NSN Search by National Stock Number

Search the MCRL (Master Cross-Reference List) provided by the FLIS (Federal Logistics Information Service) through the DLA (Defense Logistics Agency) of the DOD (Department of Defense). FLIS provides this data through their WebFLIS and FEDLOG products, but these are not available for public use. This free NSN Search provides NSN lookup of the Military NSN Database by National Stock Number.

The NSN Lookup search engine allows you to easily search for National Stock Numbers (NSN) over all of the catalogs and databases available within NATO for public use:

About 7616 results (0.09 seconds)

9535-00-232-7590 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.0630 INCHES NOMINAL
FABRICATION METHOD
ROLLED
HEAT TREATMENT
O-ANNEALED
MATERIAL
ALUMINUM ALLOY AMS-QQ-A-250/8, ALLOY 5052
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9535-01-493-4959 SHEET,METAL
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CLADDING THICKNESS
0.003 INCHES BOTH SIDES
FABRICATION METHOD
ROLLED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE
MATERIAL
ALUMINUM ALLOY 2024
MINIMUM YIELD STRENGTH
36000 POUNDS PER SQUARE INCH
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9535-01-493-4957 SHEET,METAL
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CLADDING THICKNESS
0.003 INCHES BOTH SIDES
FABRICATION METHOD
ROLLED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE
MATERIAL
ALUMINUM ALLOY 2024
MINIMUM YIELD STRENGTH
38000 POUNDS PER SQUARE INCH
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9535-00-084-4420 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.0400 INCHES NOMINAL
FABRICATION METHOD
ROLLED
HEAT TREATMENT
O-ANNEALED
MATERIAL
ALUMINUM ALLOY AMS-QQ-A-250/8, ALLOY 5052
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9535-01-493-4960 SHEET,METAL
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CLADDING THICKNESS
0.0028 INCHES BOTH SIDES
FABRICATION METHOD
ROLLED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE
MATERIAL
ALUMINUM ALLOY 2024
MINIMUM YIELD STRENGTH
38000 POUNDS PER SQUARE INCH
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5310-00-054-0468 WASHER,FLAT
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CENTER HOLE SHAPE STYLE
ROUND
CROSS-SECTIONAL SHAPE STYLE
RECTANGULAR
HOLE DIAMETER
0.370 INCHES MINIMUM AND 0.390 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A362,TEMPER T3 FED SPEC SINGLE MATERIAL RESPONSE OVERALL
MATERIAL
ALUMINUM ALLOY 2024 OVERALL
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9535-01-495-1601 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.1900 INCHES NOMINAL
FABRICATION METHOD
ROLLED
HEAT TREATMENT
T-6 SOLUTION HEAT TREATED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/12 FED SPEC 1ST MATERIAL RESPONSE
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9535-01-518-8793 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.125 INCHES NOMINAL
FABRICATION METHOD
ROLLED
HEAT TREATMENT
T-6 SOLUTION HEAT TREATED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/13 FED SPEC 1ST MATERIAL RESPONSE
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9535-01-495-1602 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.0160 INCHES NOMINAL
FABRICATION METHOD
ROLLED
HEAT TREATMENT
O-ANNEALED
MATERIAL DOCUMENT AND CLASSIFICATION
QQ-A-250/11 FED SPEC 1ST MATERIAL RESPONSE
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9535-01-399-6117 SHEET,METAL
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BASIC SHAPE STYLE
SOLID
CROSS-SECTIONAL THICKNESS
0.0320 INCHES NOMINAL
FABRICATION METHOD
ANY ACCEPTABLE
HEAT TREATMENT
T-6 SOLUTION HEAT TREATED
MATERIAL
ALUMINUM ALLOY, AMS-QQ-A-250/12, ALLOY 7075
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