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 7172056 results (0.48 seconds)
- 9530-00-129-9704 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL THICKNESS
- 0.2500 INCHES NOMINAL
- CROSS-SECTIONAL WIDTH
- 1.750 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-5 SOLUTION HEAT TREATED
- 9540-01-390-5958 STRUCTURAL SECTION,SPECIAL SHAPEDMore Info ...
- DEPARTURE FROM CITED DOCUMENT
- AS DIFFERENTIATED BY MATERIAL, TEMPER AND LENGTH REQUIREMENTS
- FABRICATION METHOD
- ANY ACCEPTABLE
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- END ITEM IDENTIFICATION
- END USE METAL, RLT-1192
- MATERIAL
- ALUMINUM ALLOY 6063
- 9540-00-140-4978 ANGLE,STRUCTURALMore Info ...
- BASIC SHAPE STYLE
- ANGLE
- BASE FLANGE THICKNESS
- 0.125 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE
- 0.156 INCHES NOMINAL
- FIRST TIP RADIUS
- 0.125 INCHES NOMINAL
- 9530-00-128-2252 BAR,METALMore Info ...
- BASIC SHAPE STYLE
- FLAT
- CROSS-SECTIONAL THICKNESS
- 0.2500 INCHES NOMINAL
- CROSS-SECTIONAL WIDTH
- 0.500 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-5 SOLUTION HEAT TREATED
- 9540-00-263-7275 ANGLE,STRUCTURALMore Info ...
- BASE FLANGE THICKNESS
- 0.250 INCHES NOMINAL
- BASIC SHAPE STYLE
- ANGLE
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE
- 0.250 INCHES NOMINAL
- FIRST TIP STYLE
- SQUARE END
- 9540-00-395-6411 STRUCTURAL SECTION,SPECIAL SHAPEDMore Info ...
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- END ITEM IDENTIFICATION
- C-141 AIRCRAFT
- MATERIAL
- ALUMINUM ALLOY AMS-QQ-A-200/9, ALLOY 6063
- NONDEFINITIVE SPEC/STD DATA
- T6 TEMPER
- 9540-01-012-0839 STRUCTURAL SECTION,SPECIAL SHAPEDMore Info ...
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- MATERIAL
- ALUMINUM ALLOY AMS-QQ-A-200/9, ALLOY 6063
- NONDEFINITIVE SPEC/STD DATA
- T6 TEMPER
- LENGTH
- 20.000 FEET NOMINAL
- 9540-01-191-3364 CHANNEL,STRUCTURALMore Info ...
- BASE FLANGE THICKNESS
- 0.125 INCHES NOMINAL
- BASIC SHAPE STYLE
- CHANNEL
- FABRICATION METHOD
- EXTRUDED
- FIRST TIP STYLE
- SQUARE END
- HEAT TREATMENT
- T-5 SOLUTION HEAT TREATED
- 9540-00-235-2436 STRUCTURAL SECTION,SPECIAL SHAPEDMore Info ...
- FABRICATION METHOD
- EXTRUDED
- HEAT TREATMENT
- T-6 SOLUTION HEAT TREATED
- MATERIAL
- ALUMINUM ALLOY AMS-QQ-A-200/9, ALLOY 6063
- NONDEFINITIVE SPEC/STD DATA
- T6 TEMPER
- LENGTH
- 12.000 FEET NOMINAL
- 9540-00-140-2401 ANGLE,STRUCTURALMore Info ...
- BASIC SHAPE STYLE
- ANGLE
- BASE FLANGE THICKNESS
- 0.125 INCHES NOMINAL
- FABRICATION METHOD
- EXTRUDED
- FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE
- 0.156 INCHES NOMINAL
- FIRST TIP RADIUS
- 0.125 INCHES NOMINAL
