Airframe Structural Components: 352545-3, 35-25529-3, 35-25751-501
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 352545-3 3525453 | 1560-00-650-5963 | Bushing, Engine Control | General Characteristics Item Description: Bronze QQ-B-637, 0.074 in. max 0.069 in. min lg, 0.312 in. max 0.311 in. min O/D | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | |
| 3-52551-19 35255119 | 1560-00-768-1042 | Cover, Access | Material: Aluminum alloy 7075 END Item Identification: F-5 aircraft Hole Diameter: 0.281 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 35-25529-3 35255293 | 1560-00-958-0535 | Seal Assy, Stabilize | The Boeing Company (82918) | ||
| 35-25529-4 35255294 | 1560-00-954-8081 | Seal Assy, Stabilize | The Boeing Company (82918) | ||
| 35-25529-5 35255295 | 1560-00-954-8082 | Seal Assy, Stabilize | The Boeing Company (82918) | ||
| 35-25529-53 352552953 | 1560-00-954-8084 | Fabric Assembly, Stabilizer | III End Item Identification: Aircraft model F4 | The Boeing Company (82918) | |
| 35-25529-54 352552954 | 1560-00-954-8085 | Fabric Assembly, Stabilizer | III End Item Identification: Aircraft model F4 | The Boeing Company (82918) | |
| 35-25529-6 35255296 | 1560-00-954-8083 | Seal Assy, Stabilize | The Boeing Company (82918) | ||
| 35-25590-2 35255902 | 1560-00-949-6828 | Flange, Static Pressure | III End Item Identification: Aircraft model B52 | The Boeing Company (82918) | |
| 352562 | 1560-00-672-7289 | Name Plate, Indexing | General Characteristics Item Description: Aluminum alloy QQ-A-250/11, 1.500 in. lg, 1.000 in. W, 0.750 in. H | Lockheed Martin Corporation (98897) | |
| 352564-1 3525641 | 1560-01-356-7973 | Panel, Structural, Aircraft | Lockheed Martin Corporation (98897) | ||
| 352564-3 3525643 | 1560-01-356-7973 | Panel, Structural, Aircraft | Lockheed Martin Corporation (98897) | ||
| 3-52567-19 35256719 | 1560-00-768-1044 | Cover, Access | END Item Identification: F-5 Hole Diameter: 0.250 inches minimum and 0.254 inches maximum Securing Device Type: Threaded fastener | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 3-52567-503 352567503 | 1560-00-759-6673 | Cover, Access, Aircraft | Securing Device Type: Threaded fastener FSC Application Data: Fuselage, aircraft Peripheral Shape Style: 108 oval, multi holes | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 352569-10 35256910 | 1560-00-898-6419 | Guard Assembly, Drain Tube | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Steel, MIL-S-18728 | Lockheed Martin Corporation (98897) | |
| 352569-11 35256911 | 1560-00-070-8584 | Tip Assembly, Condensate | General Characteristics Item Description: Consists of drain tube tip and pad | Lockheed Martin Corporation (98897) | |
| 352569-7 3525697 | 1560-00-859-7798 | Pad, Tube | III End Item Identification: C-130 aircraft General Characteristics Item Description: Used on tube assembly-condensate drain | Lockheed Martin Corporation (98897) | |
| 35-25735-503 3525735503 | 1560-01-060-7309 | Bracket, Structural Component, Air | Aircraft Mission Design Series: B-52 Aircraft Location: Upper bomb bay door bracket | The Boeing Company (82918) | |
| 35-25735-504 3525735504 | 1560-01-060-6698 | Bracket, Hinge Installation kit, U | III End Item Identification: B-52 acft | The Boeing Company (82918) | |
| 35-25751-501 3525751501 | 1560-01-060-6699 | Bracket, Hinge Installation kit, U | III End Item Identification: B-52 acft | The Boeing Company (81205,82918) |