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This report is being sent as follow-up no.1 to provide the device return date in section d9, to update section h3, and to provide the completed investigation results.The actual device has been returned for evaluation.1.Actual samples upon receipt were a fragment and a guidewire main body.2.Visual inspection of the actual sample - length of the fragment: approximately 23 mm - length of the main body: approximately 2577 mm - total length: approximately 2600 mm (normal product: 2600 mm) - the fragment had been kinked at two points.3.Magnifying inspection of the fragment - the outer layer surface near the distal end was rough.- there were wrinkles in the surface of the kinked parts.- there were lengthwise abrasions near the fracture.From this, it was thought that some hard object had come into contact with the distal end and the vicinity of the fractured part of the actual sample.4.Magnifying inspection of the guidewire main body - there was no external anomaly such as a scratch in the part other than the fracture.5.Shape of fracture - each fracture end of outer layer matched with each other in terms of shape.From the investigation results 2 and 5, it was considered that there were no major defects in the actual sample.6.Electron microscopic inspection of the fracture - both fracture ends were in a shape that looked like they had been torn off.- the outer layers of both fracture ends were wrinkled.7.Dimensional inspection - the outer diameter (undamaged area near the fracture) was within the factory's specifications.No anomaly was found.8.The outer layer was removed, and the fractured part of core wire was subjected to an electron microscopic inspection.- for both fractured parts, the side of core wire was tapered and twisted.- spiral pattern starting from the center was observed on both fracture surfaces of core wire - dimple pattern was observed on the center of both fracture surfaces of core wire.9.Past simulation tests the following simulation tests were conducted in the past based on our experience and knowledge on the guidewire fracture.It is recognized that there is regularity in the state of fractured core wire depending on the mechanism leading to fracture as follows.- when continuous one-way torque force is applied while the guidewire is held straight, - the fracture end of core wire becomes tapered.Dimple pattern on the center and spiral pattern starting from the center are observed on the fracture surface.From this, this state was considered similar to the state of the actual sample.However, the degree of taper of the actual sample was larger than that of the simulation test sample, in addition, the actual sample had been twisted.This was thought that the torque and tensile force having been applied to the actual sample was larger than that applied to the simulation test sample.- when a continuous one-way torque force is applied while the guidewire is curved, - the fracture end of core wire becomes flat, no tapering is observed on the side, and radial pattern is generated on the fracture surface.The state of the actual sample was considered different from this state.- when tensile force was applied while the distal end is trapped, - the side of fracture end becomes tapered.Roughness is observed on the fracture surface.The state of the actual sample was considered different from this state.- when repetitive bending force is applied while the distal end is trapped, - the fracture end of core wire becomes flat, and no tapering is observed on the side, and a dimple pattern (hole-like pattern) is observed on the fracture surface.The state of the actual sample was considered different from this state.- when tensile force is applied while the distal end is trapped and the shaft is looped, - the side of fracture end becomes curved and tapered, and roughness is observed on the fracture surface.The state of the actual sample was considered different from this state.(cause of occurrence) from the investigation results, as one of possibilities in this case, it was presumed that the core wire was fractured due to metal fatigue because continuous torque force and tensile force were applied to the actual sample in the same direction while the actual sample was trapped by some kind of hard object (e.G., calcification lesion).The actual sample in the above state was exposed to further tensile and torque force, which resulted in the tear in the outer layer leading to complete fracture.As for the kinked parts, it was inferred that it was caused by excessive bending force having been applied during the procedure, however, the timing of occurrence could not be clarified.(countermeasure) ashitaka factory assures the quality of this product by performing following inspections and control.- through eddy current flaw detection*, it is confirmed that there is no crack in the core over the entire length.- the outer diameter of core is controlled to assure the strength of core.- before the packaging process, 100% visual inspection is performed to confirm that there is no anomaly such as a kink or scratch.(*eddy current flaw detection: when an alternating current is passed through a coil, a magnetic field is generated in the direction perpendicular to the current.When the coil is brought close to the conductor (core), an eddy current is generated on the surface of the conductor.If any anomaly including a crack is generated in the conductor, the eddy current avoids the crack and flows around the conductor, so that the flow changes as compared with the case where there is no crack.The method of detecting changes in the flow of eddy currents and searching for cracks is called eddy current flaw detection.) ifu of this product includes the following warning.[warnings] if any resistance is felt or if the tip's behavior and/or location seems improper, stop manipulating the glidewire and/or the catheter and determine the cause by fluoroscopy.Failure to exercise proper caution may result in bending, kinking, separation of the guide wire's tip, damage to the catheter, or damage to the vessel.Terumo medical products (tmp) (importer) registration no.2243441 is submitting this report on behalf of ashitaka factory of terumo corporation (manufacturer) registration no.9681834.
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