System and method for aircraft engine inspection

Abstract

A method for creating a computer-implemented data system, includes: providing a virtual 3D engine model of an engine including a plurality of components; providing component-specific data associated with said each of the plurality of components; and virtually linking the virtual 3D engine model to the component-specific data by creating virtual data markers in the virtual 3D engine model at a coordinate of each of the plurality of components, and associating each virtual data marker with the component-specific data of its corresponding one of the plurality of components. In this regard, the component specific data may include, for example, part number, name, inspection intervals, etc. The engine may be an aircraft engine, and may further be an aircraft engine casing. Further, in addition to the virtual 3D engine model, the method may include providing 2D images of the plurality components, and the step of virtually linking may further include linking the 2D images to the component specific data.

Dependencies are inferred from the claim text.