Attachment 2- Specifications (SAVE AND THEN OPEN).pdf

The document is a technical drawing and schematic for a Metal Bonded Course Trailing Edge Panel, designed for repair training purposes. The panel specifications include precise material requirements: bottom and top skins of .020" 2024-T3 aluminum (NSN 9535-00-167-2277), a .020" shim, and an aluminum honeycomb core material meeting MIL-C-7438G standards. The final requested panel dimensions are 30" x 7.5" x 2", with a 30-degree angle and +/- .125 tolerance on width and length.

The accompanying page details the trailing edge repair process, illustrating components such as overlay patch, film adhesive, core plug, edge doubler, internal doubler, and filler. The repair methodology involves multiple steps including core splice with foam adhesive and strategic application of film adhesive to bond various components. The document appears to be a technical training resource from AETC (Air Education and Training Command), likely used for maintenance and repair instruction in aerospace applications.