Installation guide

iv SkyView System Installation Guide - Revision R
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. Dynon Avionics makes no claim as to the suitability of its
products in connection with FAR 91.205.
Dynon Avionics’ products incorporate a variety of precise, sensitive electronics. SkyView products do not contain any field/user-serviceable
parts. Units found to have been taken apart may not be eligible for repair under warranty. Additionally, once a Dynon Avionics unit is opened
up, it is not considered airworthy and must be serviced at the factory.
Dynon Avionics Returns and Warranty web page can be found at http://support.dynonavionics.com.
Revision History
Revision
Revision Date
Description
A
December 2009
Initial release
B
March 2010
Document number changed to 101320-001.
Minor style, grammar, and cross reference changes and corrections.
Updated guide to reflect SkyView firmware version 1.5 behavior and requirements.
Added servo installation information in various chapters.
Clarified SV-ADAHRS-200/201 installation orientation requirements.
Clarified SkyView display basic operation procedures. Most notably, added a screen
synchronization section.
SV-D700 / SV-D1000 Installation and Configuration Chapter Updates:
 Called out the use of a 5 amp breaker instead of a 7.5 amp breaker on page 4-7.
 Added important backup battery information on page 4-7.
 Consolidated serial device installation into this chapter.
 Added installation information for external dimming control and audio outputs.
 Expanded the Brightness Setup Section.
 Added a section regarding installed databases.
 Added a section reminding users outside of North America that they will need to
install an applicable terrain database file on page 4-14.
 Added a section regarding Aviation Data.
Cautioned against the use of ferrous pneumatic fittings on page 5-3.
SV-EMS-220 Installation and Configuration Chapter Updates:
 Clarified the theory behind and the use of EMS sensor definition and
configuration files in SkyView.
 Added a section regarding SV-EMS-220 wire harnesses.
 Added example engine sensor and transducer installations.
 Removed the requirement for a 200 ohm pull down resistor in the Rotax oil
pressure sensor installation.
 Removed the requirement for a 1.21k ohm pull up resistor in the Rotax CHT
sensor installation.
 The SV-EMS-220 is capable of measuring differential fuel flow. All information in
the guide has been updated to reflect this.
 Fixed the fuse call-out on in the Ammeter Shunt Section. Revision A called out a
7.5 amp fuse. This guide calls out a 1 amp fuse.
 Documented other minor sensor installation requirements corrections as
required.
Clarified SV-GPS-250 installation requirements.
Expanded Appendix C: Wiring and Electrical Connections.
C
May 2010
Document number changed to 101320-002.
Minor style changes.
Added information in applicable locations regarding the SV-NET-SERVO wiring kit.