Aluminum alloy edging, doublers and skin. Core is stm 28-102 type i.O/a dim. Inner skin is 0.016 by 48.00 by 56 in., outer skin is 0.016 by57.00 by 61.00 in.
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.
Classification: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)
NSN 2925-01-442-4171
NSN 6145-00-610-2283
NSN 6620-00-250-1980
NSN 5990-01-421-3325
NSN 6220-01-020-8018
NSN 6135-00-993-6823
NSN 5960-01-441-5340
NSN 5925-00-823-2909
NSN 7035-01-071-0197
NSN 6110-00-060-7704
NSN 6150-00-076-2751
NSN 5855-00-177-3529