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Dynon Avionics SkyView Classic - Page 111

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SV-ADAHRS-200/201 Installation and Configuration
SkyView System Installation Guide - Revision AA 5-7
Mounting requirements for the SV-ADAHRS-200/201:
Must be mounted within one degree of parallel to all three aircraft axes,
The pneumatic fittings must face toward the front of the aircraft,
The mounting tabs must be towards the bottom of the aircraft, with the label towards
the top of the aircraft.
Figure 47 ADAHRS Installation Orientation above shows the correct orientation of the
ADAHRS as it would appear if you were above the aircraft, looking down at it. The module will
not operate properly if it is rotated or inverted in any other orientation.
There are no module-to-module proximity requirements when installing multiple
SV-ADAHRS-200/201 modules in an aircraft. For example, an SV-ADAHRS-201 may
be installed on top of a SV-ADAHRS-200 (most easily accomplished using the
Dynon Avionics Dual ADAHRS Mounting Kit (P/N 102532-000). Other installation
location requirements still apply.
The ADAHRS installation location should also adhere to the following requirements:
Avoid locations that are lower than the lowest point in the AOA/Pitot/Static system to
reduce the chance of allowing moisture to enter the module.
Avoid locations that are subject to severe vibration.
Avoid locations that are subject to rapid changes in temperature.
Avoid locations that are subject to extreme humidity.
Leave ample working room for electrical and pneumatic connections.
Table 15 SV-ADAHRS-200/201 Inputs and Sensors describes which sensors and inputs are
used to generate displayed instruments.
Displayed
Instrument
GPS
Pitot
Static
AOA
Internal
Magnet-
ometer
Remote
Magnet-
ometer
Rate
Sensors
Accel-
erometer
OAT
Airspeed
Altitude
Angle of Attack
(AOA)
Attitude
* GPS used only during
Pitot failure
*
Ball
Density
Altitude (DA)
Flight Path
Marker (Internal
Magnetometer)
Flight Path
Marker (External
Magnetometer)

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