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Critical information regarding product handling, repair, and airworthiness.
Identifies the module and its role as a redundant ADAHRS solution.
Details the sensors within the module for flight instrument generation.
Illustrates which sensors are used for different displayed instruments.
Explains how attitude is generated using sensors and airspeed.
Describes the module for engine monitoring and its measured parameters.
Details the GPS receiver module and its WAAS capability.
Explains the optional backup battery and its power capabilities.
Describes how the backup battery manages charging and power supply.
Mentions servos that enable SkyView to operate as an autopilot.
Describes the navigation mapping option and its licensing.
Details the TSO'd transponder module with ADS-B Out capability.
Describes the ADS-B receiver for traffic and weather information.
Details how joysticks and buttons are used for various functions.
Explains how to navigate SkyView menus and wizards using a structure.
Explains behavior during aircraft power loss when backup battery is connected.
Describes how to access the menu for flight-specific tools.
Details how to customize screen layouts and data distribution.
Displays important flight information and Synthetic Vision elements.
Lists key data shown on the PFD, including Synthetic Vision.
Details the altimeter display elements and their functions.
Describes the VSI display and how to use the vertical speed bug.
Explains the compass rose, gyro, and heading bug display.
Details the use and adjustment of airspeed, altitude, heading, and VS bugs.
Explains how to toggle bugs and their interaction with autopilot control.
Explains airspeed ranges, indicated airspeed, and trend indicator.
Visual representation of lateral acceleration for coordinated flight.
Explains how multiple ADAHRS modules provide redundancy and cross-checking.
Shows how to view ADAHRS side-by-side when a cross-check problem occurs.
Illustrates comparison screen and disabling one ADAHRS.
Indicates when only a single ADAHRS is available for use.
Steps to select and configure the ADAHRS source.
Explains ACTIVE, STANDBY, PRIMARY, and ALTERNATE ADAHRS status.
How to change ADAHRS to PRIMARY or DISABLE an ADAHRS.
Describes Synthetic Vision depictions of terrain, runways, and obstacles.
How fuel remaining, used, efficiency, and range are calculated.
Steps to obtain accurate fuel data and reset the fuel computer.
Adjusting fuel computer settings like quantity and total fuel.
How SkyView interfaces with the Vertical Power VP-X System.
Lists features available via the VP-X page for monitoring and control.
Depicts aircraft electrical system graphically, showing current draw and status.
Lists and describes the status of configured circuits in the VP-X system.
How to highlight, select, and control circuits using the joystick.
Options for resetting circuits or controlling flaps/trim.
Details the Class 1/2 Mode S transponder and ADS-B Out features.
Details ADS-B OUT capabilities and compliance with FAA mandates.
Explains the Moving Map requirements (GPS, terrain, aviation data).
Explains how SkyView uses GPS sources for the Moving Map display.
How traffic information is displayed on the Map Page.
Details SkyView's ability to receive traffic from various devices.
Explains that traffic info is informational and requires pilot vigilance.
How SV-ADSB-470 works with transponder for FIS-B traffic picture.
Explains symbols, relative altitude, and vector arrows for traffic targets.
Describes targets with high chance of near-aircraft encounter.
How to navigate directly to a waypoint.
How to navigate directly to an airport or navaid.
How a flight plan consists of waypoints and legs.
How to activate routing and view guidance on HSI and Map.
Displays active flight plan on map and in a separate window.
Shows active flight plan guidance on HSI and map.
How to enter the user waypoint creation tool from the Map Menu.
Editable fields for creating waypoints (Identifier, Name, Lat/Long, Icon).
How to display NEXRAD weather and TFRs on the map page.
How to display NEXRAD weather and TFRs on the map page.
Describes the module's ability to receive weather via ADS-B.
How NEXRAD radar data is processed and displayed.
How to toggle the map page between terrain and weather views.
Information about the ADS-B receiver's state and data age.
Failsafe features ensuring the autopilot can always be disabled.
Summary of the roll axis autopilot modes and their effects.
Holds or turns to match the magnetic heading bug.
Holds or turns to match the GPS ground track bug.
Governs turns in HDG, TRK, and turn rate modes, with bank angle limits.
Summary of pitch axis autopilot modes and their effects.
Holds altitude or climbs/descends to match the altitude bug target.
Displays HDG when roll axis is armed/engaged in heading mode.
Displays TRK when roll axis is armed/engaged in track mode.
Displays NAV data source (green/magenta) for roll axis in navigation mode.
How autopilot follows GPS steering commands for turns.
Displays ALT when pitch axis is armed/engaged in altitude mode.
Shows VS text and target altitude bug when changing altitude.
Denotes when aircraft airspeed is outside the specified autopilot range.
How to engage/disengage roll axis and set its mode.
Menu to set autopilot roll axis mode (HDG, TRK, NAV).
How to engage/disengage pitch axis and set its mode.
Menu to set autopilot pitch axis mode (VS:DFLT, VS:BUG).
Procedure to set pitch axis mode and toggle SYNC.
Procedure to engage or disengage the roll axis via the AP Menu.
Procedure to engage or disengage the pitch axis via the AP Menu.
Primary function of the button is to disengage the autopilot.
Using the button to engage autopilot if configured for HOLD TO ENGAGE.
How to steer using the control wheel while autopilot is engaged.
Explains the different modes for Control Wheel Steering.
Adjusting bugs when autopilot is engaged or disengaged.
General| Display Size | 10.4 inches |
|---|---|
| Display Type | LCD |
| Resolution | 1024 x 768 pixels |
| Operating Temperature | -20°C to +55°C |
| Supply Voltage | 10-30 VDC |
| Aspect Ratio | 4:3 |
| Input Voltage | 10 to 30 VDC |
| Certifications | TSO-C113, TSO-C115, TSO-C146, TSO-C145 |
