Originally Posted by
EFHF
This is incorrect. It was a design and tolerance fault of the actuator, not of the flight control system overall design. From the investigation report (section 3.2):
Further detail in section 3.1.2:
Also, the current pertinent AD for the servo actuators:
I was not saying that a ”control jam” was the reason for that accident 2005... But Thanx EFHF for completing my post with these facts...
