Special Features:

Skin panel assembly, rh; u/o shipboard compatible mh-53j; c/o -50 sandwich assembly (1) material: glass 120, kevlar 285, film adhesive, tedlar and phenolic honeycomb core; -90 stiffener assembly rh (1) material 2024-t62 aluminum alloy qq-a-250/5; -91 insert (8) material: epoxy microbaloon or phenolic resin; 8834600-25 spacer (16) and nas1919b04s03 blind rivet (8)

Properties:

A preformed item of various shapes, and contours, which may have a sandwich or honeycomb core bonded to a metallic or nonmetallic facing material. it is used to enclose integral portions of the fuselage or to form partitions or sections within a wing, empennage, fuselage, nacelle or crew compartment. it may have mounting provisions such as predrilled holes to facilitate installation, but will have no items attached to it except bracket (s) or other securing devices to accommodate its own mounting or support. it may be mounted by means of fasteners, bonding or welding. excludes panel, interior lining, aircraft; cover access; cover, access, aircraft; floor (1), aircraft; core material, cellular, structural.