Special Features:

C/o: -118a cor (1)size 0.524 x 21 x 49, matl 5052 alum alloy per qq-a-250/8, core to be mil-c-7438, class 2, 5.73/166-20n.5052 mil.519 max.529 thk; -112a & 116a doubler(2)size .032x4x24 matl 7075-t6 alclad per qq-a-250/13; -110a& -114a doubler(2)size .032x5.4x44 matl 7075-t6 per qq-a-250/13; -108a inner skin(1)size .013x21x45, matl 7075-t6 alclad per qq-a-250/13; -106a outer skin(1) size .016x24x50, matl 7075-t6 alclad per qq-a-250/13

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.