Model: 206-032-103-11
Aircraft Structural PanelSpecial Features:
Skin forward 46.500 in. Lg; 9.900 in. W, 0.064 in. Thk, core 45.000 in.Lg, 8.600 in. W, 0.500 in. Thk, glass fabric skin aft, 48.000 in. Lg, 11.000 in. W
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.
Part 206-032-103-11 NSN 1560-01-005-4816
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsFreight Classification
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Schedule B and Export
- Schedule B: 8803909060
- SITC: 79297
- End Use: Parts for military-type goods
- NAICS: 336419
- USDA: 1
Freight Class: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)
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