Product Details | AIRCRAFT STRUCTURAL PLATE

1560-01-521-8968 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: 1560-01-521-8968, 01-521-8968, 1560015218968, 015218968

Aircraft and Airframe Structural Components | Airframe Structural Components

Supply Group (FSG) NSN Assign. NIIN
15 01-521-8968

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Technical Data | NSN 1560-01-521-8968

Characteristic Specifications
MATERIAL ALUMINUM ALLOY 7475
MATERIAL DOCUMENT AND CLASSIFICATION FMS 3004 MFR REF ALL MATERIAL RESPONSES
AIRCRAFT LOCATION WING SPAR,FRONT
AIRCRAFT MISSION DESIGN SERIES F-16
OVERALL LENGTH 2.000 INCHES NOMINAL
OVERALL WIDTH 2.000 INCHES NOMINAL
MATERIAL THICKNESS 0.500 INCHES NOMINAL
SPECIAL FEATURES DIMS ARE STOCK MATERIAL; NHA 16W030M1
PART NAME ASSIGNED BY CONTROLLING AGENCY FILLER
MANUFACTURERS CODE 81755
DESIGN CONTROL REFERENCE 16W592-12

Restrictions/Controls & Freight Information | NSN 1560-01-521-8968

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
Electro-static Discharge Susceptible:ANo known Electrostatic Discharge (ESD) or Electromagnetic Interference (EMI) sensitivity
Category Code Description
No Freight Information