Of course the OEM views data like this as proprietary data. Typically the panels in the interior Boeing aircraft are made with one inch thich nomex honeycomb core and 2 plies of fiberglass. According to sources I now have the shear strength of a NAS1836-3-11 is 300 lbs. If the panel is made...
I have a problem where I am trying to fasten a class divider curtain on a Boeing aircraft to the top of the overhead bins and extending across the aisle. I am proposing to use aluminum U-channels that will be fastened to the top of the overhead bins using potted inserts (p/n SL3378-3-500) and...
