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Originally Posted by sportpilot
The way we learned to use castle nuts is tighten them to their snug fit, then crank in just enough more to make the cotter pin hole line up to the next slot..
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Well, something was lost in the translation then. This is why we have minimum and maximum torque values on nuts. If they were all self locking, there would just be 1 standard torque for each size and thread type.
The correct way, in general, for castellated nuts is to torque to the minimum specified torque value and see if the castellations line up with the hole. If not, you may turn it in the direction of tightening until you line up the holes or reach the maximum torque value, which ever occurs first. This is an absolute maximum value for the hardware. If the holes can't be aligned someplace between the minimum and maximum torque values, remove the nut, re-clock the threads or add a thin washer if the stack up can accept it, then repeat the process until you are successful.
As to the control bolts, if the part must move, then mobility takes precedence over the standard torque values and you torque it only enough to not impede the movement. Generally in more documented aircraft, the publications would specify a special torque for those type of installations. This would be one that ensures the assembly stays together while the parts move as required.
Thought it necessary to correct the record because torquing correctly is important.
Jekyll