Product Details | AIRCRAFT STRUCTURAL PLATE

1560-01-168-5209 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: 1560-01-168-5209, 01-168-5209, 1560011685209, 011685209

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-168-5209

Cross Reference | NSN 1560-01-168-5209

Part Number Cage Code Manufacturer
16B5141-83 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS
16B5141-93 81755 LOCKHEED MARTIN CORPORATION DBA LOCKHEED MARTIN AERONAUTICS

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Technical Data | NSN 1560-01-168-5209

Characteristic Specifications
MATERIAL ALUMINUM ALLOY
MATERIAL DOCUMENT AND CLASSIFICATION QQ-A-250/4 T62 FED SPEC SINGLE MATERIAL RESPONSE
AIRCRAFT STATION NUMBER FS279 TO FS 341
AIRCRAFT MISSION DESIGN SERIES F-16
OVERALL LENGTH 63.000 INCHES NOMINAL
OVERALL WIDTH 26.000 INCHES NOMINAL
MATERIAL THICKNESS 0.100 INCHES NOMINAL
SPECIAL FEATURES FINISH A708; SAME AS AND TO REPLACE -55 EXCEPT ADD HOLE AND MODIFY ETCH POCKET
MANUFACTURERS CODE 81755
DESIGN CONTROL REFERENCE 16B5141-83

Restrictions/Controls & Freight Information | NSN 1560-01-168-5209

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