Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-486-8201 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 Alternates: 160D71215118, 160D712151-18, 1560-01-486-8201, 01-486-8201, 1560014868201, 014868201

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-486-8201

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Technical Data | NSN 1560-01-486-8201

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 5052
MATERIAL DOCUMENT AND CLASSIFICATION MIL-C-7438 MIL SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION UPPER SPEED BRAKE
AIRCRAFT MISSION DESIGN SERIES A-10
SPECIAL FEATURES HONEYCOMB CORE; GRADE B, CLASS2; NON-PERFORATED; FOIL THK. RANGE FROM .001 TO .0015; PART OF -4 PANEL ASSEMBLY
MANUFACTURERS CODE 26512
DESIGN CONTROL REFERENCE 160D712151-18

Restrictions/Controls & Freight Information | NSN 1560-01-486-8201

Category Code Description
Hazardous Material Indicator CodePThere is no information in the HMIS; however, the NSN is in an FSC in Table II of Federal Standard 313 and an MSDS may be required by the user. The requirement for an MSDS is dependent on a hazard determination of the supplier or the intended end use of the product
Category Code Description
No Freight Information