At Broadline NSN, our aim is to help customers meet their operational requirements by supplying an extensive inventory of items that are available for procurement. On this page, you can explore a catalog of high-demand parts that are organized under the NSN 9540-00-148-4853, a unique identifier for products that are exceptionally popular. This includes top-requested part numbers like LS236, AMS-QQ-A-200, 1M519, 1093762, 111164, and numerous others, and you always have the option to pinpoint desired parts using our search engine and filters. We are the only independent distributor that operates with a NO CHINA SOURCING pledge, meaning that every item is sourced from a trusted NSN parts supplier on our Approved Vendor List (AVL).
As soon as you come across an item of interest, do not hesitate to submit a quote request by simply clicking on the “RFQ” button situated next to any offering. When completing an RFQ form, we ask that you include desired delivery dates and target price points, among other pertinent details about your needs for NSN 9540-00-148-4853. Within 15 minutes or less of submission, one of our industry experts will reach out with a customized quote that features competitive pricing and convenient shipping options. Get started today and see how we can serve as your strategic sourcing partner!
| Item Name | Beam Structural |
| Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
| Federal Supply Class (FSC) | 9540 Structural Shapes Nonferrous Base Metal |
| National Item Identification Number (NIIN) | 00-148-4853 (001484853) |
| NCB Code | USA (00) |
| Manufacturer | Lockheed Martin Corporation, Society Of Automotive Engineers Inc, Boeing Company The, Textron Aviation Inc, Aluminum Co Of America, Beechcraft Corporation, International Light Metals Corp, Sae International, Transtar Metals Corp, Alcoa Reynolds Metals Company, Federal Specifications |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| LS236 | lockheed martin corporation | beam structural | RFQ |
| AMS-QQ-A-200 | society of automotive engineers inc | beam structural | RFQ |
| 1M519 | boeing company the | beam structural | RFQ |
| 1093762 | boeing company the | beam structural | RFQ |
| 111164 | textron aviation inc | beam structural | RFQ |
| 22008 | aluminum co of america | beam structural | RFQ |
| 111164 | beechcraft corporation | beam structural | RFQ |
| 13683 | international light metals corp | beam structural | RFQ |
| AMS-QQ-A-200 | sae international | beam structural | RFQ |
| PA6569 | transtar metals corp | beam structural | RFQ |
| 199985 | alcoa reynolds metals company | beam structural | RFQ |
| 2-2232 | lockheed martin corporation | beam structural | RFQ |
| 60-726 | transtar metals corp | beam structural | RFQ |
| QQ-A-200/3 | federal specifications | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 1.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.065 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.065 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJB | FIRST TIP RADIUS | 0.031 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.065 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 1.500 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.200 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | SQUARE END |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-3510 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T3510 TEMPER OR T3511 TEMPER |
| Relevant Components for NSN - 9540-00-148-4853, 9540001484853 | ||||
| 9515-01-465-0696 (9515014650696) | 9530-00-973-5699 (9530009735699) | 9530-00-060-5019 (9530000605019) | 9530-00-236-0309 (9530002360309) | |
| 9535-00-231-8391 (9535002318391) | 9535-01-633-1693 (9535016331693) | 9520-00-277-4938 (9520002774938) | 9515-14-379-9914 (9515143799914) | |
| 9515-01-612-9969 (9515016129969) | 9515-01-604-3872 (9515016043872) | 9510-01-043-3619 (9510010433619) | 9520-00-516-5814 (9520005165814) | |
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