Airframe Structural Components: 3524995, 3-52528-1, 352544-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3524995 | 1560-01-125-9157 | Cover Assembly, Amplifier | General Characteristics Item Description: 11.795 in. lg. max.; 8.930 in. W.; nickel plate III FSC Application Data: Amplifier, control detecting ranging system | Raytheon Company (82577) | |
| 3-52502-7 3525027 | 1560-00-768-1038 | Cover, Access, Aircraft | Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5, T4 fed spec single material response Securing Device Type: Threaded fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52503-1 3525031 | 1560-00-768-1039 | Adapter, Dorsal Drain | General Characteristics Item Description: 1.520 in. lg, 1.250 in. id, 4 mtg holes 0.281 in. dia | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52517-1 3525171 | 1560-00-792-8546 | Fitting, Water Tank | General Characteristics Item Description: Aluminum alloy, QQ-A-601, 2.750 in. lg, 2.520 in. W, 0.221 in. dia hole thru base 1 place | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52520-501 352520501 | 1560-00-606-0166 | Fitting, Water Drain | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 3525205-100 3525205100 | 1560-01-262-9266 | Panel, Structural, Aircraft | Raytheon Company (82577) | ||
| 3525264-120 3525264120 | 1560-01-106-9121 | Seal, Crew Door | Raytheon Company (82577) | ||
| 3-52528-1 3525281 | 1560-00-830-9133 | Tank, Fuel, Aircraft | Aircraft Mission Design Series: T-38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52528-25 35252825 | 1560-00-073-4710 | Cover, Fuel Tank | III End Item Identification: Aircraft model F-5 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52528-27 35252827 | 1560-00-073-4711 | Pan Assembly, Fuel | III End Item Identification: Aircraft model F5 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52528-3 3525283 | 1560-00-798-6828 | Cover Assembly | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | ||
| 3-52528-7 3525287 | 1560-00-798-6830 | Pan Assembly, Fuel | III End Item Identification: Aircraft model F5 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52530-1 3525301 | 1560-00-705-2706 | Compartment, Fuel Tank | III End Item Identification: Aircraft model T-38 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 35-25303-506 3525303506 | 1560-01-365-7917 | Fairing, Aircraft | Aircraft Mission Design Series: B-52G Special Features: Used on 35-25303-2 fairing instl, R/H side, P/O stub wing-pylon assy | The Boeing Company (82918) | |
| 3-52531-1 3525311 | 1560-00-792-8547 | Plate Assembly, Stanchion Stowage | Special Features: This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition General Characteristics Item Description: Aluminum alloy QQ-A-362, 12.59 in lg, 1.54 in. W, applicable to model C-130 aircraft Criticality Code Justification: FEAT | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52531-2 3525312 | 1560-00-793-0300 | Fitting, Center Tank Drain | General Characteristics Item Description: Aluminum alloy, QQ-A-601, 4.108 in. min, 4.112 in. max lg, 0.221 in. dia hole thru base 2 places | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 352534 | 1560-00-691-2947 | Shim, Countersunk Anchor nut | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
| 35-25380-2 35253802 | 1560-00-943-3457 | Door, Access, Aircraft | Securing Device Type: Hinge | The Boeing Company (82918) | |
| 352544-3 3525443 | 1560-00-533-5854 | Link, Engine Conditi | Lockheed Martin Corporation (98897) | ||
| 352544-4 3525444 | 1560-00-533-5855 | Link, Engine Conditi | Lockheed Martin Corporation (98897) |