Section G5 - Pitot, Static, and AOA System Leak Check.
The flight controls through all extents were checked and there was no interference between the tubing, wires or any flight controls nor flaperon linkage.
Both wings were installed and both spar pins were engaged.
The pitot tubing was disconnected from the ADAHRS pitot fitting and the AOA tubing was connected on the ADAHRS pitot fitting.
When pushing air into the AOA port with the syringe and when the stopwatch indicated 130 kts the airspeed was 125 kits after one minute.
The pitot and AOA tubes were reattached to the proper ADAHRS port fittings.
The plunger was pushed-in until 130 kts indicates then stop pushing-in. When EFIS indicated 120 kts it started timing. The airspeed was 119 kts after one minute.
