A joint between a first preform component and a second preform component that are constructed for ultimate use in a gas turbine engine includes a plurality of extended fibers which may be integral with the first preform component and be at least partially enveloped by the second preform component. A method for making the component provides a first preform component having extended fibers integral therewith, and supplying a second preform component. The method further includes inserting the extended fibers at least partially into the second preform component body.