Klompder
Aerospace
- Jan 12, 2007
- 6
Hi there, I'm currently facing an out-of-round reamed up Cold Worked Flange Bush (FTI). The remaining wall thickness after further reaming up for the repair bearing will be about 0.055 inch (1.4mm), about half of the "design" thickness of min. 0.1 inch. My question is what the strength (static/fatigue) effect is on the lug and the flange bush. From my engineering judgement I would guess that the lug has already been cold worked when installing the original FTI bush and the compressive stresses at the lug hole will remain. The reduction in wall thickness of the FTI bush to 0.055 inch seems to me still acceptable.
However I cannot find any literature that substantiates this, except for some vague quotes on Internet.
Anybody out there with more experience on this?
However I cannot find any literature that substantiates this, except for some vague quotes on Internet.
Anybody out there with more experience on this?