Product Details | AIRCRAFT STRUCTURAL PLATE

1560-01-102-0585 A flat or preformed item of metallic or nonmetallic material. It may vary in shape and its surface may be smooth and/or serrated. Its thickness is small in comparison to both its length and width. It is designed to be mounted upon a surface or between two surfaces. Its primary function is to strengthen, join, or separate aircraft structural parts. Excludes PLATE, MENDING; SHIM; and SPACER, PLATE.

Part Alternates: 53G8102145, 53G81021-45, 1560-01-102-0585, 01-102-0585, 1560011020585, 011020585

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-102-0585

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Technical Data | NSN 1560-01-102-0585

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 2024
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4-T3 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT MISSION DESIGN SERIES F-4
OVERALL LENGTH 2.380 INCHES NOMINAL
OVERALL WIDTH 2.380 INCHES NOMINAL
MATERIAL THICKNESS 0.040 INCHES NOMINAL
MANUFACTURERS CODE 76301
DESIGN CONTROL REFERENCE 53G81021-45

Restrictions/Controls & Freight Information | NSN 1560-01-102-0585

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