Product Details | AIRCRAFT STRUCTURAL PANEL

1560-01-116-0451 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: 4W14181103B, 4W14181-103B, 1560-01-116-0451, 01-116-0451, 1560011160451, 011160451

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-116-0451

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Technical Data | NSN 1560-01-116-0451

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7075
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT LOCATION UPPER WING PANEL ASSEMBLY
AIRCRAFT STATION NUMBER FS1347 TO 1383
AIRCRAFT MISSION DESIGN SERIES C-5A
MANUFACTURERS CODE 98897
DESIGN CONTROL REFERENCE 4W14181-103B

Restrictions/Controls & Freight Information | NSN 1560-01-116-0451

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