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 5998-01-422-1516
NSN 6105-01-157-7011
NSN 5920-00-722-4894
NSN 5925-00-905-5135
NSN 5935-01-536-2409
NSN 5990-01-631-5537
NSN 6150-01-267-5057
NSN 5965-01-538-4947
NSN 4140-00-205-6491
NSN 5905-00-713-2500
NSN 6150-01-370-5239
NSN 5895-00-278-5194