Dynon Avionics EFIS-D10A Installation Guide - Manual (Page 9)

2. WIRING OVERVIEW
Please follow these instructions explicitly as improper wiring can result in permanent damage to
your instrument and/or the accompanying sensors.
All electrical power and EFIS-specific lines interface with the EFIS-D10A via the female 25-pin
D-sub connector on the back of the instrument. Ensure that the unit powers on and that all
indicators display expected values before completing the final physical assembly.
Recommended Wiring Practices
For all electrical connections, use correct wiring techniques, taking care to properly
insulate any exposed wire. A short circuit between any of the wires may cause damage to
the EFIS-D10A and/or your aircraft. Make all connections to your harness before
plugging it into any of the components of the system. Do not make connections while
power is applied at any point in the system.
Dynon Avionics sells a wiring harness for all connections to the EFIS-D10A. The harness is
made up of 22 AWG wire and meet Mil Standard MIL-W-22759/16 (Tefzel insulation). If you
have opted not to purchase this harness, please refer to the provided wiring diagrams for
construction information. We recommend that all wire you use also meets Mil Standard MIL-W-
22759/16; all wire supplied by Dynon Avionics (with the exception of thermocouple wire, which
uses FEP insulation) meets this specification.
When using any pre-manufactured harness, verify that each pin has continuity with the expected
wire on the wiring diagram. This test can be easily done with a multimeter. When verifying
harnesses, use the wiring charts and diagrams in this guide as your ultimate authority on pin
function (for any harness) and wire color (for harnesses purchased from Dynon Avionics).
Route all wiring such that there are no spots where it could chafe or break. Use appropriate strain
relief at all junctions between wires and connectors. We recommend that you secure all wires at
regular intervals along wiring runs to accommodate vibration effects.
All connections on the EFIS female 25-pin harness are described in the Instrument Installation
section on page 3-1.
Power Requirements
22 AWG wire is normally sufficient for the power supply and ground lines, but we recommend
that you consult a wire sizing chart and determine the size required for the wire routing in your
particular aircraft. Ensure that the power lines include a circuit breaker or an appropriately sized
fuse for the wire you select. Power is fed to the EFIS-D10A via pins in the female D-25
connector as shown on the 25-Pin Female EFIS Harness diagram on page 2-2.
The EFIS-D10A system-wide power requirement is 8 watts typical and 13 watts maximum. On
a 12-volt system, this translates to about 1 amp of maximum current draw. On a 24-volt system,
this translates to about 0.5 amp maximum current draw. Normally, a 2-amp circuit breaker or
fuse is sufficient.
EFIS-D10A Installation Guide 2-1