Airframe Structural Components: 332-311112-3, 33-2357-501, 3325526-5
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 332-311112-3 3323111123 | 1560-00-144-8014 | Cover, Access, Aircraft | Material: Aluminum alloy 7075 Material Document and Classification: QQ-250/13 fed spec single material response Peripheral Shape Style: 46 rectangle, multi holes | Rockwell International Corp. (89372) | |
| 332-311112-5 3323111125 | 1560-00-143-7338 | Door, Access, Aircraft | Rockwell International Corp. (89372) | ||
| 33-2322 332322 | 1560-00-778-8294 | Collar, Switch, Control Wheel | General Characteristics Item Description: Steel, MIL-S-6758, 0.740 in. min, 0.745 max dia, 0.620 in. min, 0.635 max id first end, 0.500-32 UNS-3B thd second end | The Boeing Company (81205,82918) | |
| 3323266-500 3323266500 | 1560-00-213-2832 | Latch Assembly, Aircraft | Aircraft Mission Design Series: C-118 | Boeing Company, The (18355,88277) | |
| 3-32350-1 3323501 | 1560-01-515-6650 | Stabilizer, Horizontal | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-32350-2 3323502 | 1560-01-515-6651 | Stabilizer, Horizontal | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-32350-501 332350501 | 1560-01-515-6652 | Stabilizer, Horizontal | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 33-2351 332351 | 1560-00-876-5840 | Coupling, Engine Control | III End Item Identification: B-52 aircraft General Characteristics Item Description: Cres, MIL-S-5059, 18-8, AISI301, 0.025 hardness, center hole for 0.188IN. bolt | The Boeing Company (81205) | |
| 33-2357 332357 | 1560-00-790-5860 | Support Assembly, Electrical | III End Item Identification: B52 acft General Characteristics Item Description: C/O 1 ea support P/N 33-2357-1, 1EA nut plate minature P/N RM52LHTA575M-02; used on engine oil cooler | The Boeing Company (81205,82918) | |
| 33-2357-501 332357501 | 1560-00-731-5445 | Support Assy, Electr | The Boeing Company (81205,82918) | ||
| 3-32360-1 3323601 | 1560-01-515-6653 | Stabilizer, Horizontal | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-32360-2 3323602 | 1560-01-515-6654 | Stabilizer, Horizontal | III End Item Identification: F5 aircraft | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-32360-501 332360501 | 1560-01-419-4885 | Stabilizer, Horizontal | Aircraft Mission Design Series: F-5 Material: Aluminum alloy Overall Length: 62.000 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-32360-502 332360502 | 1560-01-419-4886 | Stabilizer, Horizontal | Aircraft Mission Design Series: F-5 Material: Aluminum alloy Overall Length: 62.000 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 33-2446-1 3324461 | 1560-00-731-5449 | Support, Spring, Door | The Boeing Company (81205,82918) | ||
| 3325082-1 33250821 | 1560-01-496-5794 | Tab, Trim, Aircraft | Lockheed Martin Corporation (98897) | ||
| 332518-8 3325188 | 1560-01-447-9855 | Beam, Aircraft | III End Item Identification: C-130 aircraft | Lockheed Martin Corporation (98897) | |
| 332-533310 332533310 | 1560-00-231-1520 | Duct Assy, Inlet | Rockwell International Corp. (89372) Sabreliner Corporation (0ESK8) | ||
| 3325445-1 33254451 | 1560-01-455-9439 | Balance Weight, Aileron | Aircraft Mission Design Series: C-130J Aircraft Location: Aileron assembly End Item Identification: Hercules aircraft, model C-130J | Lockheed Martin Corporation (98897) | |
| 3325526-5 33255265 | 1560-01-523-5745 | Wing Section, Outer | Aircraft Mission Design Series: C-130E Special Features: Opposite of P/N 3325526-6 | Lockheed Martin Corporation (98897) |