Structural Shapes: IM2607, LS3908, LS6378
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| IM2607 | 9520-01-286-4211 | Angle, Structural | Boeing Company, The (76301) | ||
| K633035-17 K63303517 | 9520-01-558-4504 | Angle, Structural | Special Features: Structural End Item Identification: SH2 aircraft | Kaman Aerospace Corporation (84955) | |
| K633035-18 K63303518 | 9520-01-558-4503 | Angle, Structural | Special Features: Structural End Item Identification: SH2 aircraft | Kaman Aerospace Corporation (84955) | |
| KC1772 | 9520-00-740-9812 | Channel, Structural | Material: Steel Fabrication Method: Centrifugal cast Length: 1.917 feet nominal | Diamond REO Truck Co. (56442) | |
| KD84035-125 KD84035125 | 9520-01-589-0479 | Angle, Structural | Material: Aluminum alloy, QQ-A-200/3 Special Features: End item:support tray | Kaman Aerospace Corporation (84955) | |
| L3X2X0.375X5.9LB/FT L3X2X0375X59LBFT | 9520-01-276-3459 | Angle, Structural | Material: Steel, MIL-S-22698, grade AH36 Overall Width: 3.000 inches nominal Left Side Flange Thickness: 0.375 inches nominal | Defense Logistics Agency (14153) | |
| LL-H47-0327 LLH470327 | 9520-01-447-6734 | Molding, Metal | Special Features: Used on main frame;drive pack assembly-head; end item application 6530-01-447-1838; bed, adjustable; model 5U2.369 | Naval Medical Material Support (66736) | |
| LL-H47-0341 LLH470341 | 9520-01-447-9999 | Molding, Metal | Special Features: Used on drive pack; tube-drive, head; end item application 6530-01-447-1838; bed, adjustable; model 5U2.36P | Naval Medical Material Support (66736) | |
| LL-H47-0346 LLH470346 | 9520-01-448-0489 | Molding, Metal | Special Features: Drive pack assembly-knee; usedf on main frame | Naval Medical Material Support (66736) | |
| LL-H47-0352 LLH470352 | 9520-01-448-1204 | Molding, Metal | Special Features: Link-drag; used on under carriage End Item Identification: 6530-01-447-1838; bed, adjustable; model 5U2.36P | Naval Medical Material Support (66736) | |
| LS1013597 | 9520-01-505-7890 | Beam, Structural | General Dynamics Land Systems Inc. (01417) | ||
| LS1013597 | 9520-01-505-9114 | Beam, Structural | General Dynamics Land Systems Inc. (01417) | ||
| LS10140-2001 LS101402001 | 9520-01-457-3574 | Structural Section, Special Shape | End Item Identification: Aircraft frame C-5 series | Lockheed Martin Corporation (98897) | |
| LS2221 | 9520-01-240-0343 | Channel, Structural | Lockheed Martin Corporation (98897) | ||
| LS35090C2D2913 | 9520-01-571-4166 | Angle, Structural | Special Features: Extruded angle End Item Identification: Used on C-130 aircraft/general usage | Lockheed Martin Corporation (98897) | |
| LS37640 | 9520-01-532-1479 | Angle, Structural | Overall Width: 0.130 inches minimum and 0.190 inches maximum Basic Shape Style: Angle Left Side Flange Thickness: 0.012 inches nominal | Lockheed Martin Corporation (98897) | |
| LS37641-1 LS376411 | 9520-01-104-5105 | Structural Section, Special Shape | Material: Steel, ams 5516 Fabrication Method: Hot rolled or cold rolled Length: 10.000 feet minimum and 12.000 feet maximum | Lockheed Martin Corporation (98897) | |
| LS3908 | 9520-01-424-4799 | Beam, Structural | Special Features: Material aluminum alloy 2024-T4; one side of T is 125 deg angle Right Side Top Flange Distance to Center of Both Flanges: 1.810 inches nominal Left Side Top Flange Distance to Center of Both Flanges: 1.400 inches nominal | Lockheed Martin Corporation (98897) | |
| LS4133 | 9520-01-431-4585 | Structural Section, Special Shape | Lockheed Martin Corporation (98897) | ||
| LS5018 | 9520-00-973-7839 | Structural Section, Special Shape | Lockheed Martin Corporation (98897) | ||
| LS6378 | 9520-01-345-7813 | Beam, Structural | Lockheed Martin Corporation (98897) |