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NSN 9535-01-531-2513, 9535015312513
PLATE,METAL

Federal Supply Classification
FSC 9535 - Plate, Sheet, Strip, and Foil; Nonferrous Base Metal
National Item Identification Number
NIIN 015312513
Codification Country
United States
Item Name Code
INC 37013
Criticality
(X) This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.
Hazardous Material Indicator Code
(N) There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials.
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DLMS® Summary

National Stock Number 9535-01-531-2513

National Stock Number (NSN) 9535-01-531-2513, or NIIN 015312513, (plate,metal) was assigned June 29, 2005 in the Federal Logistics Information System (FLIS). This NIIN is Available for Manual Assignment. This NSN does not replace any other NSNs.

There are 2 manufacturer part numbers associated with this NSN. One of those part number(s) are considered obsolete. The manufacturer part numbers were originally supplied by one supplier. Today, one supplier is listed as an Active supplier for this NSN. Of the active suppliers, only one supplier is deemed design controlled or valid supply parts.

This part number has not been procured by the US Government in over 5 years.

This NSN is assigned to Item Name Code (INC) 37013. [A FERROUS OR NONFERROUS PRODUCT WITH CROSS-SECTIONAL DIMENSIONS. EXCLUDES:ARMOR PLATE; PLATE, FLOOR, METAL; TERNEPLATE; AND TINPLATE. FOR SILVER PLATE ITEMS SEE SILVER SHEET.]. This item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. There is no data in the HMIRS and the NSN is in an FSC not generally suspected of containing hazardous materials. NSN 9535015312513 does not contain precious metals.

This information was last updated on .


Technical Characteristics

END ITEM IDENTIFICATION
(AGAV) FUSELAGE, F4F JET AIRCRAFT
BASIC SHAPE STYLE
(AGTA) SOLID
CROSS-SECTIONAL THICKNESS
(ADVM) 1.0000 INCHES NOMINAL
FABRICATION METHOD
(AARN) COLD FINISH
LENGTH
(ABRY) 10.000 FEET NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATION
(MDCL) QQ-A-225/9 FED SPEC 1ST MATERIAL RESPONSE
MATERIAL
(MATT) ALUMINUM ALLOY 7075
MINIMUM TENSILE STRENGTH
(CQBC) 77000 POUNDS PER SQUARE INCH
MINIMUM YIELD STRENGTH
(CQHQ) 66000 POUNDS PER SQUARE INCH
WIDTH
(ABGL) 3.000 INCHES NOMINAL
III END ITEM IDENTIFICATION
(AGAV) FUSELAGE, F4F JET AIRCRAFT
MATERIAL
(MATL) ALUMINUM ALLOY, QQ-A-225/9
UNABLE TO DECODE
(MATL) UNABLE TO DECODE


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