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This report is being submitted as follow-up no.1 to provide a correction to section d4, to provide the device return date in section d9, to update section h3, and to provide the completed investigation results.The returned samples were a guidewire main body and a fragment.Visual inspection: the main body and the fragment were confirmed to measure approximately 2557 mm and 43 mm respectively, which is the total length was approximately 2600 mm.Confirmation of the involved product code: the product code pointed out in this ppr was rf/ga35183a, whose specified length is 1800mm.Meanwhile, as the total length of the actual sample was found not 1800mm as shown in the investigation result 2, we requested tmc to reconfirm the product code.Nevertheless, we received the additional information from tmc that the involved product code was gr3508 (rf/ga35183a); therefore, further investigation was performed considering that the involved product code was unknown.Magnifying inspection found that: the outer layer of the fracture end of the fragment had been stretched and had a shape that looked like it had been torn off.The outer layer of the fracture end of the body also had a shape that looked like it had been torn off.The core wire was exposed at the fracture end of the main body.There were no external anomalies such as scratches on other parts.Electron microscopic inspection found that the outer layer of both portions had been wrinkled near the fracture end.The outer diameter of the undamaged part was confirmed to be within our control standard.No anomaly was observed.The outer layer of the actual sample was removed, and the fractured part of the core wire was subjected to an electron microscopic inspection.There was no taper-shaped deformity on the fracture end of either portions and both were flat.Radial pattern was observed on the fracture surface of both portions.Past simulation test: 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 a continuous one-way torque load is applied while the guidewire is curved the fracture end of core wire becomes flat and does not deform in taper shape.Radial pattern is observed on the fracture surface.From this, the state of the actual sample was considered to be similar to this state.When a continuous one-way torque load is applied while the guidewire is straight, spiral pattern starting from the center is observed on the fracture surface of core wire.This state was considered different from that of the actual sample.When a bending load is applied repeatedly, the fracture end of core wire becomes flat and does not deform in taper shape.A dimple pattern (a hole-like pattern) is observed on the fracture surface.This state was considered different from that of the actual sample.When a pulling load is applied, the fracture end of core wire deforms in taper shape.This state was considered different from that of the actual sample.When a pulling load is applied to a looped guidewire, the fracture end of the core wire becomes curved and deforms in taper shape.Roughness is observed on the fracture surface.This state was considered different from that of the actual sample.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 wire over the entire length.The outer diameter of wire is controlled to assure the strength of wire.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 wire), 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 in a detour, so the flow will change compared to when 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.In this case, it was inferred that the actual sample was subjected to continuous torque load while it was curved and, as a result, the core wire was fractured due to metal fatigue at approximately 43 mm from the distal end.After that, it was inferred that the outer layer was torn off due to pulling load during withdrawal, which resulted in the complete separation of the actual sample into two portions.In addition, since the product code of the actual sample was unknown, it was not possible to clarify whether the aggregated length of the actual sample and the fragment was equivalent to that of a normal product.Ifu states: "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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