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(b)(4).Supplemental emdr.Investigation findings: upon receipt the returned sample received a visual examination and functional check.The following markings were found on the device: sp95, a date code of h21, a 2-d udi barcode, snowden pencer, (b)(6), and usa.Upon visual inspection and functional check, the reported failure mode was confirmed.The bovie post had separated from its receptacle at the top of the handle bearing/knob.Normally, the bovie post fastened into the rotation knob bearing through the handle.The knob/bearing assembly was still intact and did not separate from the handle.Furthermore, it was observed that approximately 0.770 inch of the 0.865-inch bovie post had sheared off, leaving approximately 0.095-inch remaining of the post retained inside the knob/bearing assembly.This small remainder was holding the assembly together.Examination of the broken edges on both the internal and external ends indicated possible heavy forces and/or mechanical overstress causing the metal to shear off in a single directional manner.No other signs of damages, excessive forces cracking, or breaking was observed across the remainder of the sample.The bovie post was joined to the bearing using a uv luminescent thread locking adhesive.Evidence of this adhesive was found on the surfaces adjacent to the through hole in the handle for the bovie post.The practice of using thread-locking adhesive was to dip the threads of the male component into a pool of the thread locking adhesive, then fastened the two threaded components together.This act trapped the thread locking adhesive in the space between the internal threads of the bearing and the external threads of the bovie post.It was obvious that the thread locking adhesive was applied, due to the post not failing at the threads.Finally, due to the bovie post breaking along its metal distal end, it was tested for proper hardness specification.Per product specifications, the hardness range was noted to be within tolerances on the broken bovie post piece.Furthermore, the broken post was measured and found to be within product specifications.Upon further examinations the proximal end which had the splayed tips, displayed a possible sign of damage and/or heavy force application.The damage was characterized as a flattening/deformation of the metal surfaces at the very tip ends.The damage was on both sides of the split in the post, with both flats forming two inline planes, and suggested that as a strong force was acting to pull the bovie post in a single direction, which the concentrated force acted to flatten the tip while snapping most of the bovie post from the base that was secured to the bearing.Based on the gathered information it was clear that the sample¿s failure was causing by excessive forces placed on the bovie post end causing it to break off.Additionally, the sample was confirmed to have been manufactured correctly.
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