Dynon Avionics SkyView SV-D700 User Manual
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Dynon Avionics SkyView SV-D700 User Manual

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SkyView
Pilot's User Guide
This product is not approved for installation in type certificated aircraft
Document 101321-012, Revision M
For use with firmware version 5.1
January, 2013
Copyright © 2009-2013 by Dynon Avionics, Inc.
Permission to print this this manual is granted to third parties

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  • Page 1 SkyView Pilot’s User Guide This product is not approved for installation in type certificated aircraft Document 101321-012, Revision M For use with firmware version 5.1 January, 2013 Copyright © 2009-2013 by Dynon Avionics, Inc. Permission to print this this manual is granted to third parties...

  • Page 3: Contact Information

    Contact Information Dynon Avionics, Inc. 19825 141 Place NE Woodinville, WA 98072 Phone: (425) 402-0433 - 8:00 AM – 5:00 PM (Pacific Time) Monday – Friday Dynon Technical Support available 7:00 AM–4:00 PM (Pacific Time) Monday – Friday Email: support@dynonavionics.com Fax: (425) 984-1751 Dynon Avionics offers online sales, extensive support, and frequently updated information on its products via its Internet sites:...
  • Page 4 Dynon Avionics retains the exclusive right to repair or replace the instrument or firmware or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. These instruments are not intended for use in type certificated aircraft at this time.

  • Page 5: Revision History

    Revision History Revision Revision Date Description December 2009 Initial release Document number changed to 101321-001. Minor style, grammar, and cross reference changes and corrections. Added information regarding Autopilot servos in applicable sections. Addressed screen synchronization in applicable sections. SV-D700 and SV-D1000 Operation Chapter updates: ...
  • Page 6 Revision Revision Date Description Added information about User Waypoint power user feature that is fully documented on wiki web page. Added information about menu changes that may be present in SLSA and other aircraft that SkyView is integrated into as an OEM component. Added transponder operation information and specifications.
  • Page 7 Revision Revision Date Description Clarified that Jeppesen data must be transferred to USB stick via the Jeppesen JSUM program. Added PocketFMS information. Clarified bearing sources and limitations (SBY bearings from some NAV radios and no availability of bearings from LOCs). Clarified EMS timers.

  • Page 9: Table Of Contents

    Table of Contents Contact Information ..............................iii Copyright ..................................iii Limited Warranty ................................iii Revision History ................................v 1. Introduction Before You Fly ................................1-1 Warning ..................................1-1 Dynon Avionics Product Registration ......................... 1-1 About this Guide ................................. 1-1 2. System Overview SV-D700 and SV-D1000...............................
  • Page 10 Table of Contents License Information ..............................7-1 Databases ................................... 7-3 GPS Source .................................. 7-6 Moving Map Page Layout ............................7-7 Moving Map Symbology ............................. 7-8 MAP Menu ................................7-24 Navigation Mapping Software Features ........................7-26 Weather and TFR Information ..........................7-47 8.

  • Page 11: Introduction

    1. Introduction Thank you for purchasing the Dynon Avionics SkyView system. This chapter provides some important cautionary information and general usage instructions for this guide. The printed version of this guide is in grayscale. Some figures and diagrams contain important color information.
  • Page 12 Introduction This guide discusses the most common operation scenarios. If you have an operational issue that is not discussed in this guide, you can find additional operational information on Dynon’s internet sites:  wiki.dynonavionics.com–Dynon’s Documentation Wiki provides enhanced, extended, frequently updated online documentation contributed by Dynon employees and customers.

  • Page 13: System Overview

    2. System Overview This chapter provides a general overview of the various parts of SkyView as well as a theory of operation. The information in this chapter serves as a reference only and helps familiarize you with the inner workings of the units. It should not be used for diagnostic or reparative work. Dynon Avionics provides periodic firmware updates that enable new functionality.
  • Page 14 System Overview functionality until full troubleshooting can be performed on the ground. These alerts are presented in SkyView’s alerting system, which is described in a later chapter of this guide. Serial I/O SkyView displays have five RS-232 serial ports for connection to compatible equipment. All serial ports are wired into the SkyView Display Harness (SV-HARNESS-D37).

  • Page 15: Sv-Adahrs-20X

    System Overview SV-ADAHRS-20X This guide uses SV-ADAHRS-20X to refer to both the SV-ADAHRS-200 and the SV- ADAHRS-201. The SV-ADAHRS-200 and SV-ADAHRS-201 are identical in performance and are designed to work together as a redundant ADAHRS solution. An SV-ADAHRS-200 must be installed in your SkyView system in order to use an SV- ADAHRS-201.

  • Page 16: Sv-Ems-22X

    System Overview Attitude Calculation The SkyView artificial horizon display (attitude) is generated via a complex algorithm using a multitude of sensors as described in Table 2. In normal operation SkyView uses airspeed to provide superior attitude accuracy. Compass Accuracy Effects on Synthetic Vision, Map Performance, and Autopilot It is critical that the magnetic heading be as accurate as possible for optimal Synthetic Vision and Moving Map performance.

  • Page 17: Autopilot Servos

    System Overview When connected, the battery's charge level is automatically managed by the SkyView display it is physically connected to. This ensures that SkyView has a fully charged backup battery in case of emergency. Charging a completely discharged battery may take up to 4 hours. To conserve your aircraft battery, the SV‐BAT‐320 is only charged when SkyView detects that your alternator or generator is online.

  • Page 19: Sv-D700 And Sv-D1000 Operation

    (e.g., adjusting the barometer), refer to the PFD, EMS, and Moving Map operation chapters. The SkyView SV-D700 and SV-D1000 displays are identical in functionality and presentation. The only difference is in the size and resolution of the screen.

  • Page 20: Joystick And Button Operation

    SV-D700 and SV-D1000 Operation Note the Top Bar, screen, joystick and button labels, light sensor, two joysticks and eight buttons. The Top Bar is user configurable and displays important textual information. The Top Bar in the current release of SkyView only shows time and autopilot status. Future firmware updates will enable expanded functionality.
  • Page 21 SV-D700 and SV-D1000 Operation A button has a function if there is a label above it. If there is no label, there is no function. The figure below shows an example button label. Figure 3–Example Button Label When you press a button, its label is highlighted. When you release the button, its action is invoked.

  • Page 22: Menu Navigation

    SV-D700 and SV-D1000 Operation Menu Navigation All menu navigation in this guide starts at the In Flight Setup Menu. After the display turns on, you will see a screen similar to the one in Figure 1. This guide refers to the label bar at the bottom of the screen as the Main Menu. Throughout this guide, the “>”...

  • Page 23: Basic Display Operation Procedures

    SV-D700 and SV-D1000 Operation Basic Display Operation Procedures This subsection covers basic operation procedures for displays. Detailed instructions for various menus and individual menu items are described in the SkyView System Installation Guide. How to Turn the System On or Off Table 4 summarizes the procedures for toggling SkyView system power states.
  • Page 24 SV-D700 and SV-D1000 Operation How to Reboot the Display Press and hold buttons 1, 2 and 5 simultaneously to instantly reboot the system. This may be helpful if you need to cycle power after changing certain settings and for general troubleshooting.

  • Page 25: Screen Layout Configuration

    SV-D700 and SV-D1000 Operation How to Enter the In Flight Setup Menu When airspeed is greater than zero or groundspeed is greater than 15 knots, simultaneously pressing and holding buttons 7 and 8 when on the Main Menu will open the In Flight Setup Menu.
  • Page 26 SV-D700 and SV-D1000 Operation Table 5–Onscreen Data Allotments The following diagram illustrates example screen layout configurations. Figure 6–Example Screen Layout Configurations Manufacturers that install SkyView into their aircraft can choose to standardize the screen layouts that are available. When a SkyView system is set up this way, you may not be able to remove some or all of the pages on a display.
  • Page 27 SV-D700 and SV-D1000 Operation Reversion Mode In multi-display SkyView systems, you can specify a reversion mode that automatically changes the screen configuration to a specific layout when only one display remains powered on. For example, if you normally have your left display configured to show PFD and your right display showing Engine and Map, reversion mode could be configured to show all three pages automatically on the single remaining display, should the other fail.

  • Page 29: Pfd Operation

    4. PFD Operation One of the main functions of SkyView is its Primary Flight Display (PFD) with Synthetic Vision. This chapter highlights the layout of the PFD page, its symbology, and contains instructions for adjusting bugs. SkyView’s PFD requires data from an SV-ADAHRS-20X module. Synthetic Vision further requires valid GPS data.

  • Page 30: Pfd Symbology

    PFD Operation  Altimeter with Altitude Bug, Altitude Trend Rate, Barometer Setting, and Density Altitude  Vertical Speed Indicator with Vertical Speed Bug  Compass Rose/Directional Gyro with Heading Bug  Slip/Skid Ball  Angle of Attack Indicator (not shown in Figure 7) ...
  • Page 31 PFD Operation Figure 8–All Bugs On For example, if the vertical speed bug (VS) is off, it is not an option in the Joystick Menu as illustrated in Figure 9. The same is true for other bugs. Figure 9–Vertical Speed Bug Off If all bugs are off, none of them show up in the Joystick Menu as illustrated in Figure 10.

  • Page 32: Attitude Indicator

    PFD Operation The airspeed tape displays indicated airspeed including gray, white, green, yellow, and red ranges to provide a graphical representation of aircraft speed in relation to the aircraft's limits. These ranges are controlled by setting the airspeed limitations for the aircraft. Refer to the SkyView System Installation Guide for instructions on how to configure the airspeed limitation color thresholds.
  • Page 33 PFD Operation Figure 13–Example Attitude Indicator The roll scale contains tick marks at 10, 20, 30, and 60 degrees and larger white triangles at 0 and 45 degrees. The roll pointer (small yellow triangle on the bottom side of the roll scale) points to your current bank angle.
  • Page 34 PFD Operation GPS Assist In the event of airspeed loss (due to icing or other blockage) an accurate attitude is maintained if there is an accurate GPS ground speed source. When in this mode, a magenta GPS ASSIST message is displayed on the PFD and the ground speed is displayed below the indicated airspeed (IAS).
  • Page 35 PFD Operation Altimeter The altimeter is displayed on the right side of the PFD. It incorporates an altitude tape and digital readout, Density Altitude (DA), barometer setting, and altitude bug. Figure 15 is an example SkyView altimeter. The altitude tape displays 200 units above and below the current altitude digital readout.
  • Page 36 PFD Operation Altitude Bug The altitude bug is displayed in cyan on the altitude tape and its associated digital readout is displayed at the top of the altimeter. The altitude bug is used as a target for the pitch axis of the SkyView Autopilot when a pitch axis servo is installed.
  • Page 37 PFD Operation Vertical Speed Indicator The vertical speed indicator (VSI) is displayed to the immediate right of the altimeter and incorporates a vertical speed tape, vertical speed pointer (with digital readout), and bug. Figure 16 is an example SkyView VSI. The VSI tape can display ±1000 units, ±2000 units, or ±4000 units.
  • Page 38 PFD Operation The vertical speed bug is used by the autopilot as a target vertical speed when it is climbing or descending. Reference the Autopilot Operation Chapter for more information regarding autopilot functionality, symbology, and operation information. Compass Rose/Directional Gyro The compass rose/directional gyro is displayed on the lower center of the PFD and incorporates a magnetic...
  • Page 39 PFD Operation To set the heading/track bug: 1. Enter the Joystick Function Menu. 2. Move the joystick up or down to highlight (HDG) or (TRK). 3. Move the joystick left or right to close the menu (this is optional). (HDG) or (TRK) will now display just above that joystick. The heading/track bug setting on the PFD will be outlined to signal that it is selected.
  • Page 40 PFD Operation Course Indicator Figure 20 - HSI Course Indicator The course indicator has an arrow at its end which points to the currently selected course. When a GPS source is selected, course direction is normally set implicitly by the programmed route.
  • Page 41 PFD Operation direction as the arrow at the end of the course line, then that is a "to" indication. If it is pointing the opposite direction of the arrow at the end of the course line, then that is a "from" indication.
  • Page 42 PFD Operation HSI Info Items Figure 25 - HSI GPS Info Figure 26 - HSI NAV Info (LOC Example) Textual info items that provide additional data about the HSI source are displayed to the left of the HSI display. The information available depends on the data being provided by the HSI source.

  • Page 43: Adahrs (Flight Instrument) Redundancy And Cross-Checking

    PFD Operation Outside air temperature (OAT) as shown in Figure 30 is displayed in the very lower-right corner of the PFD. Units can be set to degrees Fahrenheit or degrees Figure 30– Celsius. Reference the SkyView System Installation Guide for instructions on Example OAT how to change the displayed units.
  • Page 44 PFD Operation Figure 32 - ADAHRS Cross-Checking Disagreement Once SkyView has annunciated a cross-check comparison problem, press COMPARE to see both ADAHRS side-by side. The ADAHRS that was previously displayed on the PFD is labeled “ACTIVE”, while the one that was not previously being displayed - but which was being used as the cross-check reference –...
  • Page 45 PFD Operation Once you have determined which ADAHRS is incorrect, press DISABLE to tell SkyView not to use it for the duration of the flight: Figure 34 - ADAHRS Cross-Check Comparison (one ADAHRS disabled) Press exit to return to normal operation. The PFD will annunciate that only a single ADAHRS is available for use: Figure 35 - Single ADAHRS Mode Flag If, after you’ve entered the ADAHRS comparison screen, you do not disable an ADAHRS, a red...
  • Page 46 PFD Operation If you are on the ground, this will be under SETUP MENU > PFD SETUP > ADAHRS SOURCE SELECTION. ADAHRS Status The ADAHRS labeled ACTIVE is the one that is being displayed on the PFD. An ADAHRS labeled STANDBY is being used for cross-checking, but it is not being displayed on the PFD.

  • Page 47: Pfd Menu

    PFD Operation PFD Menu The PFD Menu is accessible from the Main Menu by pressing PFD (MAIN MENU > PFD). Users can reset the baro, toggle Synthetic Vision on or off, and configure the bearing and NAV sources. Back Press BACK to return to the Main Menu. G Meter Press G METER to toggle the G Meter on and off.
  • Page 48 PFD Operation Synthetic Vision (SYNVIS) Synthetic Vision depictions of terrain, runways, obstacles, and other information are meant as informational aids only. These depictions should not be used as the primary means for obtaining situational awareness of these features in flight. Terrain data is obtained from third party sources.
  • Page 49 PFD Operation  Runway edge lines  Runway centerline  Runway numbers  Runway thresholds / displaced thresholds  Aiming point markings: two white strips drawn 1000’ after the threshold on runways 4000’ and longer  Runway width threshold markings: drawn immediately after the runway threshold, these groups of parallel lines visually indicate the width of the runway in the following manner according to runway width: o 0’-59’...
  • Page 50 PFD Operation Figure 38 - Traffic Display on Synthetic Vision Traffic information is informational only, and does not relieve the pilot-in-command of his or her responsibility to see and avoid traffic. The graphical depiction of traffic is only displayed when Synthetic Vision is turned on via the PFD>SYNVIS menu option.
  • Page 51 PFD Operation traffic targets that are shown to the left or right of the center of the attitude indicator are not directly ahead of you. Traffic displayed on the PFD page can be configured to include just Traffic Advisories (TA), all targets, or no targets. See the SkyView Installation Guide for information on how to configure how traffic is displayed.
  • Page 52 PFD Operation systems (such as the Garmin 430), and panel-mounted navigation radios (such as the Garmin SL30). Reference the SkyView System Installation Guide for more information regarding external serial device installation and configuration. Also note that using the NAVSRC button to toggle the HSI source does not affect what is displayed on the SkyView map: it is always sourced from SkyView’s own internal Direct-To and flight planning capabilities.

  • Page 53: Ems Operation

    5. EMS Operation This chapter describes SkyView EMS functionality and a few of the advanced ways to use it to monitor the health and operation of your engine. This chapter references the Engine Page. This page should have been configured during SkyView installation.

  • Page 54: Rotax 912 Behavior

    EMS Operation The green markings on pitch/roll/rudder trim indications, if they exist, nominally depict the take-off position markings as defined during calibration. Combined CHT/EGT Gauge The combined CHT/EGT Gauge shown in Figure 45 displays all of the engine’s CHTs and EGTs in one compact gauge.

  • Page 55: Engine Menu

    EMS Operation Oil Temperature Gauge for Rotax 912: When OIL TEMP < 190ºF, the OIL TEMP gauge displays these ranges:  100-120 and 230-266ºF in YELLOW  120-190ºF in GREEN if OIL TEMP has been above 190ºF “more recently” than OIL TEMP was below 120ºF;...
  • Page 56 EMS Operation temperature itself due to space constraints). Given this information, you may set your mixture more accurately to achieve a given EGT delta value on either the rich or lean side of peak EGT. This is depicted in Figure 47. Figure 47–EGTs Peaking After the last cylinder peaks during a leaning operation the difference in fuel flow between the first and last cylinder peaks is displayed.

  • Page 57: Timers

    EMS Operation leaning that this data matches your install and engine. If the EMS does not have all of the information it needs to calculate the peak state, UND (undetermined) is shown. FUEL The FUEL menu primarily contains controls for adjusting the fuel computer. See the dedicated Fuel Computer section for details on fuel computer operation.

  • Page 58: Fuel Computer

    EMS Operation The Flight Trip Timer - labeled FLT TRIP when displayed on an Engine Page -runs any time that SkyView determines that the aircraft is in flight, just like the Total Flight Timer. Unlike the Total Flight Timer, it can be reset by pressing ENGINE > CLR TMR. Fuel Computer The Fuel Remaining, Fuel Used, Fuel Efficiency, Fuel at Waypoint, and Range values are not directly measured.
  • Page 59 EMS Operation Fuel computer adjustments are made under the ENGINE > FUEL menu. When FUEL is pressed, the window in Figure 49 is displayed: Figure 49–Fuel Computer and Fuel Menu  “Fuel Computer Quantity Adjustment” is the amount of fuel that you have told the fuel computer to presently add or subtract from the previous total fuel state.

  • Page 60: Vp-X Operation

    EMS Operation Auto Fuel Detect The fuel computer can optionally be configured to detect when fuel has been added while SkyView was off, as would be the case during a normal refueling operation. When configured to detect fuel additions, SkyView will automatically display the FUEL menu upon startup as a reminder to adjust the fuel computer, along with a FUEL MISMATCH message to indicate that the fuel measured by the in-tank fuel quantity sensors does not closely match the fuel computer’s fuel remaining value.
  • Page 61 EMS Operation  On the Engine Page: Widgets for VP-X measured battery voltage, VP-X measured starter status, and VP-X fault status can be added to any of the EMS pages via the EMS SETUP > SCREEN LAYOUT EDITOR. Displaying the VP-X Page The VP-X page is displayed on-demand by pressing MAIN MENU >...
  • Page 62 EMS Operation  Upper left: Main and auxiliary (if installed) alternators. The status of the alternator, as well as the amount of current (in Amps) it is producing is displayed. Current will not be displayed if an amps shunt is not installed and connected to SkyView. Yellow cautions and red warning levels are triggered at the values specified during setup.
  • Page 63 EMS Operation When a circuit is selected the menu at the bottom of the SkyView screen automatically changes to allow control of the circuit. All Circuits  RESET button: Press this button to reset any circuit that has a fault condition that the VP-X will allow to be reset.

  • Page 65: Transponder Operation

    6. Transponder Operation Dynon Avionics offers two transponder modules that can be connected to SkyView. When installed and configured, SkyView displays gain an integrated transponder that is controlled directly from the SkyView display. The SV-XPNDR-262 is a Class 2 Mode S transponder that is limited to use beneath 15,000 feet and under 175 knots.

  • Page 66: Transponder Menu

    Transponder Operation a. SBY: The transponder is on, but will not reply to any interrogations. This is the mode that the transponder is in when none of the modes below are active. b. GND: The transponder will respond to Mode S ground interrogations from surface movement radar.
  • Page 67 Transponder Operation Note that there are some situations when the selected transponder mode may be different from the status annunciated in the Transponder Status Area. For example, if you select ALT mode, but there is a squat switch installed, it will keep the transponder in GND mode until the aircraft has become airborne.

  • Page 68: Reported Pressure Altitude

    Transponder Operation Press to quickly tune the VFR squawk code. This is usually 1200 in the US and 7000 in Europe. Refer to the Installation Guide to set the VFR code that this button tunes. Once pressed, the VFR button will remain highlighted until the transponder code is changed to show that you are in VFR mode.

  • Page 69: Sv-Map-270 Navigation Mapping Software

    7. SV-MAP-270 Navigation Mapping Software This chapter outlines what users should expect from SkyView’s Navigation Mapping Software capabilities and also covers operations that are specific to this function. SkyView’s Moving Map requires valid GPS and terrain data to function as a real time, look down topographical map.
  • Page 70 SV-MAP-270 Navigation Mapping Software If Navigation Mapping Software is not available, then either the system is not licensed or there is no valid aviation database in the system. To determine which of these is the case, check the status of the license in the Setup Menu under SETUP MENU > LOCAL DISPLAY SETUP > LICENSE. See the SkyView Installation Guide for more details about using Setup to check licenses.

  • Page 71: Databases

    SV-MAP-270 Navigation Mapping Software then entered in SETUP MENU > LOCAL DISPLAY SETUP > LICENSE > LICENSE CODE. If you have more than one display in the aircraft, choose one to install it onto and provide information for only that display. Once any display is licensed, all connected displays in the Aircraft can use the Navigation Mapping Software.
  • Page 72 SV-MAP-270 Navigation Mapping Software Databases Section of this guide for instructions on how to import the file onto a SkyView display. Aviation/Obstacle Databases Aviation and obstacle databases are used to display airports, runways, nav aids, airspace, obstacles, and other aviation data on the Moving Map. It also allows SkyView to provide detailed information about aviation features.
  • Page 73 SV-MAP-270 Navigation Mapping Software  Reference the Loading Databases section below of this guide for instructions on how to import the file onto a SkyView display. Additional technical support from Jeppesen can be found online at http://www.jeppesen.com/support/technical-support.jsp Loading Databases 1. Download database file(s) from downloads.dynonavionics.com, Jeppesen, or PocketFMS.

  • Page 74: Gps Source

    SV-MAP-270 Navigation Mapping Software Removing Databases SkyView automatically removes databases when new ones are installed. They can also be removed manually by going to SETUP MENU > LOCAL DISPLAY SETUP > INSTALLED DATABASES. Highlight the database you wish to remove, and then press the REMOVE button. The FAA periodically publishes Aviation Data updates.

  • Page 75: Moving Map Page Layout

    SV-MAP-270 Navigation Mapping Software Moving Map Page Layout The Moving Map Page as shown in Figure 53 displays a real-time topographical map in Track Up or North Up mode (depending on user setting). The map is sourced from a database that is stored inside the display and correlated to your current position using a GPS feed.

  • Page 76: Moving Map Symbology

    SV-MAP-270 Navigation Mapping Software Moving Map Symbology Topography with Terrain Proximity Alerts SkyView’s Terrain Proximity Alerting should not be used as the primary terrain avoidance tool. It should be used as an aide with primary navigation instruments, charts, and other tools. Moving Map terrain is displayed in sectional chart color variations, representing various topographical elevations.
  • Page 77 SV-MAP-270 Navigation Mapping Software Distance Circle The distance shown on the map between the aircraft icon and the inner circular ring is the distance between them. The distance between the aircraft and the outer Ground Track Arc is twice this distance. Figure 56–Distance Circle This distance is displayed in the middle of the right side of the Map Page, near the Distance Circle.
  • Page 78 SV-MAP-270 Navigation Mapping Software The current ground track as shown in Figure 58 is displayed in two ways: the digital readout and the white ground track line. The border around the digital readout is normally magenta when based on the GPS ground track. When the aircraft is not moving fast enough for SkyView to reliably determine the ground track direction, magnetic heading is used instead.
  • Page 79 SV-MAP-270 Navigation Mapping Software Figure 61 - Course Line Flight Plan Legs Flight plan legs appear in the Moving Map display whenever a flight plan has been activated. The magenta line corresponds to the current leg of the Flight Plan and subsequent legs are shown in white.
  • Page 80 SV-MAP-270 Navigation Mapping Software Obstacles SkyView’s Moving Map represents obstacles using the same symbology found on sectional charts, as shown in Figure 63 and Figure 64. Only high- intensity lighted obstacles are shown as lit. The geographic location of the obstacle is represented by the tip on single icons and the point directly between the tips of group icons.
  • Page 81 SV-MAP-270 Navigation Mapping Software Airspace SkyView’s Moving Map represents different classes of airspace with the colors specified in Table 6. The floors and ceilings of airspaces are shown within each airspace segment in the familiar sectional-style notation. Airspace Type Color Example Solid orange with interior shading.
  • Page 82 SV-MAP-270 Navigation Mapping Software Airspace Type Color Example Class E (only those areas that Solid green with interior shading extend to the surface in US depictions) Restricted and Solid orange with ticks marks Prohibited Warning, Caution, Yellow tick marks (not solid) Training, and Alert Areas Military Operations Area Solid purple with ticks marks...
  • Page 83 SV-MAP-270 Navigation Mapping Software Airspace Type Color Example CTA (Control Area) Solid purple CTR (Control Zone) Blue/orange solid Mode C Veil Not shown None Upcoming Temporary Yellow Flight Restriction (TFR) Active Temporary Flight Restriction (TFR) Stadium Temporary Orange Flight Restriction (TFR) Air Defense None Identification Zone...
  • Page 84 SV-MAP-270 Navigation Mapping Software Navaids SkyView’s Moving Map displays navaids such as VORs, fixes, NDBs, and User Waypoints. VORs SkyView’s moving displays VORs, VOR-DMEs, and VORTACs with the same icons used on sectional charts as shown in Figure 65. VOR-DME VORTAC TACAN Figure 65–Moving Map VOR Icons...
  • Page 85 SV-MAP-270 Navigation Mapping Software Airports SkyView represents an airport with a circle and a text name. If more information is provided in the database, a modifier may be added to the icon. A line in the circle represents the direction of the primary runway.
  • Page 86 SV-MAP-270 Navigation Mapping Software Motorways, Primary Roads, Railroads, and Rivers SkyView displays motorways as thick solid black lines, primary roads as thinner solid black lines, railroads as thin dark lines with railroad “ties”, and rivers as thin blue lines: Table 9 - Roads, Railroads, and Rivers Customizing Displayed Map Items The display of various map elements can be customized to reduce visual clutter.
  • Page 87 SV-MAP-270 Navigation Mapping Software Figure 70 - Traffic Display on Map Page SkyView can receive traffic information from a variety of devices. These currently include the SV-ADSB-470 (US Only), TIS traffic supplied by the SV-XPNDR-26X or Garmin GTX 330 Transponders, passive traffic from the Zaon XRX, FLARM (predominantly in Europe) and the NavWorx ADS-B receivers.
  • Page 88 SV-MAP-270 Navigation Mapping Software SV-ADSB-470 Traffic Display Capabilities (US Only) The SV-ADSB-470 works in tandem with your SV-XPNDR-26X transponder modules to provide the FIS-B traffic picture around your aircraft when you have both products. This is enabled by the following bidirectional data link capability: 1.
  • Page 89 SV-MAP-270 Navigation Mapping Software Traffic is displayed using a set of symbols that are commonly used in aviation for traffic/TCAS systems. As seen in Figure 71, this includes:  A symbol that depicts the type of traffic. It can be a Traffic Advisory Symbol, Proximity Advisory Symbol, or Non-Threat Symbol.
  • Page 90 SV-MAP-270 Navigation Mapping Software considers a target a threat if the device providing traffic reports that it is a threat. The TIS system considers a target to be a threat if it is calculated to be within 1/4 mile of your aircraft at its closest approach within 30 seconds (20 seconds if the target is not reporting altitude).
  • Page 91 SV-MAP-270 Navigation Mapping Software  ZAON: A Zaon XRX.  FLARM: A device outputting FLARM format data (predominantly in Europe) Possible states include:  SkyView is receiving traffic data from the device and there is at least one target present. ...

  • Page 92: Map Menu

    SV-MAP-270 Navigation Mapping Software B system delivers all known ADS-B equipped traffic and all radar targets that FAA radar system can see. 2. TIS transponder from SV-XPNDR-26X / Garmin GTX 330 (when in an active TIS coverage area). 3. Flarm device. 4.
  • Page 93 SV-MAP-270 Navigation Mapping Software about the airport or navaid that was most recently used or selected. The cursor will highlight the tab for the selected item type at the top of the window. From here, you can either move the CURSR joystick down to find the desired item by identifier, facility, or city. Or, move the CURSR joystick left to the RECENT tab to choose from the most recently used and viewed airports and navaids.

  • Page 94: Navigation Mapping Software Features

    SV-MAP-270 Navigation Mapping Software Figure 78 - Map Menu To select an operation from the menu, scroll up and down by turning the joystick or moving it up/down. Move the joystick left to exit the menu, or move the joystick knob right to accept/initiate the selected operation or sub-menu.
  • Page 95 SV-MAP-270 Navigation Mapping Software Figure 79–Moving Map Find Window When the Info window is first displayed it shows detailed information about the airport or navaid that was most recently used or selected. From here, you can move the CURSR joystick down to find the desired item by identifier, facility, or city*.
  • Page 96 SV-MAP-270 Navigation Mapping Software Nearest Airports, Navaids, and User Waypoints To quickly bring up a list of the nearest airports, navaids, and user waypoints press MAP > NRST. A window similar to the one seen in Figure 80 will be displayed. Figure 80–Moving Map Nearest Window Each tab in the bar of tabs at the of the Nearest window contains a list of aviation features.
  • Page 97 SV-MAP-270 Navigation Mapping Software airports have multiple runways listed under the RWY tab. Once the RWY tab is selected, different runway information can be displayed by turning or moving the CURSR knob up/down. You may press ADD->FPL from the info window to add the displayed facility as a waypoint to the Flight Plan.
  • Page 98 SV-MAP-270 Navigation Mapping Software Figure 82 - Airport Comms Info Figure 81 - Airport Info Figure 84 - Airport Remarks Figure 83 - Airport Runway Info 7-30 SkyView Pilot’s User Guide - Revision M...
  • Page 99 SV-MAP-270 Navigation Mapping Software Information available for different types of facilities include:  Name  Type (public/military/private*/vor/ndb/etc.)  Identifier  Current distance/bearing to facility  Region  Field elevation  Parking availability*  Communications frequencies  ATIS/AWOS Frequencies  Traffic pattern altitude/direction* ...
  • Page 100 SV-MAP-270 Navigation Mapping Software Figure 85 - Map/HSI with Navigation Active Clearing the Active Waypoint Press when it is highlighted to bring up the current waypoint information. From the resulting menu, press STOP to clear the active waypoint and cancel navigation. If a waypoint is selected in any window that waypoints can be selected in, pressing will immediately replace your current destination with the selected...
  • Page 101 SV-MAP-270 Navigation Mapping Software Figure 86 - Map Panning Mode To exit Map Panning Mode, press or “click” the center of the joystick. The map will revert to following the aircraft. Pressing the joystick again will return to the Map Panning Mode at the last known Map Pointer position.
  • Page 102 SV-MAP-270 Navigation Mapping Software Pressing NRST in Map Panning Mode will cause the list of nearest airports and other aviation features to be based on the location of the Map Pointer instead of the aircraft. This noted at the top of the Nearest Window. Flight Planning A Flight Plan consists of a sequence of one or more waypoints.
  • Page 103 SV-MAP-270 Navigation Mapping Software Creating and Working with Flight Plans This section describes the windows and menus that are available for creating and manipulating a Flight Plan. Flight Plan Window Press the FPL button in the MAP Menu to open the Flight Plan window and menu. The Flight Plan window contains two tabs of information: ACTIVE and IMPORT.
  • Page 104 SV-MAP-270 Navigation Mapping Software  DIST: The distance of the leg. For the active leg, it is the distance from the aircraft to the next waypoint.  ETE: The estimated time en-route for the leg, based on the current ground speed if flying, and based on the Vno speed setting if stationary.
  • Page 105 SV-MAP-270 Navigation Mapping Software Figure 89 - Flight Plan Import Tab Import Menu When the Flight Plan window is open with the IMPORT tab displayed, select one of the following menu items to proceed: BACK Press to exit the IMPORT tab and return to the ACTIVE tab of the Flight Plan window. LOAD Press to import the currently selected GPX file into the Flight Plan and activate it.
  • Page 106 SV-MAP-270 Navigation Mapping Software Figure 90 - FPL Menu Figure 91 - FPL Menu Confirmation Prompt FPL MENU Actions The following actions can be initiated from the FPL MENU:  EXIT: Select to close the Flight Plan Menu.  INSERT WAYPOINT: Select to bring up the Insert Waypoint pop-up menu. ...
  • Page 107 SV-MAP-270 Navigation Mapping Software  EXPORT FLIGHT PLAN: Select to export the current Flight Plan to a USB stick memory stick in GPX format. The filename is automatically generated using the names of the first and last waypoints. Inserting a Waypoint Waypoints can be added from the FPL MENU by selecting INSERT WAYPOINT.
  • Page 108 SV-MAP-270 Navigation Mapping Software  TRN TOO STEEP: Displayed when the required bank to complete the upcoming turn as depicted on the map is excessive. Figure 94 - Flight Plan Alert Messages Activating a Flight Plan Press the ACTIVATE button to activate your Flight Plan routing. Guidance will be provided directly to the first waypoint in the Flight Plan and along each leg in the Flight Plan thereafter.
  • Page 109 SV-MAP-270 Navigation Mapping Software Figure 95 - Active Flight Plan: Map and Flight Plan View Figure 96 -Active Flight Plan: HSI and MAP Depictions SkyView User Waypoints SkyView supports the ability to create, manipulate, and import/export User Waypoints. A User Waypoint is a point on the map which shows up as an icon of your choosing.
  • Page 110 SV-MAP-270 Navigation Mapping Software Figure 97 - Waypoint Tools in the Map Menu Move the CURSR joystick up and down to move the cursor between the various fields. Turn it to select characters. The editable fields include:  Identifier – Like other airports and navaids, the identifier is displayed on the map. ...
  • Page 111 SV-MAP-270 Navigation Mapping Software Editing and Deleting Waypoints Select MAIN MENU > MAP > MENU > EDIT USER WAYPOINTS to view a list of all current user waypoints. To modify or delete a waypoint, highlight the waypoint of interest and press EDIT or DELETE.
  • Page 112 SV-MAP-270 Navigation Mapping Software  Altitude o Integer, feet  Icon o Possible choices include: HOME ; OFFICE ; AIRPORT_FILLED ; AIRPORT_HOLLOW ; AIRPORT_GLIDER ; AIRPORT_PRIVATE ; AIRPORT_HELICOPTER ; AIRPORT_ULTRALIGHT ; AIRPORT_HANG_GLIDER ; AIRPORT_SEAPLANE ; VOR ; TOWER_TALL ; TOWER_SHORT ; PIN_GREEN ; PIN_BLUE ; PIN_RED ; PIN_YELLOW ;...
  • Page 113 SV-MAP-270 Navigation Mapping Software Using User Waypoints User Waypoints are searchable via the “USER” tab on the “Nearest” window. The “USER” tab only appears if there are User Waypoints stored in SkyView. User Waypoints can also be found like any other airport or navaid by searching on identifier or name in the Info Window.
  • Page 114 SV-MAP-270 Navigation Mapping Software o ETE (Final)  The remaining estimated time en route to the final waypoint in the flight plan. If GPS ground speed is <25 knots, your Vno speed setting is used for so that you can see approximate travel times while on the ground. o ETE (Next) ...

  • Page 115: Weather And Tfr Information

    SV-MAP-270 Navigation Mapping Software Weather and TFR Information When connected to an SV-ADSB-470 module, SkyView can display NEXRAD weather and Temporary flight Restriction (TFR) information visually on the SkyView map page. Additionally, textual METAR and TAF weather reports are available for airports that report such information. The SV-ADSB-470 receives traffic and weather via the 978 MHz UAT ADS-B frequencies, which are only utilized by the FAA’s ADS-B system.
  • Page 116 SV-MAP-270 Navigation Mapping Software weather deterioration or improvement are aggregated into SkyView’s weather reporting capability. TAFs (Terminal Area Forecasts) TAFs are future weather forecasts, centered on many (but not all) airports and include the predicted future weather conditions. NEXRAD Radar Imagery NEXRAD radar transmits short high-frequency beams of radio energy into the atmosphere from the ground at various angles and receives reflections of that energy back at the original site.
  • Page 117 SV-MAP-270 Navigation Mapping Software Figure 99 - Map Page: Terrain View (no Weather)  WEATHER: Terrain is not depicted. This allows the NEXRAD weather /TFR layers to be displayed against a dark background for maximum legibility. Other databases (aviation, obstacles, base map, etc) are still displayed. Figure 100 - Map Page: Weather View SkyView Pilot’s User Guide - Revision M 7-49...
  • Page 118 SV-MAP-270 Navigation Mapping Software  WX+TERR: The terrain layer is displayed, but in muted tones, to allow the NEXRAD weather / TFR graphics to stand out. Other databases (aviation, obstacles, base map, etc) are still displayed. Figure 101 - Map Page: WX+Terrain View NEXRAD Legend NEXRAD imagery is color-coded to indicate density of precipitation: Purple...
  • Page 119 SV-MAP-270 Navigation Mapping Software  Data has not yet been received for an area for which there is available coverage, due to the time it takes for the ADS-B system to transmit information. For example, the following figure depicts what the continental US would look like when higher resolution regional NEXRAD weather information has been received, but the lower resolution continental US (CONUS) NEXRAD imagery has not yet been received: Figure 103 - Regional NEXRAD Only / No CONUS...
  • Page 120 SV-MAP-270 Navigation Mapping Software o Current (green) – Data is between 0 and 60 minutes old. o Stale (yellow) – Data is between 60 and 75 minutes old. o Expired (red) – Data is at least 75 minutes old. METAR/TAF Information Textual METARs and TAFs are can be viewed for individual airports on their INFO pages.
  • Page 121 SV-MAP-270 Navigation Mapping Software Individual Airport METARs / TAFs When METAR and/or TAF weather reports are available for an airport, they are accessed by selecting the WX tab the INFO window for that airport. Alternatively, pressing INFO when the list of NRST WX is being shown will also bring you directly to the WX tab of the airport’s INFO PAGE.
  • Page 122 SV-MAP-270 Navigation Mapping Software Sports stadium TFRs are persistent and transmitted without active times, and thus they are always depicted in orange to distinguish them from regular TFRs. However, the restrictions are only in effect during sporting events. To reduce clutter these TFRs can be turned off and are listed as a separate option under MAP MENU >...

  • Page 123: Autopilot Operation

    8. Autopilot Operation This chapter guides you through the functionality, symbology, and operation of the SkyView Autopilot. It assumes that the Autopilot servos have been properly installed, calibrated, tested, and tuned according to the procedures in the SkyView System Installation Guide. Autopilot Safety Features The Dynon Avionics Autopilot is designed with multiple failsafe features to ensure that the autopilot can always be disabled, even in the event of electronic or mechanical failure.

  • Page 124: Vertical Autopilot Functionality

    Autopilot Operation NAV Mode The autopilot controls the aircraft to center the CDI needle on the HSI when the roll axis is engaged in navigation (NAV) mode. This assumes that a valid and active navigation source is selected on the HSI. Functionality Common to All Horizontal Modes Turns to new headings in HDG and TRK modes are governed by the roll axis mode chosen during servo installation (e.g.

  • Page 125: Control Wheel Steering Functionality

    Autopilot Operation the default climb VS when engaged). These default speeds are configured in the Pitch Axis Menu (IN FLIGHT SETUP MENU > ENTER FULL SCREEN SETUP MENU… > AUTOPILOT SETUP > PITCH AXIS). If the pitch axis mode is set to VS:BUG, the autopilot uses the current VS bug as its target rate of change when engaged.
  • Page 126 Autopilot Operation All of these items are described in more detail in the following sections. Note that the Top Bar is always on regardless of the screen layout and cannot be turned off. The visual indicators are contextual and are based on the installed autopilot axes (e.g., if there is no roll axis hardware, there will not be roll axis indicators) and are always present for installed axes.
  • Page 127 Autopilot Operation Heading Mode HDG is displayed in the roll axis information area when the roll axis is armed or engaged in heading mode. The white numerical value to the right of HDG - as shown in Figure 117 - is the target magnetic heading.
  • Page 128 Autopilot Operation Figure 123–Roll Axis Example: Navigation mode, GPS, disengaged Figure 124–Roll Axis Example: Navigation mode, GPS, engaged Some GPS units, such as the Garmin 430/430W, have the ability to output GPS Steering (GPSS) commands to the Autopilot. When in GPSS mode, the autopilot listens to direct bank angle requests as they are provided by the GPS.
  • Page 129 Autopilot Operation Roll Axis Top Bar Appearance Roll Axis Mode Heading State FUTURE DISENGAGED TARGET TARGET ENGAGED CURRENT FUTURE DISENGAGED TARGET TARGET ENGAGED CURRENT NAV RADIO DISENGAGED NAV RADIO ENGAGED NAV GPS DISENGAGED NAV GPS ENGAGED SLIP SLIP ERROR DISENGAGED Table 12–Top Bar Roll Axis Information Summary Pitch Axis Information Pitch axis mode, target, and status information is to the right of the AP text.
  • Page 130 Autopilot Operation An altitude value in blue denotes that the pitch axis is holding that altitude as shown in Figure 131. Note that the AP text and roll arrow are present indicating that the pitch axis is engaged. Figure 131–Pitch Axis Example: Altitude mode, engaged and holding 1500 VS Mode When the autopilot is changing altitude, the Top Bar denotes that the active mode is VS (blue text) and the target is the value of the altitude bug (white text).
  • Page 131 Autopilot Operation Pitch Slip You may see this during periods of turbulence or if the strength of the servo is not sufficient to actuate the control surface. If slipping occurs on the pitch servo, SkyView displays a slip warning as illustrated in Figure 133. Figure 133–Pitch Axis Slip Indicator Reference the SkyView System Installation Guide for more information regarding servo slippage.

  • Page 132: Ap Menu

    Autopilot Operation Figure 136–Control Wheel Steering Indicators Reference the Control Wheel Steering Section for more information. Airspeed Indicator SkyView uses the indicator shown in Figure 137 to denote that the aircraft airspeed is outside of the specified autopilot airspeed range as specified during installation. When SPD is displayed in the Top Bar the autopilot cannot be engaged.
  • Page 133 Autopilot Operation Figure 138–Press AP in the Main Menu to enter the Autopilot Menu The Autopilot Menu is illustrated in Figure 139. Figure 139–AP Menu All of the buttons in Figure 139 are explained in the following sections in the order they show up in the AP Menu from left to right.

  • Page 134: Autopilot Operation And Procedures

    Autopilot Operation ALT:[ON or OFF] Button 4 in the AP Menu has two purposes. It indicates the state of the pitch axis and is a way for the user to engage or disengage the pitch axis. Two visual indicators are used to denote the state of the pitch axis: text and the appearance of the button label.
  • Page 135 Autopilot Operation is immediately displayed in the Top Bar and the behavior of the autopilot changes to reflect the new mode. If you turn SYNC on while the roll axis is disengaged, the Top Bar heading or track target will display HOLD (in white text).
  • Page 136 Autopilot Operation 3. Press BACK to return to the Main Menu. Note that the pitch axis immediately engages in the selected mode after you press button 4 and its label indicates ON. The Top Bar also indicates this with green AP text and a green roll engaged arrow.
  • Page 137 Autopilot Operation  OFF is the default setting and disables Control Wheel Steering. Setting Control Wheel Steering to OFF does not disable the disengage or engage functions of the button.  HOLD HEADING/ALTITUDE configures the autopilot to hold the current heading and/or altitude when you release the button to end Control Wheel Steering mode.

  • Page 139: Messages And Alerts

    9. Messages and Alerts SkyView annunciates important notifications onscreen, in a dedicated Message Window, and optionally via audio (if connected and configured). This chapter describes SkyView alert behavior. Loss of Information SkyView notifies users with a large red X and a descriptive label if a major failure occurs that prevents the display of information.
  • Page 140 Messages and Alerts Alerts and messages are all categorized into one of three severity levels:  Message: Advisory message.  Caution: A condition which is abnormal but not critical in nature; may increase pilot workload.  Warning: A critical condition that should be addressed immediately; may affect safety of flight if not addressed.
  • Page 141 Messages and Alerts Engine warning alerts are only triggered when their respective sensors are configured as self-clearing or latching alarms. If a sensor’s alarm is configured as off, no alert will trigger, even if that sensor’s measurement enters a range defined as red.

  • Page 142: Prompts Requiring Interaction

    Messages and Alerts Alert and Message Acknowledgement New messages and alerts that have not been seen are considered unacknowledged and are highlighted. Acknowledged messages are not highlighted in the Message Window. Display the Message Window with the rightmost button to acknowledge an alert message. This action displays the current alerts and messages and causes the Message Notification Area to stop flashing.

  • Page 143: Messages, Alerts, And Audio Alert Details

    Messages and Alerts Messages, Alerts, and Audio Alert Details Message Displayed Notification Spoken Alert (if in Message Area Alert Description configured) Window (severity) “Warning” ADAHRS FAIL ADAHRS failure “ADAHRS Cross Check Displayed after an ADAHRS cross- Error” check error was announced in a ADAHRS CROSS CHK multi-ADAHRS systems, but the ERROR...
  • Page 144 Messages and Alerts Message Displayed Notification Spoken Alert (if in Message Area Alert Description configured) Window (severity) “Caution” Transponder failure. TRANSPONDER FAIL “Caution” BACKUP BATTERY IN System has switched to SkyView Backup Battery. “Caution” A SkyView Display has failed or is OTHER DISPLAY no longer communicating via OFFLINE...
  • Page 145 Messages and Alerts Message Displayed Notification Spoken Alert (if in Message Area Alert Description configured) Window (severity) “Message” SkyView components are not all SOFTWARE running the same software MISMATCH version “Message” OEM CONFIG OEM-customized displays are not MISMATCH in sync with each other “Message”...
  • Page 146 Messages and Alerts Message Displayed Notification Spoken Alert (if in Message Area Alert Description configured) Window (severity) “Approaching Altitude” / Altitude alerter notification that “Leaving Altitude” None the aircraft is approaching or leaving the bugged altitude “Overspeed” Indicated airspeed is exceeding None “Flaps Overspeed”...

  • Page 147: Appendix A: Skyview System Specifications

    10. Appendix A: SkyView System Specifications SV-D700 and SV-D1000 Quick Specifications 7.64” wide x 5.51” tall x 2.14” deep (194 x 140 x 55 mm) SV-D700 Mechanical 2 lb 6.1 oz (1.08 kg) not including SV-HARNESS-D37 10.32” wide x 7.06” tall x 2.14” deep (262 x 180 x 55 mm) SV-D1000 Mechanical 3 lb 0.7 oz (1.38 kg) not including SV-HARNESS-D37 Operating Temperature...

  • Page 148: Sv-Adahrs-20X Quick Specifications

    Appendix A: SkyView System Specifications SV-ADAHRS-20X Quick Specifications 4.71” wide x 1.22” tall x 2.61” deep (120 x 31 x 67 mm) Mechanical 8.2 oz (0.23 kg) Operating Temperature -22° to 140° F (-30° to +60° C) (1) 9-pin D-sub male connector Connections (1) 2-wire connector (3) 1/8”...

  • Page 149: Sv-Arinc-429 Quick Specifications

    Appendix A: SkyView System Specifications (1) 25-pin D-sub male connector Connections (1) Antenna connector (TNC) Mode S Transponder: Class 1 (SV-XPNDR-261) or Class 2 Transponder Capabilities (SV-XPNDR-262); ADS-B OUT via 1090ES; TIS Traffic Input. SV-ARINC-429 Quick Specifications 4.75” wide x 1.09” tall x 2.61” deep (120 x 27 x 67 mm) Mechanical 6 oz (0.17 kg) Operating Temperature...

  • Page 150: Sv-Gps-250 Quick Specifications

    Appendix A: SkyView System Specifications (2) Voltmeters (0 to 30 volts DC) (11) General Purpose (3) General Purpose Enhanced (2) Fuel Flow (1) Amps (differential) (1) Manifold Pressure Sensor Inputs (2) General Purpose Thermocouple (SV-EMS-220 only) (Left and Right) RPM (Left and Right) RPM (6) CHT (6) EGT...

  • Page 151: Autopilot Servo Quick Specifications

    Appendix A: SkyView System Specifications Connections (1) 3 pin power SkyView Display voltage above 12.25V: SkyView runs on aircraft power; SV-BAT-320 is charged. SkyView Display voltage above 10V, but below 12.25 V: Charge Behavior SkyView runs on aircraft power, but SV-BAT-320 is not charged (standby mode).

  • Page 153: Appendix B: License Information

    11. Appendix B: License Information GPL License Information SkyView's operating system contains copyrighted software that is licensed under GPL. A copy of that license is included in this document on the following page. You may obtain the complete Corresponding Source code from us for a period of three years after our last shipment of this product, by sending a check or money order for $15 to: Dynon Avionics Attn: GPL Source Code Offer...
  • Page 154 Appendix B: License Information It is not the purpose of this section to induce you to infringe any patents or other property right claims or to contest validity of any such claims; this section has the sole purpose of protecting the integrity of the free software distribution system, which is implemented by public license practices.

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