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General| Resolution | 1280 x 800 pixels |
|---|---|
| Touchscreen | Yes |
| Power Supply | 10-30 V DC |
| Display Type | LCD |
| AHRS | Integrated |
| Autopilot Compatibility | Yes |
| Operating Temperature | -20°C to +55°C |
| Synthetic Vision | Yes |
| Traffic Display | Yes |
| Terrain Awareness | Yes |
| Interfaces | Ethernet, USB |
| Engine Monitoring | Yes, with optional modules |
| ADS-B | Supported |
| Weather Display | Yes |
| GPS | Built-in |
Register your Dynon Avionics SkyView HDX system online to ensure up-to-date contact information and expedite warranty claims.
Recommendations for printing the manual sections as needed for your build, suggesting office supply retailers for best quality.
Discusses STC AML applicability, substantiating installation, and FAA form 337 requirements.
Responsibility of the mechanic to record component installation locations in the airplane's permanent record.
Lists the essential equipment required for the SkyView HDX System STC SA02594SE installation.
Lists optional equipment that may be installed, with a note to check SA02594SE_AML for aircraft-specific options.
Examples of Dynon-provided equipment typically mounted to the instrument panel, serving as an installation example.
Explains what a SkyView system is and how to build one, with high-level diagrams of typical system overview.
Details the SkyView Network, its connectors, and how it communicates between displays and modules.
Lists external switches and indicators that may be installed, referring to Appendix I for details.
Describes the high-resolution, non-reflective screens of SkyView displays and their resolutions.
Specifies the system's capability to include up to three SkyView displays in any combination.
Provides power specifications for SkyView displays and devices, including current requirements and circuit protection recommendations.
Details Dynon Avionics SkyView harnesses and network cables, including SV-NET-SERVO, SV-NET-SPL, and SV-NET-HUB.
Explains the importance of connecting Ethernet ports for database transfer and future functionality.
Lists Dynon Avionics part numbers and descriptions for components used to build a SkyView system.
Provides information for benchtop testing or immediate post-installation checkout of the SkyView system.
Discusses CFR Part 23 regulations for information display and recommends IA agreement on installation methods.
Details structural integrity requirements, edge margins, and sheet metal thickness guidance for replacement panels.
Defines FAA's Primary Flight Information (PFI) and its display area on SkyView HDX as Primary Flight Display (PFD).
Explains quantitative requirements for information display based on AC 23.1311-1C Section 15.0 Pilot Field-of-View Considerations.
Describes the normal line-of-sight visual fields from the design eye reference point, accommodating eye movement only.
Defines the vertical and horizontal visual fields from the design eye reference point, accommodating eye movement and minimal head movement.
Discusses factors like readability, clutter, pilot workload, and attention-getting for assessing displayed information acceptability.
Provides volumetric space requirements for displays and control panels, including space for electrical connectors and harnesses.
Details the installation of optional avionics trays for mounting SkyView HDX displays and components, including panel cut-out dimensions.
Provides mechanical dimensions and guidance for mounting SkyView displays, including panel cut-outs and mounting hole details.
Covers primary power input, grounding, master contactor considerations, and SV-BAT-320 connection rules.
Explains the two D9 connectors on the display back are SkyView network connectors, not RS-232.
Guides on connecting modules in a network, powering on displays, and performing network configuration.
Explains the importance of connecting Ethernet ports for database transfer and future functionality.
Explains how Zulu/GMT time is obtained and retained using GPS or SV-BAT-320.
Provides advice on connecting non-Dynon Avionics devices via RS-232 serial ports, including specific instructions for common devices.
Details how to configure SkyView serial ports, including input device, function, baud rate, and output device.
Explains how to characterize the display's backlight behavior manually, automatically, or via external control.
Details recording important aircraft information, including tail number, essential for network configuration and operation.
Describes how to perform display/screen setup and layout as an operational function via the Main Menu.
Covers touch interface specific settings like SHOW TOUCHES and diagnostic options.
Explains how to display a Glide Ring and the settings required for accurate display.
Details how SkyView HDX assists in computing Weight and Balance, requiring definition of CG limits and stations.
Explains how SkyView HDX provides up to 10 maintenance reminders based on date, elapsed time, or text.
Details how to configure the SV-KNOB-PANEL into the SkyView Network using the setup menu.
Describes verification steps for knobs and dim commands after installing the SV-KNOB-PANEL.
Provides guidelines for choosing a location for the SV-BAT-320, emphasizing proximity to the display and avoiding vibration/humidity.
Details connecting the SV-BAT-320 module's connector to the SV-HARNESS-D37 mating connector for proper function.
Explains the automatic charging process in flight and conditions for charging on the ground or during aircraft construction.
Describes the battery status icon displayed on the top bar, including 'No Battery Icon', 'Needs Test Icon', and 'Fault/Test Failed Icon'.
Guides on checking battery status, including connected state, last shutdown, test results, and charge status.
Details the procedure to ensure the SV-BAT-320 is fully functional after installation, by testing its capacity.
Provides instructions for contacting Dynon Avionics Technical Support if the SV-BAT-320 fails the initial test.
References Appendix B for detailed specifications of the SV-BAT-320.
Provides guidance on returning the battery for warranty replacement, including shipping regulations for Lithium-Ion batteries.
Specifies the location requirements for the SV-ADAHRS-200 module within 12 feet longitudinally and 6 feet laterally of the aircraft's center-of-gravity.
Details mounting orientation: parallel to aircraft axes, pneumatic fittings facing front, mounting tabs towards bottom, label towards top.
Describes which sensors and inputs are used to generate displayed instruments, including GPS, Pitot, Static, AOA, etc.
Guides on connecting the SV-ADAHRS-200 to the SkyView network using specified hardware and D9 connectors.
Explains the necessity of in-aircraft compass calibration after build completion to ensure accurate magnetic heading.
Details the step-by-step process for performing an on-ground compass calibration, including aircraft positioning and data collection.
Describes the procedure for in-flight compass calibration, emphasizing VFR day conditions and maneuvers for improved accuracy.
Covers configuration of PFD-related ADAHRS settings, including Aircraft Icon, Measurement Units, Airspeed Limitations, and Vertical Speed Scale.
Details additional calibrations like Altitude Offset and Zero Pressure IAS/AoA Calibration.
Emphasizes installing the SV-MAG-236 in a magnetically benign area to ensure accurate magnetic heading sensing.
Explains the option to connect the SV-OAT-340 to the SV-MAG-236 if it is more accessible.
Guides on connecting the SV-MAG-236 to the SkyView network using a SkyView Network Cable and proper connector placement.
Discusses the need for in-aircraft compass calibration after build completion, displaying a 'NEED COMPASS CAL' message until performed.
Details the steps for on-ground compass calibration, including positioning the aircraft and collecting data at cardinal directions.
Provides guidelines for installing the SV-OAT-340 sensor to ensure accurate air temperature measurement, avoiding heat sources.
Guides on routing and securing sensor wires and connecting the sensor to the SV-ADAHRS-200 or SV-MAG-320.
Provides guidelines for choosing a location for the SV-EMS-220 Engine Monitor module, typically on the avionics tray behind the display.
Details connecting the EMS module to the SkyView network and wiring systems/sensors according to diagrams.
Explains the use of a file to define sensor behavior and map sensors to SV-EMS-220 pins for onscreen representation.
Lists the premade wire harnesses offered by Dynon Avionics for connecting sensors and transducers to the SV-EMS-220.
Details the 5V and 12V power outputs provided by the SV-EMS-220 module for various sensors.
Lists and describes certified sensors available through Dynon Avionics for the SV-EMS-220.
Lists commonly used tools and equipment that may apply to the installation.
Explains how to use EMS D37 connector pins to monitor voltage in the electrical system.
Provides guidance on EGT sensor wire length, extension, and placement on the exhaust manifold for accurate readings.
Details CHT sensor wire length, extension, and installation using bayonet adapters on engine cylinders.
Explains how to set tachometer pulses/revolution and options for connecting tachometer inputs on the SV-EMS-220.
Describes the integral assembly, wiring, and mounting of the Dynon Avionics Manifold Pressure Sensor.
Guides on securely mounting the oil pressure sensor to the aircraft structure and using appropriate fittings.
Details connecting oil temperature sensors to the SV-EMS-220 and proper installation according to engine manufacturer's directions.
Instructs on mounting the fuel pressure sensor securely to aircraft structure, avoiding engine ports, and using appropriate fittings.
Explains how to configure the fuel flow transducer using pulses/gallon value and provides connection details.
Discusses connecting resistive and capacitive fuel level sensors to the SV-EMS-220.
Details mounting the ammeter shunt to prevent electrical contact and describes three installation locations for current flow indication.
Guides on installing the carburetor temperature sensor in the venturi area where ice first begins to form.
Explains connecting and calibrating position potentiometers for trim and flap indicators on the EMS.
Describes utilizing any Dynon Avionics temperature sensor as a general purpose sensor for inputs like cabin temperature.
Explains how to use a contact to monitor landing gear state and enable audio alerts, naming the contact GEAR 1-4.
Details wiring and configuring an LED or incandescent lamp as an External Alarm Light for EMS warning conditions.
Guides on specifying engine type, horsepower, RPM, and setting Hobbs and Tach time via the Engine Information Wizard.
Describes how sensors are defined, mapped to SV-EMS-220 pins, and their settings configured within SkyView.
Explains how to map SV-EMS-220 pin numbers to physical sensors using premade files or manually.
Details configuring alarm and graphical properties for EMS sensors, including alarm settings, display limits, and ranges.
Explains how to set pulses/gallon for the fuel flow sensor and configure fuel computer presets.
Provides a procedure to manually configure sensor settings for alarm, graphical display, units, and ranges.
Guides on configuring the style and layout of onscreen EMS gauges on various engine pages.
Explains that fuel level sensors and position potentiometers must be calibrated using SkyView's onscreen wizards.
Discusses considerations for laying out engine sensors on the ENGINE BOTTOM BAND page, including dial and bar graph placement.
Explains the SV-GPS-2020's ability to receive satellite-based WAAS correction data for improved positional accuracy.
Provides guidelines for mounting the SV-GPS-2020 on the upper fuselage for an unobstructed sky view, avoiding transmitting antennas and shadows.
Details the wiring of the SV-GPS-2020, including power, ground, and serial connections to SkyView displays.
Guides on configuring serial port 5 for the SV-GPS-2020, setting input device, function, baud rate, and output device.
Covers basic serial port functionality checks and troubleshooting steps for the SV-GPS-2020 installation.
Explains how to verify GPS signal reception and status, including satellite reception and fix quality indicators.
Provides guidance on verifying GPS signal reception by moving the aircraft to an open area with an unobstructed sky view.
Details necessary steps for FAA 2020 ADS-B Out mandate compliance, including software updates and GPS data source configuration.
Describes mounting the SV-XPNDR-261 in a convenient location, considering heat sources and airflow, and securing the mounting tray.
States that the SV-XPNDR-261 meets TSO requirements without forced air-cooling.
Lists items needed for installation not included in the SV-XPNDR-261 package, such as antenna, cables, and mounting hardware.
Covers harness construction, D25F connector pinout, and wiring details for connecting the SV-XPNDR-261.
Explains how to set up the SV-XPNDR-261 as a serial device in SkyView and configure its related display settings.
Details selecting the serial port for the SV-XPNDR-261 connection and configuring the input device.
Covers essential settings for the transponder, including STATUS, GPS DATA, TRANSPONDER HEX CODE, and AUTO ALT/GND.
Discusses equipping for ADS-B Out mandate compliance, including transponder and GPS requirements.
Explains that altitude encoder calibration is not necessary as SkyView uses SV-ADAHRS-200 for pressure altitude.
Provides instructions on how to update the SV-XPNDR-261 software using a USB flash drive, recommending powering off other displays.
Outlines required post-installation checks for transponder operation, including Mode S interrogations, altitude verification, and squat switch indications.
Explains the transponder's self-diagnostic capability and provides a table for interpreting messages and recommendations.
Provides guidelines for choosing a location for the SV-ARINC-429 module, considering vibration, humidity, and working space.
Details connecting the SV-ARINC-429 module to the SkyView network and compatible ARINC-429 devices.
Shows the pinout for the SV-ARINC-429 D25M connector, detailing functions and notes for each pin.
Illustrates preferred connection schemes between SV-ARINC-429 and common radios and GPS units.
Provides typical Garmin and SkyView configuration settings for combining these products.
Details typical Garmin and SkyView configuration settings for GTN series devices with SV-ARINC-429.
Guides on configuring ARINC-429 settings in SkyView, including input/output speed, navigation source, and auto switch options.
Specifies mounting the SV-ADSB-472 on the avionics tray or another convenient location, considering space for cables and connectors.
Provides a step-by-step procedure for installing the SV-ADSB-472, including selecting position, securing the device, and listing additional required items.
Details connecting the SV-ADSB-472 to the SkyView system using the SV-HARNESS-ADSB harness and its D9F connector.
Explains the power requirements for the SV-ADSB-472 and the need to connect to aircraft power, not SkyView voltage outputs.
Guides on establishing communication between SV-ADSB-472 and SkyView via a bidirectional serial connection, noting parallel connections for multiple displays.
Recommends a 978 MHz Rod type antenna for the SV-ADSB-472 and provides guidance on antenna siting and cable routing.
Discusses the importance of a ground plane for monopole antennas and provides critical dimensions for optimal performance.
Specifies acceptable coaxial cable characteristics, including loss, impedance, and braid screens for routing.
Describes the technique for attaching an antenna cable to a BNC Male connector, noting the SV-ADSB-472 has a BNC Female connection.
Guides on configuring the SV-ADSB-472 within the SkyView system, including serial port setup and traffic display settings.
Details procedures for confirming communication and status of the SV-ADAHRS-472 after configuration.
Shows recommended panel cutouts, mounting hole patterns, and dimensions for SV-COM-PANEL/V and SV-COM-PANEL/H.
Covers power input, audio signal grounding, audio shielding, and SkyView network connections for the SV-COM-X83 system.
Guides on configuring the SV-COM-X83 within the SkyView Network and adjusting COM RADIO settings like squelch and mic gain.
Explains how to display the status of a COM radio on the SkyView top bar for selected radio and frequency settings.
Lists on-ground checks for SV-COM-PANEL buttons, knobs, dimming, and PTT functionality.
Introduces autopilot servo installation, emphasizing aircraft-model specificity and referring to the AML and Servo Installation Manual.
Provides general advice on wiring choice to minimize voltage drop and conduct required current without overheating.
Emphasizes care in aircraft wiring to prevent chafing, excessive flexing, or connection failures due to vibration.
Describes adjustable parameters in the Autopilot Setup Menu for tuning autopilot behavior, accessible after servo test.
Explains the two distinct control schemes: SIMPLIFIED and EXPERT, noting EXPERT mode requires two servos.
Details how SkyView displays a flight director with SINGLE CUE or DUAL CUE styles for autopilot control cues.
Covers roll axis torque setting to prevent slip while allowing pilot override, and includes a test procedure for servo override force.
Explains the Default Climb Vertical Speed and Default Descent Vertical Speed parameters for autopilot control.
Discusses setting the maximum airspeed parameter, recommending adjustment with the AP disengaged.
Explains setting the minimum airspeed for autopilot engagement and how SkyView indicates when airspeed drops below this limit.
Covers configuring disengage button options like 'Hold to Engage' and 'Enable Broken Line Detect'.
Shows installation dimensions for the SV-BUTTON-LEVEL, including panel cut-out and mounting hole details.
Details the electrical connections for the SV-BUTTON-LEVEL, including power, ground, and SkyView display pin connections.
Provides recommendations for connecting the External LEVEL Button to multiple displays for redundancy, superseding prior guidance.
Presents two options for connecting SV-BUTTON-LEVEL to multiple displays for failover/redundancy, including using diodes.
Describes the red, momentary button for autopilot disconnect, its installation on the stick or yoke, and required resistor.
Details the installable instrument panel version of the autopilot disconnect button, its backlighting control, and appearance.
Provides mounting dimensions for the SV-BUTTON-APDISC, including panel cut-out and mounting hole details.
Details the electrical connections for the SV-BUTTON-APDISC, including wire color and connection points.
Lists the essential steps for installing a Dynon EFIS-D10A, from power connection to panel installation.
Specifies the current requirements at 12V and 24V DC, and the recommended circuit protection for the EFIS-D10A.
Provides the weights of the EFIS-D10A and associated Dynon-supplied sensors for aircraft weight and balance considerations.
States the operating temperature range for the EFIS-D10A, which is -22° to 122° F (-30° to 50° C).
Indicates the EFIS-D10A has a single power input located on the DB25 connector.
Details the procedure for installing the backup battery into the EFIS-D10A unit, including screw tightening torque.
Provides outside dimensions and considerations for mounting the EFIS-D10A, including panel angle and obstructions.
Guides on mounting the EFIS-D10A directly into the panel using studs, washers, and nuts, ensuring proper alignment.
Explains how to connect pitot and static lines using standard 1/8” NPT Male fittings, referencing a back view diagram for placement.
Outlines essential calibration and configuration steps required before using the EFIS-D10A, ensuring proper performance.
Explains how SkyView configurations synchronize automatically across multiple displays, except for specific local settings.
Illustrates the front of an SV-D1000 display, identifying important parts like the top bar, screen, joysticks, and buttons.
Describes the use of joysticks and buttons for unit operation, menu navigation, and value adjustment, including knob functions.
Explains the menu structure (SETUP MENU > MENU > ... > PAGE/WIZARD) and how to navigate through it.
Covers basic procedures for displays, including turning systems on/off and handling loss of aircraft power with SV-BAT-320.
Details how to toggle SkyView system power for one or multiple displays, including using button 1.
Explains how the system behaves during aircraft power loss when an SV-BAT-320 is connected, including indefinite power or 30-second countdown.
Provides instructions for instantly rebooting the system by pressing specific buttons simultaneously, useful for troubleshooting.
Explains how to adjust display brightness manually or automatically via the ambient light sensor.
Describes specifying which bug a knob or joystick adjusts when rotated, enabling desired bugs in the PFD menu.
Explains accessing the Setup Menu or In-Flight Setup Menu by pressing buttons 7 and 8 simultaneously.
Lists links to useful menus during flight, such as ADAHRS Source Selection and Autopilot Setup.
Provides an overview of system configuration options, including SYSTEM EVENT, SYSTEM SOFTWARE, and SYSTEM SETUP.
Appears only if the SkyView display detects a 'system event,' providing instructions on what to do next.
Details functions for updating software, loading/deleting files, and exporting system settings using a USB flash drive.
Contains menus for the entire SkyView system, synchronizing settings across displays, including network setup and aircraft information.
Covers settings specific to individual SkyView displays, such as installed databases, hardware information, and brightness setup.
Includes menus for Primary Flight Display settings, such as ADAHRS source, pitch adjust, airspeed limitations, and vertical speed scale.
Contains menus for Engine Monitoring System pages and data sources, including engine information and sensor setup.
Includes menus and pages related to the MAP page and data sources, such as terrain warnings and base map settings.
Configures autopilot system aspects, including status, controls (EXPERT/SIMPLIFIED), roll/pitch axis, disengage button, and flight director.
Contains options to set up and configure the SV-XPNDR-261 module, including status, GPS data, HEX CODE, and AUTO ALT/GND.
Provides links to menus for ADAHRS calibration, EMS sensor calibration, AP servo calibration, and trim motor configuration.
Enables features like airport, airspace, obstacles, traffic display, procedure charts, and synthetic vision when GPS and databases are installed.
Details the various databases used for moving map and navigation, including Charts, Aviation, Obstacles, Terrain, Base Map, and Stadium TFR.
Allows users to view installed databases, their versions, and expiration dates, with popup messages for expired data.
Explains SkyView uses high-resolution terrain databases for topographic maps and Synthetic Vision, offering downloadable files for different regions.
Describes how aviation and obstacle databases display airports, runways, navigation aids, airspace, and obstacles on the moving map.
Covers SkyView's charting capabilities for displaying procedures, airport diagrams, and showing aircraft position on charts.
Provides free Base Map (Cultural Data) worldwide, including roads, city names, railroads, rivers, and political boundaries.
Instructions on downloading and importing database files from Dynon Avionics, Jeppesen, or PocketFMS onto a USB flash drive.
Recommends using iCloth Avionics wipes and advises against using solvents that can damage the bezel and anti-glare coating.
Explains how to save screenshots to a USB flash drive for sharing with Dynon Avionics Technical Support or for personal records.
Describes how to save system configuration settings to a USB flash drive for backup or restoring to a new display.
Details the procedure for saving a diagnostic file, requested by Dynon Avionics Technical Support for troubleshooting AP performance.
Indicates an abnormal number of errors on the internal Solid State Disk (SSD), requiring factory repair.
Provides procedures for returning SkyView displays, ADAHRS modules, and autopilot servos to service after repair.
Explains how a multi-display system can continue operation with one display failed or powered off, dependent on network connections.
Describes accessing vital operational information via the Display Hardware Information Page, including serial number, software version, and voltage.
Lists periodic checks mandated by regulations, such as transponder tests, pitot/static system tests, and annual SV-BAT-320 battery tests.
Assumes an initial test is done and details the procedure for the annual test to ensure the battery remains capable.
Provides troubleshooting steps for SkyView network problems, including checking wiring, unplugging modules, and observing LED status.
Explains how SkyView detects and annunciates problems with SkyView Network wiring or module failures.
Troubleshooting steps if compass calibration fails, emphasizing the need for valid GPS signal and checking ADAHRS status and location.
Troubleshooting steps for displays that do not power on, including checking power wiring, fuses, and Ethernet port lights.
Highlights the importance of GPS for system functions and provides troubleshooting steps for lack of GPS signal.
Instructs to ensure sensors are installed, defined, mapped, and configured per SV-EMS-220 installation instructions.
Lists approximate weights for various SkyView and Dynon Avionics equipment, including sensors and network cables.
Provides a table of compatible engine sensors, their range/type, fittings, and Dynon Avionics part numbers.
Details the specifications of the SV-BAT-320, including cell description, chemistry, voltage, current, and shipping safety.
Provides detailed specifications for the SV-XPNDR-261 transponder, including compliance, FCC ID, software, power, and physical dimensions.
Covers the SV-XPNDR-261's support for Extended Squitter ADS-B out and its DO-260B compliance.
Lists the ADS-B parameters transmitted by the SV-XPNDR-261 when connected to an appropriate GPS receiver.
Details GPS units compatible with SV-XPNDR-261 for a 14 CFR § 91.227 compliant ADS-B Out installation.
Specifies GPS units that form the basis of an AMC20-24 compliant ADS-B installation with SV-XPNDR-261/262.
Explains how the SV-XPNDR-261 reports ADS-B surface/airborne messages via squat switch or automatic detection.
Provides specifications for the SV-COM-X83, including compliance, FCC identification, and power requirements.
Details the environmental test results for the SV-COM-T8, covering temperature, altitude, vibration, and fluids susceptibility.
Lists specifications for the SV-GPS-2020, including compliance, WAAS reception, data interface, and physical dimensions.
Recommends 22 AWG wire for power/ground lines, consulting wire sizing charts, and using circuit breakers or fuses.
Emphasizes connecting sensor grounds to SV-EMS-220 ground pins for minimal voltage difference and ensuring solid electrical connections.
Recommends specific Mil Spec DSUB crimp pins and indentation contact crimpers for avionics applications.
Recommends using the included harness but provides guidance for fabricating custom harnesses using AC43.13-1B and AC43.13-2B.
Advises bundling wires with heat shrink and strain relieving them when exiting connectors.
Notes the unique USB cable in SV-HARNESS-D37 and recommends USB extension cables instead of terminating typical USB cables.
Provides specifications for connecting a non-Dynon Avionics harness to the SV-BAT-320 for proper charging and operation.
Illustrates connectors on SkyView displays, ADAHRS, EMS, GPS, SV-BAT-320, servos, and pinout tables.
Shows the pin numbering for the servo's D9M connector, used with the SV-NET-SERVO harness.
Details the D37M connector pinout on SkyView displays and the corresponding wire colors from the SV-HARNESS-D37.
Illustrates the basic SkyView display D37 electrical connections, showing power, ground, serial, and other inputs/outputs.
Provides the pinout and wire colors for SkyView Network D9M connectors used for device communication.
Details the pin numbering for the SV-EMS-220 D37M connector used for engine sensors and the D25F connector for thermocouples.
Shows the pinout for the SV-ARINC-429 D25F connector, detailing functions and notes.
Details the pin numbering for the SV-ADSB-472 D9F connector and its wiring harness.
Provides the pinout for the SV-XPNDR-261 D25F connector and its corresponding wire colors from the SV-HARNESS-XPNDR.
Details the pin numbering for the SV-AP-PANEL's D15M connector used for trim control, servos, and buttons.
Shows the pin numbering for the SV-COM-PANEL's D15M connector used for transceiver connection and optional pushbutton input.
Details the pin numbering for the SV-COM-T8's D25M connector used for connection to the SV-COM-PANEL.
Details industry standard NMEA 0183 Version v4.00 sentences for serial output, including BASIC and FULL formats.
Describes the format of DYNON ADAHRS serial output data, including start character, data type, system time, pitch, roll, and heading.
Details the format of DYNON SYSTEM serial output data, including start character, data type, system time, and heading bug.
Explains the format of EMS data output, including oil pressure, temperature, RPM, manifold pressure, fuel flow, and fuel level.
Describes four retrievable data logs (User Data, Recent Flight, Alert, History) that can be exported for analysis.
Details the filename format and content of the User Data Log, which records the entire state of the SkyView system.
Describes the Recent Flight Data Log, which records the most recent 15 minutes of flight at a data recording rate of 16 times per second.
Explains that the Alert Data Log appends a new record for each SkyView alert, useful for diagnosing alerts that clear automatically.
Describes the History Data Log as a cumulative history of files loaded and changes made, used for troubleshooting.
Covers choosing the data recording frequency and clearing data logs via the SETUP MENU.
Instructs on exporting data logs to a USB flash drive, recommending a separate drive per engine for dual-engine configurations.
Explains how to display raw data from engine sensors to assist in troubleshooting sensor issues, showing pin mapping and data format.
Explains that personalized checklists can be displayed in SkyView via TOOLS > CHECKLIST, requiring a UTF-8 character encoding.
Details how to save checklist files using UTF-8 character encoding in Mac TextEdit and Windows Notepad for proper SkyView display.
Provides an example checklist format and notes on character limits for display on SkyView screens.
Explains checklist numbering, title line format, and item numbering conventions for creating checklists.
Introduces a tool developed by Dynon Avionics for generating checklists from Excel, simplifying formatting and content focus.
Guides on saving a checklist file to USB and loading it into SkyView, including error handling and synchronization across displays.
Shows how checklists are displayed in various window sizes (40%, 50%, 60%) and how they interact with other displayed data.
Lists external switches, controls, and indicators compatible with SkyView units, referring to relevant sections for detailed installation instructions.
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