Investigation results: the broken components were examined visually and microscopically.The rod is broken about 35 mm after the hexagon.We made a visual inspection of both fracture surfaces.There are clearly visible so called arrest lines, which are signs of a fatigue fracture on both parts.There are also little areas of secondary damages (metallic bright shining areas, caused by rubbing off the surfaces against another) visible.The fracture surface of both parts show no material or manufacturing abnormalities like blowholes or foreign material inclusions.Furthermore, especially the rod surface of part a shows material abrasion areas, which were caused due to loosening of the connection between the rod and the corresponding bracket.According to the information provided, the damage at part b is caused due to a drill in a first try to take out the rod.Unfortunately there are no information available about the patient and other external circumstances.Furthermore there are no x-ray figures available.Based on the information available as well as a result of our investigation, the root cause of the failure is most probably patient related/usage.Due to the fatigue fracture seen at analysis, and the visible material abrasions at the surface of the rod, it is apparent that the implant was exposed to micromovements.These micromovements, possibly coupled with high external load over an extended period of time, are likely to have lead to the breakage of the rod.No manufacturing relationship is established to the damage seen.The device quality and manufacturing history records have been checked for the available lot number and found to be according to our specification valid at the time of production.No similar incidents have been filed with products from this batch.
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