Eddy Current Testing Device For Aircraft Fuselage Skin Crack Detection

摘要

The present invention relates to an eddy current inspection device for detecting edge cracks in a fastener hole located on a fuselage skin. The eddy current inspection device according to an embodiment of the present invention includes an inspection guide comprising: a stopping step which is provided at one side thereof, exposes an edge of the fastener hole and shields the rest of the fuselage skin; and a handle which is provided at the other side thereof, is connected to a guide unit, and brings the stopping step into contact with the fuselage skin.