Dynon Avionics EFIS-D10A Installation Guide - Manual (Page 96)

Appendix
7-24 EFIS-D10A Installation Guide
Appendix D: Dynon AOA/Pitot Installation and Calibration
Thank you for your purchase of Dynon’s AOA/Pitot Probe. This guide walks you through the
steps to install and calibrate both the heated and unheated versions of the AOA/Pitot Probe.
While the probe senses standard pitot pressure, allowing it to work with any standard airspee
indicator, its AOA functionality is designed specifically to work with Dynon’s EFIS series of
products. Do not expect it to work pro
d
perly with another AOA system.
nstall the probe correctly and perform the
specified calibration steps. W
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HEATING: PRINCIPLES OF OPERATION
The heated version of Dynon’s AOA/Pitot Probe utilizes a heating mechanism unlike any other
heated pitot on the market. The probe is heated by a high-quality nichrome heating element
whose temperature is accurately measured and regulated by the heater controller. This controller
– located in an enclosure which can be mounted in a wing or elsewhere – regulates the heat at the
tip of the probe to a constant temperature. There are several advantages to this, including: lower
power consumption, increased heating element lifespan, and a much cooler pitot on the ground
when de-icing is not necessary. This unique technique ensures that the pitot can be rapidly de-
iced when required, but does not needlessly waste electricity when not in icing conditions.
While the probe does not operate like a normal heated pitot, it will still get fairly hot in normal
ambient temperatures. When turned on, it will regulate its internal temperature to about 70°C to
80°C. To ensure that the heater is working, briefly touch the end of the pitot farthest from the
snout after 1 minute of operation and verify that it is warm.
FAILURE WARNING
Designed to meet the indication requirements of FAR 23.1326, the heated pitot controller has an
output that can trigger a warning light in the cockpit whenever the probe heater is turned off or is
not functioning properly. While not required for Experimental and LSA category aircraft, this
feature provides peace of mind, giving you instant feedback that your probe’s heater is working
as designed.
To ensure accuracy, it is very important that you i
e recommend that you read the entire guide before proceeding with
installation.
on s Heated AOA/Pitot Probe is nickel-plated. Do not polish the probe as this will cause t
sh to come off.
OA CALCULATION: PRINCIPLES OF OPERATION
on Avionics’ AOA/Pitot probe performs two functions: airspeed sensing and angle of attack
in . These functions require two pressure ports on the tip of the probe. The normal pitot
e front face of the probe and is designed to be insensitive to angle of attack.
second pressure port is located on an angled surface just under the pitot port and is designed
ry sensitive to AOA. The EFIS-D10A then uses the difference between these two
es to calculate the current angle of attack.