Airframe Structural Components: 3305072-9, 3305079-1, 3305159-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3305072-9 33050729 | 1560-01-436-8871 | Panel, Cabin Air Outlet | III End Item Identification: C130-J hercules Material: Aluminum alloy General Characteristics Item Description: Oval shape, 27 holes 0.143/0.149 in. dia around outside of panel, 26 holes 0.515/0.524 in. dia around inside of panel | Lockheed Martin Corporation (98897) | |
| 3305074-1 33050741 | 1560-01-436-9644 | Wedge, Cabin Air Outlet | III End Item Identification: C130-J hercules Material: Aluminum alloy General Characteristics Item Description: Material spec QQ-A-225/6 alloy 2024-T351, wedge taper down to .160 raduis, backward letter C cutout on wide width end of 0.500 in. with .320 in. raduis, 0.500 in. dia hole spaced 1.34 along length from wide width to center of hole, finish color code no. 34424 | Lockheed Martin Corporation (98897) | |
| 3305076-1 33050761 | 1560-01-433-1962 | Support Duct, Empennage | Material: Aluminum alloy Overall Length: 4.760 inches nominal Overall Height: 5.150 inches nominal | Lockheed Martin Corporation (98897) | |
| 3305078-1 33050781 | 1560-01-432-9968 | Duct Assembly, Empennage | Material: Steel corrosion resisting Overall Length: 80.000 inches nominal Overall Diameter: 3.000 inches nominal | Lockheed Martin Corporation (98897) | |
| 3305079-1 33050791 | 1560-01-432-9628 | Duct Assembly, Bleed Air | Aircraft Mission Design Series: C130-J Material: Steel comp 347 and steel comp 321 Aircraft Location: Fuselage station | Lockheed Martin Corporation (98897) | |
| 3305084-1 33050841 | 1560-01-535-9018 | Angle, Installation | III End Item Identification: C130 General Characteristics Item Description: Inspection of wing-to-fuselage attach angle fitting III Functional Description: Center wing sta 61.625 | Lockheed Martin Corporation (98897) | |
| 3305084-2 33050842 | 1560-01-535-9023 | Angle, Installation | III End Item Identification: C130 General Characteristics Item Description: Inspection of wing-to-fuselage attach angle fitting III Functional Description: Center wing sta 61.625 | Lockheed Martin Corporation (98897) | |
| 3305108-2 33051082 | 1560-01-542-5574 | Longeron | III End Item Identification: Used on C-130 hercules aircraft Special Features: Longeron splice bar, 434 steel Material: Steel | Lockheed Martin Corporation (98897) | |
| 3305108-3 33051083 | 1560-01-564-6608 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-130 Special Features: Dim. are stock material Material: Steel comp 4340 | Lockheed Martin Corporation (98897) | |
| 3305108-4 33051084 | 1560-01-564-9187 | Fitting, Structural Component, Air | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130 aircraft Special Features: Make from -992; cond F-2 | Lockheed Martin Corporation (98897) | |
| 3305109-2 33051092 | 1560-01-542-5575 | Plate, Structural, Aircraft | Aircraft Mission Design Series: C-130 Material: Steel comp 4340 Aircraft Location: Longeron splice | Lockheed Martin Corporation (98897) | |
| 3305109-3 33051093 | 1560-01-567-5451 | Fitting, Structural Component, Air | III End Item Identification: C-130 aircraft Aircraft Mission Design Series: C-130 Special Features: 4340 steel per AMS-S-5000;HEAT treat to 160, 000-180, 000 psi | Lockheed Martin Corporation (98897) | |
| 3305109-4 33051094 | 1560-01-564-9987 | Fitting, Structural Component, Air | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130 aircraft Special Features: Forginf m/F -992; finish C-1; cond F-2 | Lockheed Martin Corporation (98897) | |
| 3305110-2 33051102 | 1560-01-542-8782 | Fitting, Structural Component, Air | Lockheed Martin Corporation (98897) | ||
| 3305149-17 330514917 | 1560-01-439-1211 | Bracket, Structural Component, Air | III End Item Identification: Hercules C130J acft Aircraft Mission Design Series: C130J Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3305149-27 330514927 | 1560-01-439-1212 | Bracket, Structural Component, Air | III End Item Identification: Hercules C130J acft Aircraft Mission Design Series: C130J Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3305149-3 33051493 | 1560-01-439-1213 | Bracket, Structural Component, Air | III End Item Identification: Hercules C130J acft Aircraft Mission Design Series: C130J Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3305159-1 33051591 | 1560-01-006-7409 | Bar, Longeron Splice | General Characteristics Item Description: 22.400 in. lg, 3.440 in. W | Lockheed Martin Corporation (98897) | |
| 3305159-2 33051592 | 1560-01-564-9453 | Fitting, Structural Component, Air | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130 aircraft Special Features: Bar, m/F -992 forging from -994; cond E-2; | Lockheed Martin Corporation (98897) | |
| 3305159-3 33051593 | 1560-01-564-9180 | Fitting, Structural Component, Air | III End Item Identification: C-130 aircraft Aircraft Mission Design Series: C-130 acft Special Features: Cond E-2 forging; make from -995 | Lockheed Martin Corporation (98897) |