Crew latrine left panel assembly (NSN 1680-01-111-4817)
End Application
C-141a/b aircraft
General Description
Panel fabricated from fiberglass cloth, per mil-c-9084, type 8, and resin, per mil-r-9300, fabrication process to include a 0.19-0.022 in. Gel coat, color white, prior to layup, matte weaving design feature incorporated into mold, to be equivalent to weave side of laminated cloth mil-c-43006, assembly consists of 2 wire mesh screens, 10 retainingwashers, 10 stud assemblies, adhesive per mil-a-46146, 1 pane, 1 grill, and 1 panel, panel is 30.88 in. Wide and 50.71 in. Long, has 10 0.281 in. Max and 0.283in. Min diameter holes for stud assemblies, has centrally located hole, 2.50 in. Min diameter and 2.56 in. Max dia
