Post by
djwarner »
https://forums.nicoclub.com/djwarner-u152452.html
Thu Apr 29, 2010 8:20 am
The procedure is called "Stop Drilling".
Simply drilling a hole would suffice for a nonstructural part. A lot of parts such as fairings or access hole covers fit in this category. There's a lot of vibration in aircraft.
Many aircraft parts are custom made have no replace parts available. Replacement are either locally fabricated or the originals are repaired using standard procedures. ie, skin panels would be stop drilled and a doubler plate added. The standard of local repairs is to make the repaired part stronger than the original. Thus even if you replaced a stress cracked skin panel, you would use a heavier gauge sheet.
Unfortunately, for things that are dynamic, such as your fan blades, simple repairs would destroy the parts balance.
If you re-read my last post, I suggested stop drilling as a stop gap measure until the parts could be located and replaced.
Two things are assured. 1) If you do nothing, the crack will continue and a structural failure will result. 2) A stop drilling repair will do the least upset to balance, resonant frequencies, and remaining strength of the part.