Garmin 530w Manual
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191 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 9 - AUX PAGES 190-00357-00 Rev K
192 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 9 - AUX PAGES 190-00357-00 Rev K
193 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. 9 - AUX PAGES 190-00357-00 Rev K
194 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. 9 - AUX PAGES 190-00357-00 Rev K
195 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. 10 - VNAV 190-00357-00 Rev K
196 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 10 - VNAV 190-00357-00 Rev K
197 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 10 - VNAV 190-00357-00 Rev K
198 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. 11 - FDE 190-00357-00 Rev K
199 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 190-00357-00 Rev K
200 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 190-00357-00 Rev K