Installation Guide Instruction Manual
 Appendix 
FlightDEK-D180 Installation Guide    9-7 
Appendix B: Dynon EFIS OAT Probe Installation and Usage 
Note that this section only applies to the OAT with 3 wires (colored red, yellow, and blue), for 
connection to the EDC-D10A. If you have the 2-wire EMS OAT connected to the DB37 
connector, you do not need to also have the EFIS OAT connected. See the Outside Air 
Temperature Sensor installation section on page 3-13 for information on installing the 2-wire 
OAT. Ensur
e that no EMS GP input is configured as an OAT. Only one type of OAT can be 
connected to the system. 
The following instructions provide information on installing and using the FlightDEK-D180 
OAT probe. Keep in mind that this probe is designed specifically to work with Dynon products. 
Do not expect it to work properly with another OAT or TAS/Density Altitude system. Your 
FlightDEK-D180 can receive its OAT value from the 2-wire EMS OAT; it is not necessary to 
use both OATs. 
TOOLS AND MATERIALS REQUIRED 
  Dynon Avionics OAT probe/cable with nylon nut and washer. 
  Drill with 3/8” bit 
  Dynon Avionics EDC-D10A remote compass module. 
  2 machined D-sub pins 
  D-sub pin crimp tool 
  Loctite 
INSTALLATION 
Mount Location 
It is important that the OAT probe be mounted somewhere on the skin of the aircraft where it 
will not be affected by heat sources (sun, engine, aircraft interior, etc). The ideal location would 
receive no heat from the aircraft engine or any other source in the aircraft body. While this may 
be impractical, it is a good idea to mount the probe as far away from heat sources as possible. On 
the RV series, common locations include the wingtip and under the horizontal stabilizer. Avoid 
these three locations: 
  Engine exhaust paths 
  The engine itself 
  Where the sensor will have direct sunlight 
  Where the backside is exposed to a heated cabin 
Mounting Instructions 
After the mounting location has been determined, drill a 3/8” hole in the skin at the desired 
location. Uncoil the cable attached to the OAT probe. Remove the nylon nut from the cable. 
From outside the skin of the aircraft, insert the cable first and then the threaded end of the OAT 
probe. From within the skin of the aircraft, gently pull the cable until the threaded end of the 
OAT probe pokes through the hole. Thread the nylon nut down the cable and up to the threaded 










