Nonferrous Base Metal Structural Shapes: LS4306, LS4346, LS4353
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| LS4306 | 9540-00-027-9219 | Beam, Structural | Material: Aluminum alloy, QQ-A-200/11, alloy 7075 Fabrication Method: Extruded Length: Any acceptable | Lockheed Martin Corporation (98897) | |
| LS4317 | 9540-00-805-5989 | Beam, 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) | |
| LS4319 | 9540-00-027-9218 | Beam, 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) | |
| LS4320 | 9540-01-144-1746 | Structural Section, Special Shape | 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) | |
| LS4321 | 9540-01-453-4175 | Beam, Structural | Material: Aluminum alloy, QQ-A-200/11 Fabrication Method: Extruded Length: 2.180 inches nominal | Transtar Metals Corp. (29321) | |
| LS4322 | 9540-01-011-8027 | Beam, 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) | |
| LS4325 | 9540-01-005-4117 | Beam, Structural | Material: Aluminum alloy AMS-QQ-A-200/13, alloy 7178 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS4326 | 9540-01-213-5538 | Beam, 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) | |
| LS4327 | 9540-00-806-3646 | Beam, 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) | |
| LS4331 | 9540-00-027-9217 | Beam, Structural | Material: Aluminum alloy Fabrication Method: Extruded Length: 0.167 feet nominal | Lockheed Martin Corporation (98897) | |
| LS4331-2 LS43312 | 9540-00-556-8913 | Beam, Structural | Material: Aluminum alloy AMS-QQ-A-200/15, alloy 7075 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS4335 | 9540-00-982-4384 | Beam, Structural | Material: Aluminum alloy Fabrication Method: Extruded Length: 0.250 feet nominal | Lockheed Martin Corporation (98897) | |
| LS4336 | 9540-00-805-5984 | 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) | |
| LS4338 | 9540-00-414-3793 | Channel, 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) | |
| LS4340 | 9540-00-805-8022 | Angle, Structural | Material: Aluminum alloy, QQ-A-200/11 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS4342 | 9540-01-499-4404 | Extruded T-Section | Lockheed Martin Corporation (98897) | ||
| LS4344 | 9540-00-805-8019 | Beam, Structural | Material: Aluminum alloy, QQ-A-200/11, alloy 7075 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS4344 | 9540-01-559-5248 | Angle, Structural | III End Item Identification: Aircraft, C-5 III Part Name Assigned By Controlling Agency: Angle, structural | Society of Automotive Engineers Inc. (81343) | |
| LS4346 | 9540-00-027-9216 | Beam, Structural | Material: Aluminum alloy Fabrication Method: Extruded Length: 0.282 feet nominal | Lockheed Martin Corporation (98897) | |
| LS4349 | 9540-00-595-8624 | Angle, Structural | Material: Aluminum alloy AMS-Q-A-200/11, alloy 7075 Fabrication Method: Extruded Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS4353 | 9540-01-395-3565 | 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) |