(b)(4).Returned product consisted of a ffr comet wire separated in two pieces.The guidewire shaft was examined for any damage or irregularities.It was noticed that the device was separated when returned.The proximal end of the shaft measured approximately 155.5cm.The distal end measured 29.5cm, which equaled 185cm.The total length of a complete comet wire is 185cm.Inspection of the remainder of the device, apart from the observed damage, revealed no other damage.The sensor port showed evidence of blood.Functional testing of the device could not be completed due to the separation of the shaft.Scanning electron microscopy (sem) imaging and fractography was performed to measure the beam widths on the 1st through 7th rows adjacent to the proximal and distal fracture ends.Sem images revealed that one beam was observed to be relatively small and irregularly shaped compared to the opposed beam.The fracture face on the small beam was obscured by smeared metal so the original fracture features could not be determined.On the large fractured beam the features present were partially obscured by smeared metal but visible microscopic features included striations oriented radially and ductile dimples.These features would suggest that the beam had been subjected to some combination of cyclic straining and overloading or a series of tensile forces resulting in overload.It was noticed that the beams were narrow on the device which contributed to the failure of the wire, therefore the investigation conclusion is manufacturing execution error as the manufacturing process was not executed as validated/as designed.(b)(4).
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