Airframe Structural Components: 697989, 69-8307, 69-8362
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 697989 | 1560-01-472-8560 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-11 69798911 | 1560-01-472-8559 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-13 69798913 | 1560-01-472-8560 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-21 69798921 | 1560-01-472-8561 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-21 69798921 | 1560-01-475-6120 | Duct Assembly, Bleed Air | III End Item Identification: C-130J aircraft | Lockheed Martin Corporation (98897) | |
| 697989-3 6979893 | 1560-01-472-8562 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-5 6979895 | 1560-01-472-8564 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-7 6979897 | 1560-01-472-3157 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 697989-9 6979899 | 1560-01-472-3156 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 698000-1 6980001 | 1560-01-505-5668 | Duct Assembly, Bleed Air | III End Item Identification: Hercules aircraft, C130J | Cecom LR Center (97403) | |
| 698074-1 6980741 | 1560-01-510-3616 | Fireseal, Aircraft | Aircraft Mission Design Series: C-130J Special Features: Operational requirements include temp range of -65 deg to 1250 deg F anfire resistant to 2000 deg F for 5 mins, operating altitude of 45, 000 ft max, ambient temp -65 deg F to 250 deg F Material: Glass borosilicate | Lockheed Martin Corporation (98897) | |
| 698076-21 69807621 | 1560-01-477-5235 | Panel, Structural, Aircraft | III End Item Identification: Hercules C130J, fixed wing aircraft III Part Name Assigned BY Controlling Agency: Panel, insulated | Lockheed Martin Corporation (98897) | |
| 698076-23 69807623 | 1560-01-573-8445 | Panel, Structural, Aircraft | Aircraft Mission Design Series: C-130J Special Features: Nha is fadec/niu enclosure III Part Name Assigned BY Controlling Agency: Panel, insulated | Lockheed Martin Corporation (98897) | |
| 698076-25 69807625 | 1560-01-538-8807 | Panel, Insulated | III End Item Identification: C130J hercules aircraft, uk modification | Lockheed Martin Corporation (98897) | |
| 698078-3 6980783 | 1560-01-477-5243 | Panel, Structural, Aircraft | III End Item Identification: Hercules C130J, fixed wing aircraft Special Features: Edgelighted Aircraft Location: Adsparachute select assy | Lockheed Martin Corporation (98897) | |
| 698087-1 6980871 | 1560-01-437-0301 | Compensator, Bellows | Material: Nickel alloy General Characteristics Item Description: Seal type joint type pressured balanced (low pressure) in line bleed air ducting system compensators, intended use in absorb axial variations in duct length caused by temperture and dimensional tolerances of the structure and ducts, location outer wing leading edge Overall Length: 18.000 inches nominal | Lockheed Martin Corporation (98897) | |
| 698087-6 6980876 | 1560-01-472-5742 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 698088-25 69808825 | 1560-01-472-3638 | Duct Assembly, Bleed Air | Lockheed Martin Corporation (98897) | ||
| 698118-7 6981187 | 1560-01-483-3096 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C-130J | Lockheed Martin Corporation (98897) | |
| 69-8307 698307 | 1560-01-019-8156 | Shaft, Release, Emerg | The Boeing Company (81205) | ||
| 69-8362 698362 | 1560-01-020-4025 | Support, Structural Component, Air | Aircraft Mission Design Series: E-3A Aircraft Location: Grd door release torque tube | The Boeing Company (81205) |