Dynon Avionics Pitot/Static Test - Manual

101722-000 Rev B
April 27, 2012
Dynon Avionics Pitot/Static Test White Paper
Dynon Pitot/Static Test Background
Dynon ADAHRS/EFIS units use airspeed (or GPS ground speed when airspeed is unavailable) in the
calculation of attitude. The internal rate sensors that are used to determine attitude are monitored and
calibrated in-flight by using feedback from the accelerometers and from airspeed to achieve a highly
accurate attitude solution.
When a pitot or static test is performed, the ADAHRS/EFIS is being exposed to dynamics that are
impossible to achieve in a real aircraft flight environment – namely, there are large airspeed changes
without the accompanying accelerations and rotations. This false condition will cause a well-calibrated
unit to incorrectly adjust its calibration. Furthermore, when a unit is in a test situation a change in
applied pitot or static pressure will cause the attitude to pitch up or down. This is expected.
Performing the Dynon prescribed pitot and static test procedure to a Dynon ADAHRS or EFIS will prevent
problems with the unit’s performance in flight.
Dynon Pitot / Static Test Instructions
Basic Principles

Ensure unit is warmed up during each test reading.

Unit should be powered off when changing pressures.

Keep aircraft still (do not move) when pressure is applied.
Steps
1. The aircraft itself should be temperature stable. For example, if the aircraft is moved from
outside in the sun to a hangar for testing, tests should not be started until the airplane has
stabilized at the hangar temperature.
2. Turn EFIS on and let it warm up until the altitude reading is stabilized. This period should be at
least 5 minutes, but may take longer depending on environmental conditions.
3. Turn EFIS off.
4. While the EFIS is off, apply the pressure required by your test to pitot and/or static port via your
test equipment.
5. Turn on EFIS (external or internal battery power is acceptable). Keep aircraft still while EFIS is
powered on. Do not adjust the pitot or static pressures being applied to the EFIS/ADAHRS while
it is powered on.
6. Verify airspeed and/or altitude reading.
7. Turn EFIS off (using button 1 is a good option for this operation ) .
8. Repeat steps 4-7 for each required pressure point in the test.
*See user manual for instructions on calibrating the airspeed zero pressure setting or adjusting the altitude offset