Rev. 6
9-2
OVERVIEW
The Dynon D-180, Dynon SkyView or Garmin G3X EFIS (Electronic Flight
Information System) / EMS (Engine Monitoring System) replaces the traditional
mechanical flight information and engine monitoring instruments. For removal,
installation, inspection, or servicing of the avionics components refer to the
manufacturer user manuals.
The pitot and static systems provide static and dynamic pressure sources for
flight data calculations. The static system ports are located on each side of the tailcone.
A flexible plastic tube from the right static port crosses the tailcone to a plastic tee and
joins the flexible plastic tube from the left port. From the tee, a flexible plastic tube
routes to the floor, then forward within the center tunnel to the air data computer located
behind the instrument panel with the D-180 and in the aft fuselage with the Skyview and
G3X. The pitot port is an aluminum tube located at the tip of the spinner cone that
extends aft to an adapter block mounted to the engine. A flexible plastic tube continues
aft from the adapter block to the air data computer.
•
NOTE: This maintenance manual is intended to be used in conjunction with
the RV-12 Kit Assembly Instructions (KAI) when completing maintenance or
COMPONENTS
Garmin GTX 327 or GTX 23 ES or SV-
XPNDR-26X
See Garmin Manual or
Dynon manual
Garmin SL-40, GTR-200 or GTR-225
Emergency Locator Transmitter
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