A Re-Examination of Failure Analysis and Root Cause Determination
A Re-Examination of Failure Analysis and Root Cause Determination
A Re-Examination of Failure Analysis and Root Cause Determination
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28Visual <strong>Examination</strong>The two as-received pins are shown in figure 1 where an arrow shows the location <strong>of</strong>failure. The failure occurred in a 1.230-inch-diameter cylindrical part <strong>of</strong> the pin whichwas corroded on the outer surface. One side <strong>of</strong> the fracture surface is shown in figure2, below.Convergent chevron patterns identified the fracture initiation site on the outside surface.The fracture initiation site is marked by a red arrow in figure 2. Most <strong>of</strong> the fracturesurface had been darkened by corrosion. A series <strong>of</strong> coarse low cycle fatigue crackarrest marks was identified at the ends <strong>of</strong> the two discolored crack-propagation fronts.The exterior surface <strong>of</strong> the 1.230 inch diameter cylindrical part <strong>of</strong> the pin containedcorrosion pits. Corrosion pitting was also visible at the fracture initiation site. Thefracture surface pr<strong>of</strong>ile is shown in figure 3.A circumferential ridge <strong>and</strong> depression were found in the cylindrical surface. A similarridge <strong>and</strong> depression were seen in the unbroken pin. By comparing the cylindrical parts<strong>of</strong> the two pins it was found that the fracture <strong>of</strong> the broken pin had initiated at thecircumferential depression.The part <strong>of</strong> the fracture surface containing the fracture initiation site was macroetchedfor 30 seconds in a hot aqueous 50 percent hydrochloric acid solution to remove thecorrosion products. The clean surface showed the fracture initiation site, as seen infigure 3.