Product Details | AIRCRAFT STRUCTURAL PLATE

1560-01-046-1668 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: 16B18339, 16B1833-9, 1560-01-046-1668, 01-046-1668, 1560010461668, 010461668

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-046-1668

Cross Reference | NSN 1560-01-046-1668

Part Number Cage Code Manufacturer
16B1833-11 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS
16B1833-11S 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS

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Technical Data | NSN 1560-01-046-1668

Characteristic Specifications
MATERIAL ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4 T62 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT MISSION DESIGN SERIES F-16A/B
OVERALL LENGTH 23.000 INCHES NOMINAL
OVERALL WIDTH 3.000 INCHES NOMINAL
MATERIAL THICKNESS 0.312 INCHES NOMINAL
SPECIAL FEATURES SUPERSEDED PN 16B1833-11 OW PER ECN 54625; NHA 16B1931-6; EFF ON 0004-0034
MANUFACTURERS CODE 81755
DESIGN CONTROL REFERENCE 16B1833-9

Restrictions/Controls & Freight Information | NSN 1560-01-046-1668

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