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 2004220 results (0.95 seconds)
- 9540-00-277-6059 CHANNEL,STRUCTURALMore Info ...
- BASIC SHAPE STYLE
- CHANNEL
- BASE FLANGE THICKNESS
- 0.325 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE
- 0.290 INCHES NOMINAL
- FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE
- 0.290 INCHES NOMINAL
- 9530-00-640-4452 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL THICKNESS
- 0.3750 INCHES NOMINAL
- CROSS-SECTIONAL WIDTH
- 1.000 INCHES NOMINAL
- FABRICATION METHOD
- ROLLED OR DRAWN OR COLD FINISH
- HEAT TREATMENT
- T-6511 SOLUTION HEAT TREATED AND ARTIFICALLY AGED
- 9540-01-358-7367 BEAM,STRUCTURALMore Info ...
- BASIC SHAPE STYLE
- T SHAPE
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG
- 0.125 INCHES NOMINAL
- FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG
- 0.125 INCHES NOMINAL
- FIRST TIP RADIUS
- 0.094 INCHES NOMINAL
- 9530-01-450-6722 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL WIDTH
- 6.500 INCHES NOMINAL
- CROSS-SECTIONAL THICKNESS
- 0.50000 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- 9540-01-303-4848 BEAM,STRUCTURALMore Info ...
- BASIC SHAPE STYLE
- Z SHAPE
- BOTTOM FLANGE WIDTH
- 1.000 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG
- 0.125 INCHES NOMINAL
- FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG
- 0.125 INCHES NOMINAL
- 9530-00-228-9322 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL WIDTH
- 4.000 INCHES NOMINAL
- CROSS-SECTIONAL THICKNESS
- 0.3750 INCHES NOMINAL
- FABRICATION METHOD
- COLD FINISH
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- 9530-00-236-0333 BAR,METALMore Info ...
- EDGE TYPE
- SQUARE
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL WIDTH
- 6.000 INCHES NOMINAL
- CROSS-SECTIONAL THICKNESS
- 0.7500 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED OR COLD FINISH
- 9530-00-684-6222 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- ROUND
- CROSS SECTION OUTSIDE DIAMETER
- 1.312 INCHES NOMINAL
- FABRICATION METHOD
- COLD FINISH OR DRAWN OR EXTRUDED OR ROLLED
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- MATERIAL
- ALUMINUM ALLOY AMS-QQ-A-225/8, ALLOY 6061
- 9530-01-262-8859 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- SQUARE
- CROSS-SECTIONAL WIDTH ACROSS FLATS
- 2.500 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6511 SOLUTION HEAT TREATED
- MATERIAL
- ALUMINUM ALLOY AMS-QQ-A-200/8, ALLOY 6061
- 9530-01-497-1198 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- ROUND
- CROSS SECTION OUTSIDE DIAMETER
- 0.750 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6511 SOLUTION HEAT TREATED
- END ITEM IDENTIFICATION
- F/A-18E/F HORNET AIRCRAFT
