FSC 9540 Nonferrous Base Metal Structural Shapes: 9540-00-145-0608, 9540-00-145-4480, 9540-00-145-4530
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 9540-00-145-0608 9540001450608 | AMS-QQ-A-200/3 ASTM B221 37725 AMS-STD-184 QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Aluminum Co. of America (01634) American Society for Testing and (81346) Federal Specifications (81348) | |
| 9540-00-145-0633 9540001450633 | AMS-QQ-A-200/3 14064 QQA200-3 | Structural Section, Special Shape | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Federal Specifications (81348) Society of Automotive Engineers Inc. (81343) Aluminum Co. of America (01634) | |
| 9540-00-145-0642 9540001450642 | BAC1513-20 AMS-QQ-A-200/3 60-7825 QQA200-3A 22872 | Structural Section, Special Shape | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Aluminum Co. of America (01634) Boeing Company, The (76301) Federal Specifications (81348) | |
| 9540-00-145-0685 9540001450685 | 30000 QQ-A-200/3 AMS-QQ-A-200/3 LS3298 60-4796 | Structural Section, Special Shape | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) Aluminum Co. of America (01634) Transtar Metals Corp. (29321) | |
| 9540-00-145-4479 9540001454479 | QQ-A-200/3 S102 BAC1503-8893 734S AMS-QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | American Society for Testing and (81346) Lockheed Martin Corporation (80070) Aluminum Co. of America (01634) | |
| 9540-00-145-4480 9540001454480 | QQ-A-200/3 1M211 BAC1503-5985 734T | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Federal Specifications (81348) Aluminum Co. of America (01634) Boeing Company, The (76301) | |
| 9540-00-145-4481 9540001454481 | 734T AMS-STD-184 AMS-QQ-A-200/11 PA4450 QQ-A-200/11 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/11, alloy 7075 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Transtar Metals Corp. (06012) Aluminum Co. of America (01634) Society of Automotive Engineers Inc. (81343) | |
| 9540-00-145-4488 9540001454488 | 734Y BAC1503-13068 ASTM B221 AMS-QQ-A-200/3 QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | The Boeing Company (82918) American Society for Testing and (81346) Aluminum Co. of America (01634) | |
| 9540-00-145-4491 9540001454491 | 1312 ASTM B221 AMS-QQ-A-200/3 QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Society of Automotive Engineers Inc. (81343) American Society for Testing and (81346) Federal Specifications (81348) | |
| 9540-00-145-4502 9540001454502 | AMS-QQ-A-200/3 ASTM B221 S291 QQ-A-200/3 AND10133-0702 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Cessna Aircraft Company (71379) American Society for Testing and (81346) Society of Automotive Engineers Inc. (81343) | |
| 9540-00-145-4503 9540001454503 | QQ-A-200/3 AND10133-1001 | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Federal Specifications (81348) Airforce-Navy Aeronautical Design (99237) | |
| 9540-00-145-4509 9540001454509 | QQ-A-200/3 AND10133-1204 AMS-QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Federal Specifications (81348) Society of Automotive Engineers Inc. (81343) Airforce-Navy Aeronautical Design (99237) | |
| 9540-00-145-4513 9540001454513 | 10140 ASTM B221 AMS-QQ-A-200/3 1047872 2-1356 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Airforce-Navy Aeronautical Design (99237) American Society for Testing and (81346) Boeing Company, The (18355, 88277) | |
| 9540-00-145-4517 9540001454517 | AND10133-2403 QQA200-3 | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Airforce-Navy Aeronautical Design (99237) Federal Specifications (81348) | |
| 9540-00-145-4518 9540001454518 | QQ-A-200/3 AND10134-1003 K10A25O | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Federal Specifications (81348) Airforce-Navy Aeronautical Design (99237) Lockheed Martin Corporation (81755) | |
| 9540-00-145-4521 9540001454521 | LS10134-1005-6 AND10134-1005 AMS-QQ-A-200/11 QQ-A-200/11 AND10134-1005/QQ-A-200/11-0 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/11, alloy 7075 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) American Society for Testing and (81346) Society of Automotive Engineers Inc. (81343) | |
| 9540-00-145-4524 9540001454524 | QQ-A-200/3 AND10134-1201 LS10134-1201-1 1238984 S78 | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Airforce-Navy Aeronautical Design (99237) Boeing Company, The (18355, 88277) Cessna Aircraft Company (71379) | |
| 9540-00-145-4525 9540001454525 | 10176 2-1352 AMS-QQ-A-200/3 ASTM B221 AMS10134-1203 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Heat Treatment: T-3511 solution heat treated | Airforce-Navy Aeronautical Design (99237) American Society for Testing and (81346) Boeing Company, The (88277, 18355) | |
| 9540-00-145-4528 9540001454528 | AMS-QQ-A-200/11 AND10134-1404 QQ-A-200/11 AND10134-1404/QQ-A-200/11-T6 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/11, alloy 7075 Fabrication Method: Extruded Heat Treatment: T-6 solution heat treated | Federal Specifications (81348) Defense Logistics Agency (14153) Airforce-Navy Aeronautical Design (99237) | |
| 9540-00-145-4530 9540001454530 | QQ-A-200/3 AND10134-1405 ASTM B221 AMS-QQ-A-200/3 | Angle, Structural | Material: Aluminum alloy AMS-QQ-A-200/3, alloy 2024 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Society of Automotive Engineers Inc. (81343) Federal Specifications (81348) American Society for Testing and (81346) |