Here on Buy Military Fasteners, we offer competitive procurement options on countless NSN parts from leading manufacturers for the benefit of our customers. On this page, you can find NSN 9540-01-469-9501 parts and supplies, including in-demand part numbers like AMS-QQ-A-200 11-T73511, AMS10140-1404, AMS4617, AND10140-1404, AND10140-1404/QQ-A-200/11-T73511, and others. We encourage you to consider our various options as you see fit, and toward the bottom of this page, you can also locate associated parts of NSN 9540-01-469-9501 with ease. If you take interest in any available part number on our database where you wish to obtain information for procurement, fill out and submit a Request for Quote (RFQ) form through our website. By presenting our staff with important details like your target price and expected fulfillment timeframe, you can expect to receive tailored pricing options that are designed to meet your unique needs and restrictions alike. If at any time you wish to connect with one of our staff members for service, please give us a call or email at any time; we are readily available around the clock and are always happy to provide assistance and consultation through the procurement process. Experience how Buy Military Fasteners serves as a single-sourcing solution for countless needs when you connect with us today.
| 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) | 01-469-9501 (014699501) |
| NCB Code | USA (01) |
| Manufacturer | Society Of Automotive Engineers Inc, Sae International, Airforce-Navy Aeronautical Design Standard, Defense Logistics Agency, Federal Specifications |
| Part Number | Manufacturer | Item Name | Cage Code | RFQ |
|---|---|---|---|---|
| AMS-QQ-A-200 11-T73511 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| AMS10140-1404 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| AMS10140-1404 | sae international | beam structural | 0u583 | RFQ |
| AMS4617 | sae international | beam structural | 0u583 | RFQ |
| AMS4617 | society of automotive engineers inc | beam structural | 81343 | RFQ |
| AND10140-1404 | airforce-navy aeronautical design standard | beam structural | 99237 | RFQ |
| AND10140-1404/QQ-A-200/11-T73511 | defense logistics agency | beam structural | 14153 | RFQ |
| QQ A 200 11 T73511 | federal specifications | beam structural | 81348 | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT CEN SEC |
| AJJB | FIRST TIP RADIUS | 0.010 INCHES NOMINAL |
| BMPR | LEFT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXK | FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | LEFT QUARTER RADIUS |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | WEAPONS SYSTEM IS AIRCRAFT, B-2 BOMBER (ATB) |
| ZZZK | SPECIFICATION/STANDARD DATA | 81348-QQ-A-200/11E/CANCELED/ GOVERNMENT SPECIFICATION AND 99237-AND10140 GOVERNMENT STANDARD |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 32.900 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | I SHAPE |
| BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 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 |
| BPXN | WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| BQJH | BOTTOM FLANGE WIDTH | 2.500 INCHES NOMINAL |
| CMZZ | SECOND TIP RADIUS | 0.010 INCHES NOMINAL |
| CNQK | SECOND TIP STYLE | RIGHT QUARTER RADIUS |
| CNQN | FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/SECOND TIP |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11 |
| Components Related to NSN 9540-01-469-9501 | ||||
| 9535-01-606-4625 (9535016064625) | 9510-00-224-1676 (9510002241676) | 9515-01-562-3748 (9515015623748) | 9515-01-470-0534 (9515014700534) | |
| 9540-00-554-0533 (9540005540533) | 9540-00-401-6825 (9540004016825) | 9530-00-167-1825 (9530001671825) | 9510-01-543-5191 (9510015435191) | |
| 9525-00-277-7829 (9525002777829) | 9515-01-503-2846 (9515015032846) | 9540-00-151-3927 (9540001513927) | 9515-00-925-9565 (9515009259565) | |
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