing the Near-
    est Airport Criteria. Remember, by excluding certain 
    surface types or shorter runway lengths, you may be excluding airports from the nearest list that are more than adequate for an emergency landing! 
    Data Field Configuration
    To change the configuration of the data field 
    below the VLOC window: 
    1.   Select “Data Field Configuration” from the 
    Setup Page. 
    2.   Turn the small right knob to select the desired 
    data field option. The following options are 
    available: 
    • VOR/LOC Data — displays the identifier, 
    distance and radial FROM the tuned VOR sta
    -
    tion active in the VLOC window. When tuned 
    to a nearby localizer, the localizer identifier, 
    associated airport and runway are displayed 
    instead. 
    • Configurable Data Fields — displays a user- selectable data field of navigation data (e.g., 
    ground speed, track, distance to destination, etc.) 
    • Traffic Watch — if your 500W-series unit is connected to other equipment providing traf
    -
    fic alert information (e.g., L3 SKYWATCH™ 
    or RYAN TCAD), a window is provided to 
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    display traffic information. This allows you 
    to monitor traffic conditions from ANY page 
    and quickly identify traffic hazards. See the 
    400W/500W Series Display Interfaces Pilot's 
    Guide Addendum for more information on 
    traffic data. 
    3. Press  ENT to accept the selection. 
    4.   If “Configurable Data Fields” is selected, a 
    second selection field appears to allow you 
    to select the desired data type. Turn the large 
    right  knob to highlight this second field, then 
    turn the small right knob to display a list 
    of available navigation data types. Continue 
    turning the small right knob to select the 
    desired data type and press ENT to approve 
    your selection. 
    COM Configuration
    To set the COM channel spacing:  
    1.  Select “COM Configuration” from the Setup 1 
    Page. 
    2.   The flashing cursor highlights the channel spac-
    ing field. Turn the small right  knob to select 
    the desired channel spacing: 8.33 kHz or 25.0 
    kHz. Press ENT when finished. 
    8.33 kHz and 25.0 kHz channel spacing are  available for the GNS 530W’s COM trans-
    ceiver. Use the 25.0 kHz setting in the United  States. 
    Preset Com Frequencies
    On units configured for COM Frequency Presets 
    you may store up to 15 preset Com frequencies in the 
    Com Configuration page. On units configured with a 
    remote Com frequency recall switch, these preset fre
    -
    quencies can be loaded into the STBY frequency with 
    the press of a button. 
     NOTE: Preset Com Frequencies are only available with  Main System Software Version 3.00, or later. 
    To store a  preset Com frequency: 
     1.   Select “COM Configuration” from the Setup 1 
    Page. 
    2.   The flashing cursor will highlight the Channel 
    Spacing field. Turn the large right knob to 
    highlight the left (non-decimal) part of the first 
    frequency field. 
    Setup 2 Page
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    3.   Turn the small right knob to select the desired 
    frequency. 
    4.    Turn the large right knob to highlight the right 
    (decimal) part of the frequency field. 
    5.   Turn the small right knob to select the desired 
    frequency. 
    6.    Repeat for the desired frequencies. Press the 
    small right knob to finish. 
    When the remote Com frequency recall switch is 
    pressed, the next preset frequency will be moved into 
    the Com Standby frequency box and a small window 
    with the current Com Frequency Preset number will 
    appear next to it. You can scroll down through the 
    preset frequencies by repeatedly pressing the remote 
    Com Frequency recall switch. Empty Preset slots are 
    skipped. 
    Restoring Factory Settings
    When making changes to any Setup 1 Page item, 
    a “Restore Defaults?” menu selection allows you to 
    restore the original factory settings (for the selected 
    option only). For example, with the CDI / Alarms Page 
    displayed, the “Restore Defaults?” option restores the 
    arrival alarm, all airspace alarms and CDI settings to 
    the original factory values. 
    To restore a Setup 1 Page item to the original fac-
    tory settings: 
    1.   Select the desired item from the Setup 1 Page. 
    2.  Press  MENU to display a page options window. 
    3.   With “Restore Defaults?” highlighted, press 
    ENT. 
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    Setup 2 Page
    SBAS Selection
    To enable WAAS operation, in the Setup 2 page 
    select the SBAS (Space-Based Augmentation System) 
    item and then select WAAS. If WAAS is disabled, the 
    unit will not be able to fly WAAS approaches (LP, LPV, 
    LP +V, LNAV/VNAV, or LNAV+V). 
    If WAAS was previously disabled, it may take sev
    -
    eral minutes to achieve a 3D-Diff fix after re-enabling 
    WAAS. 
    1.  Select “SBAS Selection” from the Setup 2 Page 
    and press ENT. 
    To enable WAAS operation, select the “SBAS 
    Selection” menu option. 
    2.  The flashing cursor highlights the WAAS status 
    selection. Turn  the  small right knob to allow 
    On/Off selection. 
    To enable WAAS operation, select the “SBAS  Selection” menu option. 
    3.  Turn  the  small right knob to select “On” or 
    “Off” and then press ENT. Press the Cursor 
    knob to exit WAAS selection. 
     NOTE:  There may be other SBAS selections avail-
    able, such as MSAS. 
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    Section 10   
    Vertical Navigation (VNAV)
    The 500W-series Vertical Navigation Page allows 
    you to create a three-dimensional profile which guides 
    you from your present position and altitude to a final 
    (target) altitude at a specified location. This is helpful 
    when you’d like to descend to a certain altitude near 
    an airport. Once the profile is defined, message alerts 
    and additional data on the Default NAV and Map 
    Pages keep you informed of your progress. 
    To display the Vertical Navigation Page, press the 
    VNAV key. 
    VNAV is inhibited in the following conditions: 
    •  Groundspeed is less than 35 knots
    •  No active flight plan or direct-to destination
    •  SUSP mode
    •  Vectors-to-Final mode
    •  VLOC mode
    •  After the FAF on an approach
     WARNING: VNAV is to be used for advisory 
    purposes only.  VNAV messages or vertical speed required should not be used to maintain terrain or ATC clearances.  Terrain and ATC clearances are the sole responsibility of the pilot. 
    Vertical Navigation Page
    Target Altitude
    Vertical Speed Desired Altitude Reference  (AGL or MSL)
     Vertical Speed Required
    Target Distance 
    (from reference) Target Reference
    A message alert lets you know when to 
    begin a VNAV descent... 
    ...as well as when you’re approaching your  new target altitude. 
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    To create a vertical navigation profile: 
    1. Press  VNAV to display the Vertical Navigation 
    Page. 
    2.   Press the small right knob to activate the 
    cursor. 
    3.   With the “Target Altitude” field highlighted, 
    turn the small and large right knobs to select 
    the target altitude and press ENT. 
    Turn the small and large right knobs to select 
    a target altitude. The target altitude can be 
    above field elevation (for an airport) or you 
    can specify an MSL altitude for any waypoint  category. 
    4.  Turn the small right knob to select “Above 
    Wpt” (AGL) or “MSL”, and press ENT. “Above 
    Wpt” uses the altitude of a destination airport 
    as stored on the Jeppesen NavData card. 
    “MSL” lets you set a specific target altitude 
    for any waypoint category: airport, VOR, NDB, 
    intersection or user waypoint. 
    5.   Turn the small  and large right knobs to select 
    a distance from the target reference waypoint 
    and press ENT. If the target altitude should 
    occur at the target reference waypoint, enter 
    a distance of zero. 
    6.   Turn the small right knob to select “Before” 
    or “After”, and press ENT. This setting desig-
    nates whether the offset distance defines a 
    point before you reach the target reference 
    waypoint or after you reach the waypoint. The 
    “After” selection is not available for the last 
    waypoint. 
    Turn the small right knob to select whether 
    the distance is “Before” or “After” the refer -
    ence waypoint. 
    7.   When using a flight plan, the target refer -
    ence waypoint itself can be specified from 
    the waypoints contained in the flight plan. By 
    default, the last waypoint in the flight plan is 
    selected. To select a different waypoint, turn 
    the  small right knob to select the desired 
    waypoint and press ENT. 
    Vertical Navigation Profile
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    8.  The default profile utilizes a 400 foot-per-
    minute descent rate. To change the rate, turn 
    the  large right knob to highlight the “VS 
    Profile” field and use the small and large 
    right  knobs to enter a new rate. Press ENT 
    when finished. 
    The default profile is a 400 foot-per-minute 
    descent. Use the small and large right knobs  to enter a different vertical speed figure.  
    With the profile set, the vertical speed required 
    (VSR) is displayed on the Vertical Navigation Page. 
    Expect the following to occur when using the vertical 
    navigation feature:  •  At one minute prior to reaching the initial 
    descent point, a message “Approaching VNAV 
    Profile” occurs. The descent angle also locks 
    to prevent changes in speed from altering the 
    profile. 
    •   If selected, the vertical speed required (VSR) 
    readout on the default NAV and map pages 
    shows the desired vertical speed to maintain the 
    proper descent angle. Maximum VSR that can 
    be displayed is -6000 ft/min.  If VSR exceeds 
    -6000 ft/min, dashes will be displayed. 
    •  Course reversals are not included in the VNAV 
    calculations until the aircraft begins the course 
    reversal. While reversing course, VNAV includes 
    direct-to the course reversal wayopint in the  VNAV calculation. 
    •   At 500 feet above the target altitude, an 
    “Approaching Target Altitude” message is pro
    -
    vided. The VSR readout on the Default NAV and 
    Map Pages is blanked out, at this point. 
    Vertical navigation messages can be turned on or 
    off. (By default the messages are off.) Turning the mes
    -
    sages off allows you to keep the profile settings you’ve 
    entered previously, without having them generate mes
    -
    sages when the feature isn’t needed. 
    To disable/enable the vertical navigation (VNAV) 
    messages: 
    1.  Press  MENU to display the Vertical Navigation 
    Page Options menu. 
    2.   With “VNAV Messages On?” highlighted, press 
    ENT.  Or, if the messages are already on and 
    you wish to turn them off, make sure “VNAV 
    Messages Off?” is highlighted and press 
    ENT. 
    Select “VNAV Messages On?” to display the 
    vertical navigation alert message. 
    To restore the factory default VNAV settings: 
    1. Press  MENU to display the Vertical Navigation 
    Page Options menu. 
    2.   Turn the large right knob to highlight 
    “Restore Defaults?” and press ENT.  
    VNAV Messages
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    Section 11   
    Fault Detection and Exclusion (FDE) 
    Interface
    Fault Detection and Exclusion (FDE)
    The Garmin 500W-series software incorporates 
    a Fault Detection and Exclusion (FDE) algorithm, 
    thus providing a basis for approval per FAA Notice 
    N8110.60 requirements for “GPS as a Primary Means 
    of Navigation for Oceanic/Remote Operations”. 
    The FDE consists of two distinct features, fault 
    detection and fault exclusion. The fault detection 
    feature detects the presence of an unacceptably large 
    pseudorange error for a satellite (and presumably, 
    position error) for a given mode of flight. Upon detec
    -
    tion, fault exclusion follows and excludes the source 
    of the unacceptably large pseudorange error , thereby 
    allowing navigation to return to normal performance 
    without an interruption in service. To enhance safety, 
    FDE functionality is provided for other phases of flight 
    (non-precision approach, terminal, en route). The FDE 
    functionality for non-oceanic flight phases complies 
    with missed alert probability, false alert probability and 
    failed exclusion probability specified by DO-229C / 
    TSO-C146a. 
    Pre-departure Verification of FDE
    An FDE prediction must be performed prior to 
    departure for a flight plan involving Oceanic/Remote 
    operation where GPS is to be the sole source of 
    navigation. Prior to departure, the operator must 
    use the FDE prediction program supplied with the 
    400W/500W-series Trainer CD to demonstrate that 
    there are no outages in the capability to navigate 
    on the specified route of flight (the FDE prediction 
    program determines whether the GPS constellation is 
    robust enough to provide a navigation solution for the 
    specified route of flight). Please, refer to the instruc
    -
    tions included in the Garmin 400W/500W-series 
    Training CD for complete details on using the FDE 
    prediction program. 
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    Section 12   
    Messages, Abbreviations,  
    & Nav Terms
    Messages
    The 500W-series unit uses a flashing “MSG” annun-
    ciator at the bottom of the screen (directly above the MSG 
    key) to alert you of any important information or warnings. 
    While most messages are advisory in nature, warning mes
    -
    sages may require your intervention. Whenever the “MSG” 
    annunciator flashes, press the MSG key to display the 
    message, when pilot workload allows. Press MSG again to 
    return to the previous page. 
    The following is a list of available messages and their mean
    -
    ings: 
    ABORT APPROACH — Loss of Navigation — Execute 
    missed approach using other navigation equipment. 
    ADS-B traffic has failed — The ADS-B traffic system may 
    have lost GPS position or detected an internal fault. Contact 
    dealer for service. 
    ADS-B transmit has failed — ADS-B unit is not able to 
    transmit a message due to a failure with the ADS-B system 
    or antenna(s). Contact dealer for service. 
    ADS-B is not transmitting position — The ADS-B unit 
    has detected a position input falut. Contact dealer for 
    service. 
    ADS-B fault -  Check ADS-B Status Page — A fault has 
    been detected. Check the ADS-B unit Status page in Aux 
    mode.  
    ADS-B - Connection has been lost — The GNS is config
    -
    ured for a traffic device but is not receiving data from it. 
    Traffic will not be displayed on the GNS. Contact dealer for 
    service. 
    ADS-B Traffic Alerting not available — The ADS-B traf
    -
    fic system is reporting that the CSA application has failed. 
    Traffic alerting on ADS-B traffic is unavailable. Ensure the 
    aircraft has a clear view of the sky. If the problem persists. 
    Contact dealer for service.  Airport terrain database integrity error — The 
    500W-series unit has detected a problem with a database 
    on the TAWS/Terrain data card. The data is not usable and 
    the card should be returned to your Garmin dealer.
    Airspace ahead — less than 10 minutes — Your GPS-calcu-
    lated course is projected to enter a special use airspace within 
    10 minutes. This message is automatically disabled within 30 
    NM of an arrival airport, when an approach is loaded. 
    Airspace near and ahead — Your GPS-calculated 
    position is within 2 NM of the boundary of a special use 
    airspace and your course is projected to enter the airspace. 
    This message is automatically disabled within 30 NM of an 
    arrival airport, when an approach is loaded. 
    All data referenced to True North — The unit does not 
    have a valid aviation database, so it cannot compute mag
    -
    netic variation. 
    Approach downgraded — Use LNAV minima — This 
    message will occur 60 seconds prior to the FAF if flying 
    LNAV+V, L/VNAV, LP, or LPV approaches and WAAS 
    integrity parameters have fallen below minimal limits. As a 
    result, vertical guidance has been discontinued and the LP, 
    LPV, LP +V, LNAV+V, or L/VNAV approach you were flying 
    has been downgraded. 
    Approach is not active — The approach could not transi
    -
    tion to “active”, at 2 NM or closer to the FAF. Verify that 
    “SUSP” DOES NOT appear directly above the OBS key, 
    indicating the auto waypoint sequencing is suspended. 
    This message also appears if Receiver Autonomous Integrity 
    Monitoring (RAIM) has determined that sufficient GPS 
    satellite coverage DOES NOT exist for the phase of flight 
    you are currently in (along with a “RAIM not available from 
    FAF to MAP” message). 
    Approaching target altitude — The current GPS-com
    -
    puted altitude is within 500 feet of the final Vertical Naviga-
    tion target altitude. 
    Approaching VNAV profile — You are within one minute 
    of reaching the initial Vertical Navigation descent point. 
    12 - MESSAGES
    ABBREVIATIONS &  NAV TERMS 
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    APR Guidance Available - Use PROC before A/P APR 
    — For units configured with the KAP140 or KFC225 auto-
    pilot, this message reminds pilots, when they turn on course 
    to the FAF, that they need to enable autopilot outputs (by 
    pressing PROC and selecting “Enable A/P APR Outputs?”) 
    before switching the autopilot control panel to APR. 
    Arrival at waypoint [waypoint name] — You are within 
    the arrival alarm circle for the indicated waypoint. The size 
    of the arrival alarm circle is defined from the “CDI / alarms” 
    menu option on the Setup Page. 
    Audio database integrity error — The 500W-series unit 
    has detected a problem with the built-in TAWS Audio Data
    -
    base. TAWS audio alerts are not available. The unit should 
    be returned to your Garmin dealer for service. 
    Aviation database integrity error — The 500W-series 
    unit has detected a problem with a database on the Nav
    -
    Data® card. The data is not usable and the card should be 
    returned to Jeppesen or your Garmin dealer for service. 
    Bad geometry, parallel offset not activated — parallel 
    offset is not activated because of flight plan geometry. 
    Basemap database integrity error — The 500W-series 
    unit has detected a failure in the built-in basemap (land 
    data) database. Land data does not appear on the Map Page. 
    Other unit functions continue to work normally, however 
    the 500W-series unit should be taken to your Garmin 
    dealer for service at your earliest convenience. 
    Boot block verify failed - Return unit for repair — 
    System integrity testing has determined that the boot block 
    has become corrupted. Return the unit to your Garmin 
    dealer for service. 
    Cannot navigate locked FPL — You have attempted 
    to navigate a flight plan (FPL) with one or more locked 
    waypoints. A waypoint can be “locked” when the NavData
    ® 
    card is replaced and the waypoint(s) does not exist in the 
    new database or if attempting to crossfill user waypoints 
    when no empty user-defined waypoint slots exist (will 
    create a “lockd” point in flight plan).  Can’t change an active waypoint — An attempt has 
    been made to modify the position of the active “to” or 
    “from” waypoint. The 500W-series unit does not allow 
    modifications to user waypoints currently being utilized for 
    navigation guidance. 
    Can’t delete an active or FPL waypoint — An attempt 
    has been made to delete the active “to” or “from” user 
    waypoint. The 500W-series unit does not allow you to 
    delete user waypoints currently being utilized for naviga
    -
    tion guidance. 
    CDI key stuck — The CDI key is stuck in the enabled (or 
    “pressed”) state. Try pressing the CDI key again to cycle its 
    operation. Check for proper operation of both the internal 
    and remote keys (if present). If the message persists, contact 
    your Garmin dealer for assistance. 
    CDI key disabled — The installation has disabled the 
    CDI key so that systems (such as an EFIS) connected to the 
    500W series unit will always have GPS deviation data on 
    one output (main) and VLOC deviation data on the other 
    output (Nav). See your installer for more information. 
    Check unit cooling — The 500W-series unit has detected 
    excessive display backlighting temperature. The back
    -
    lighting has been automatically dimmed to reduce the tem-
    perature. Check for adequate ventilation or check cooling 
    airflow. Contact your Garmin dealer for assistance. 
    COM has failed — (GNS 530W only) The unit has 
    detected a failure in its communications transceiver. The 
    COM transceiver is not available and the unit should be 
    returned to your Garmin dealer for service. 
    COM is not responding — (GNS 530W only) 
    Internal 
    system-to-system communication between the main proces
    -
    sor and the COM transceiver has failed. Operational status 
    of the COM transceiver is unknown and the unit should be 
    returned to your Garmin dealer for service. 
    If the Com board is still working, it will automatically 
    tune to 121.500 MHz. Transmit and receive functions 
    may still operate regardless of the displayed frequency. 
    12 - MESSAGES
    ABBREVIATIONS &  NAV TERMS 
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