An insert, a floating nut and methods for use thereof in a panel of an aircraft are presented. Specifically, an insert includes a housing defining a cavity. An aperture is further defined in a first end of the housing and a semi-spherical portion is defined at a second end of the housing. A pair of vent openings are also defined on opposing sides of the first end of the housing.

Processes for fabricating a partially stabilized honeycomb core is disclosed where a stabilizing layer of an adhesive film is aligned with and adhered to only one exterior surface of a honeycomb sheet. The opposed exterior surface thereby remains uncovered. A preform of the partially stabilized honeycomb core may be subjected to ambient atmospheric pressure cure conditions at an elevated temperature sufficient to adhere the stabilizing layer to the one exterior surface of the honeycomb sheet and thereby provide a partially stabilized honeycomb core that is partially stabilized against compressive forces exerted in widthwise and lengthwise directions thereof yet allows bending of the partially stabilized honeycomb core about axes in the widthwise and lengthwise directions.

A tool presses a joining element against a first object into a first opening of the first object while mechanical vibration energy is coupled into the first object and the joining element. Vibration energy and pressing force make the thermoplastic material of the distal portion of the joining element flowable and interpenetrates structures of the first object to yield, after re-solidification, an anchoring of the distal portion of the joining element in the first object. The second object is placed so that a proximal portion of the joining element is inserted into a second opening, and the first and second objects are pressed against each other while mechanical vibration energy is coupled into one of the first and second objects, until thermoplastic material of the joining element proximal portion is made flowable and interpenetrates structures of the second object to yield, after re-solidification, an anchoring in the second object.

A formation method is provided during which a thermoplastic film is arranged on a fiber-reinforced thermoplastic skin. The thermoplastic film is configured from or otherwise includes thermoplastic material. A heating device is moved to a location along the thermoplastic film, where the thermoplastic film is disposed between the fiber-reinforced thermoplastic skin and the heating device. The thermoplastic film is heated with the heating device to melt the thermoplastic film and provide a melted thermoplastic film. The heating device is moved away from the melted thermoplastic film. A honeycomb core is pressed against the melted thermoplastic film to bond the honeycomb core to the fiber-reinforced thermoplastic skin with the thermoplastic material.