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 9540-00-008-6033, a unique identifier for products that are exceptionally popular. This includes top-requested part numbers like AMS QQ A 200 11, AMS-QQ-A-200 11, LS10140-4003-5, QQA200-11, AND10140-4003, 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 9540-00-008-6033. 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) | 00-008-6033 (000086033) |
| NCB Code | USA (00) |
| Manufacturer | Sae International, Society Of Automotive Engineers Inc, Lockheed Martin Corporation, Federal Specifications, Airforce-Navy Aeronautical Design Standard |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| AMS QQ A 200 11 | sae international | beam structural | RFQ |
| AMS-QQ-A-200 11 | society of automotive engineers inc | beam structural | RFQ |
| LS10140-4003-5 | lockheed martin corporation | beam structural | RFQ |
| QQA200-11 | federal specifications | beam structural | RFQ |
| AND10140-4003 | airforce-navy aeronautical design standard | beam structural | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 4.000 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | I SHAPE |
| AJJB | FIRST TIP RADIUS | 0.125 INCHES NOMINAL |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BMPR | LEFT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
| BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
| BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXK | FILLET RADIUS WHERE BOTTOM 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 |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXN | WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 2.000 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.173 POUNDS PER LINEAR FOOT |
| CMZY | FIRST TIP STYLE | LOWER RADIUS |
| CNBB | THIRD TIP RADIUS | 0.125 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | NOT IDENTICAL |
| CNQM | THIRD TIP STYLE | UPPER RADIUS |
| CNQN | FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/THIRD TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/11,ALLOY 7075 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER |
| Relevant Components for NSN - 9540-00-008-6033, 9540000086033 | ||||
| 9540-01-494-7775 (9540014947775) | 9535-01-219-0540 (9535012190540) | 9540-01-698-9454 (9540016989454) | 9530-01-186-0808 (9530011860808) | |
| 9540-01-471-8215 (9540014718215) | 9540-00-846-3462 (9540008463462) | 9535-00-277-7794 (9535002777794) | 9510-00-188-1744 (9510001881744) | |
| 9540-01-221-6527 (9540012216527) | 9505-00-962-7405 (9505009627405) | 9530-01-465-0784 (9530014650784) | 9510-00-227-8536 (9510002278536) | |
The only independent
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote