Airframe Structural Components: 388332-1, 388371-1, 388400-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 388332-1 3883321 | 1560-00-862-6346 | Bracket Assembly, Pu | Lockheed Martin Corporation (98897) | ||
| 388333-1 3883331 | 1560-00-862-6345 | Pulley Bracket Assembly | General Characteristics Item Description: Aluminum alloy, bracket QQ-A-200/11, pulley QQ-A-225/6 | Lockheed Martin Corporation (98897) | |
| 388334-1 3883341 | 1560-00-862-6344 | Box, Radio Transmitt | Lockheed Martin Corporation (98897) | ||
| 388337-11 38833711 | 1560-01-580-2343 | Stiffener, Aircraft | Lockheed Martin Corporation (98897) | ||
| 388337-14 38833714 | 1560-01-580-2722 | Stiffener, Aircraft | Lockheed Martin Corporation (98897) | ||
| 388337-5 3883375 | 1560-01-299-1158 | Former, Aircraft | Aircraft Mission Design Series: C-130 Special Features: Finish F-1; nha 388085-1 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 388337-6 3883376 | 1560-01-291-8095 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-130 Special Features: T3 clad Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 388341-1 3883411 | 1560-00-875-0063 | Manifold, Fluid, Aircraft | Overall Length: 11.140 inches nominal Overall Width: 11.100 inches nominal Material: Aluminum alloy | Lockheed Martin Corporation (98897) | |
| 388371-1 3883711 | 1560-01-233-2158 | Fitting | Lockheed Martin Corporation (98897) | ||
| 388372-1 3883721 | 1560-00-862-6343 | Support Assembly, Gear box | General Characteristics Item Description: Aluminum alloy, QQ-A-250/11, 5.550 in. lg, 0.280 in. min, 0.287 in. max dia hole thru 4 places | Lockheed Martin Corporation (98897) | |
| 388381-7 3883817 | 1560-01-398-5858 | Bracket, Structural Component, Air | Aircraft Mission Design Series: C-130B Material: Aluminum alloy 2024 Aircraft Location: Wing, inboard dry bay | Lockheed Martin Corporation (98897) | |
| 388384-19 38838419 | 1560-01-395-5910 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Aluminum alloy 2024 Aircraft Location: Wing pylon | Lockheed Martin Corporation (98897) | |
| 388392-10 38839210 | 1560-01-576-0010 | Frame, Aircraft | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130H acft Special Features: C/O shims, strap, caps, collars, lockbolts, reinforcing plate, track | Lockheed Martin Corporation (98897) | |
| 388392-9 3883929 | 1560-01-576-0034 | Frame, Aircraft | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130H acft Special Features: C/O shims, strap, caps, collars, lockbolts, cap, reinforcing plate, track | Lockheed Martin Corporation (98897) | |
| 388394-1 3883941 | 1560-01-295-3575 | Support, Structural Component, Air | Lockheed Martin Corporation (98897) | ||
| 388394-2 3883942 | 1560-01-273-2467 | Support, Structural Component, Air | Lockheed Martin Corporation (98897) | ||
| 388400-1 3884001 | 1560-00-862-8116 | Leading Edge, Aircraft | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) | |
| 388400-11 38840011 | 1560-00-862-8115 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-130 Material Document and Classification: QQ-A-250 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 388400-12 38840012 | 1560-00-863-5257 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-130 Material Document and Classification: QQ-A-250 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 388400-2 3884002 | 1560-00-862-8119 | Leading Edge, Aircraft | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) |