NAS1836

Genuine Aircraft Hardware Co. All original Text, Tables, and Drawings are Copyright 1994-2010 reproduction by permission only. NAS1832 thru NAS1836, Inserts For Composite or Honeycomb Panel Fastening These NAS1832 thru NAS1836, Potted in Inserts are the standard for fastening in composite or honeycomb panels. The panel is first prepared by drilling or routing a hole or holes in the panel as necessary, depending on whether or not the insert is a through hole insert or a closed end insert. After preparing the hole and securing the insert in place with the NAS1837 adhesive tab (comes with inserts), then the adhesive or epoxy as recommended by the panel or aircraft manufacturer is forced in through one of the potting holes until it is forced out of the other hole or slot which acts as a vent hole. After the proper curing time and procedures are followed, remove the tab, clean up as required and then fasten items to the newly installed insert as appropriate. Please use Part Number Diagram, Tables and pictures, to select inserts When selecting length on all except NAS1833 and NAS1834, allow .040”min between insert and back skin Continued.......... 174 Documents in this book for REFERENCE ONLY, not intended for design. Not guaranteed for accuracy. All original Text, Tables, and Drawings are Copyright 1994-2010 reproduction by permission only. Genuine Aircraft Hardware Co. NAS1832 thru NAS1836, Inserts For Composite or Honeycomb Panel Fastening....Continued Note: Do not sp...