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***correction: please refer to d9/h3 - the product was returned for investigation, h6 method code.The reported event could be confirmed, since the received screw is broken as complained.The device inspection revealed the following: a single screw was returned for analysis.Upon initial inspection, the word stryker and the numbers 656328 and 1000393340 were observed to be peened into the head.The screw was then thoroughly examined under high intensity lighting at up to 50x magnification.A fracture surface is at the opposite end of the screw.The tip of the screw, including the last full thread, was fractured at the minor diameter completely.Sem analysis: high magnification inspection of the fracture surfaces was completed.The fracture appears to have occurred due to fatigue propagation.The fatigue propagation resulted in a shearing overload.There is an area where the shear failure pulls away from the as-machined area.Eds analysis indicates the alloy is consistent with the part drawing.Conclusion of the device inspection: stress and strain on the screw initiated a fracture in the minor diameter (root thread), feature between the 1st and 2nd major diameter threads from the tip of the screw.Cyclic loading propagated a fatigue-related fracture that resulted in a shear overload failure.The inside of the six-sided tooling insertion feature of the head did not exhibit evidence of over-torquing.No material non-conformances or manufacturing defects were found during the analysis.Medical affairs evaluation: "in the provided x-rays, at least in the lateral view of the images after screw arthrodesis, but also still after plate osteosynthesis, a joint gap can still be delineated at the tarsometatarsal, or the lisfranc, joint-line.This suggests together with the failure, that no union was achieved.This is also what the surgeon anticipated in the answer to the patient.The screws and the plates are not foreseen to overtake the load for a longer period of time.In the case of the plate no union occurred after six months.As the loads are pretty high at the operation site in these operation it is not too surprising that the material broke.If union would have occurred at a reasonable time this would not have happened.An insufficient preparation of the joint line may have contributed to the missing union." a review of the device history for the reported lot did not indicate any abnormalities.No corrective actions are required at this time.A review of the labeling did not indicate any abnormalities.No indications of material, manufacturing or design related problems were found during the investigation.Based on investigation, the root cause was attributed to a user related issue.The fatigue failure of the screw was caused by a non-union at the fracture site.An insufficient preparation of the joint line may have contributed to the missing union.If more information is provided, the case will be reassessed.
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