xVue 1st-2

BendixKing xVue Touch

xVue Touch is a fast, simple and powerful flight display with superior craftsmanship for your experimental aircraft. xVue Touch can be installed as a primary flight display in a new experimental aircraft or as a replacement for outdated steam gauges in an existing aircraft. The 10.1” display provides the highest screen resolution in the industry. It can be used as full screen primary flight display or a split screen primary flight display and multifunction display.

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SUPERIOR CRAFTMANSHIP

Our industrial designers imagined and realized the xVue Touch delivering improved comfort & ease of use. With no cooling fan, xVue is quiet and has no moving parts to break. An ergonomic grip around the display makes it easy to access functions on screen even in turbulence. The separate controller gives you options to mount it anywhere on the panel you would like. The highest quality materials have been incorporated into the design by Honeywell experts, drawing from our programs like the F-16 avionics. Years of extensive in-lab and flight tests have been conducted to ensure superior quality, reliability & safety.

xVue 2nd
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AFFORDABLE

The low cost, high performance xVue Touch supplants all previous generations of flight displays for experimental aircraft. It comes standard with all flight indicators, the industry-leading SmartView™ synthetic vision, a vertical situation display that shows flight path over terrain, and ADS-B In weather and traffic. It includes free software upgrades coming in the near future to include engine instrument display and radio and autopilot control. xVue Touch integrates seamlessly with BendixKing KSN, Garmin GTN/GNS, and Avidyne IFD navigators, saving the cost of replacing a navigator.

FAST, SIMPLE, POWERFUL

Cutting edge touch technology provides high touch accuracy. The display and menu structure has been streamlined and simplified so that all critical functions can be reached in 2 touches or less. xVue comes with built-in Wi-Fi that allows you to upload databases within 4 minutes, and software updates in less than 10 minutes. The 10.1 inch high resolution screen provides 16.7 million colors with 1000 nits of luminescence and a 800:1 contrast ratio. The high quality coated glass provides 92% light transmissivity, and is anti-glare, anti-smudge, and anti-scratch. All of this provides you with a sharp, bright screen, easily readable in daylight.

 

Screen Displays

Optimized Menu StructureRD
Optimized Menu Structure
IFR Low DataRD
IFR Low Data
VFR Charts and SVSRD
VFR Charts and SVS
Full PFD ModeRD
Full PFD Mode
Base Map and TerrainRD
Base Map and Terrain
Dedicated Weather PageRD
Dedicated Weather Page
IFR High DataRD
IFR High Data
Airport Diagram On ChartsRD
Airport Diagram on Charts
Terrain and Vertical Situation DisplayRD
Terrain and Vertical Situation Display
Keyboard Access to ChartsRD
Keyboard Access to Charts
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System Overview

Primary Flight Display
The flight display unit includes 10.1-inch high-resolution (WUXGA) liquid crystal display (LCD) with infra-red (IR) Smart Touch technology that allows operation with a fi nger, pen, or glove. It also includes a light sensor that detects cockpit lighting conditions for automatic dimming of the display (dimming can also be controlled manually). For database uploads and maintenance functions, two options are available, a USB port or Wi-Fi connectivity.
Air Data Attitude Heading Reference System
The ADAHRS provides attitude, altitude, airspeed, air temperature, and heading information for the fl ight deck system. The air data parameters are calculated based on total pressure, static pressure, and air temperature. The attitude and heading reference system provides current airplane attitude based on inertial sensors and an aiding source (GPS or airspeed). The heading value is stabilized using the magnetometer measurement.
Control Panel
The control panel consists of three rotary push button knobs and one dual concentric push button knob. This unit provides an alternative to the touch control capability for entering barometric pressure, selected altitude, course and heading parameters. The control panel receives its power and LED backlight dimming input from the primary fl ight display.
Magnetometer
The sensing unit is located internally in the airplane wing or in the empennage, separated from all devices generating electromagnetic fields (motors, ferrous metal, wiring, magnets, antennas or anything else causing magnetic interference). The measurements of the Earth’s magnetic field are transmitted by a CAN Bus interface to the unit and data is used for long-term heading output stabilization
Outside Air Temperature (OAT) Probe
The temperature probe is a platinum 500 Ohm thermal sensor. Total air temperature is sensed by the independent probe and used to calculate the OAT and is required for the true airspeed calculation.
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