Airframe Structural Components: 353614-13L, 353626-3, 353626-8
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 353614-13L 35361413L | 1560-00-032-6616 | Striker, Ramp | III End Item Identification: Aircraft model C130 | Airborne Technologies Inc. (58730) Lockheed Martin Corporation (98897) | |
| 353614-13R 35361413R | 1560-00-032-6575 | Striker, Ramp | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
| 353614-17L 35361417L | 1560-00-182-7188 | Support Striker, Ramp Beam | General Characteristics Item Description: Aluminum alloy QQ-A-250/11, condition 0, 0.090 in. thk | Lockheed Martin Corporation (98897) | |
| 353614-17R 35361417R | 1560-00-182-7189 | Support Striker, Ramp Beam | General Characteristics Item Description: Aluminum alloy QQ-A-250/11, condition 0, 0.090 in. thk | Airborne Technologies Inc. (58730) Lockheed Martin Corporation (98897) | |
| 353614-18L 35361418L | 1560-01-339-0064 | Striker, Airframe | III End Item Identification: CC130E hercules acft General Characteristics Item Description: Aluminum alloy 6064-0 | Lockheed Martin Corporation (98897) | |
| 353614-18R 35361418R | 1560-01-253-8604 | Striker Ramp, Side Beam | Special Features: Heat treatment O-annealed;shape style is es angle; left side flange thickness is 0.090 inches nominal; base flange thickness is 0.090 inches nominal; left inside angle is 45.0 degrees; first and second tip styles are square ends Material: Aluminum Overall Length: 36.000 inches nominal | LMI Aerospace Inc. (98465) Lockheed Martin Corporation (98897) | |
| 353614-21 35361421 | 1560-01-521-0691 | Beam, Aircraft | Aircraft Mission Design Series: C130J Material: Aluminum Side FOR Which Designed: Both sides | Lockheed Martin Corporation (98897) | |
| 353614-22 35361422 | 1560-01-521-0690 | Beam, Aircraft | Aircraft Mission Design Series: C130J Material: Aluminum Side FOR Which Designed: Both sides | Lockheed Martin Corporation (98897) | |
| 353617-5 3536175 | 1560-00-731-9714 | Leading Edge, Ramp | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
| 353624 | 1560-01-394-0106 | Fitting, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel Aircraft Location: Crew entry door | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | |
| 353625-4 3536254 | 1560-01-393-8874 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel comp 4130 Aircraft Location: Crew entry door | Lockheed Martin Corporation (98897) | |
| 353625-5 3536255 | 1560-01-393-8875 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel comp 4130 Aircraft Location: Crew entry door | Lockheed Martin Corporation (98897) | |
| 353625-6 3536256 | 1560-01-394-3891 | Sleeve, Crew Door | III End Item Identification: C-130H aircraft Special Features: Used on crew entry door assembly Material: Steel | Lockheed Martin Corporation (98897) | |
| 353625-7 3536257 | 1560-01-394-0107 | Sleeve, Aircraft Door | III End Item Identification: C-130H aircraft Special Features: Telescoping sleeve on crew entry door Material: Steel | Airborne Technologies Inc. (58730) Lockheed Martin Corporation (98897) | |
| 353625-9 3536259 | 1560-01-393-6950 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H aircraft Material: Steel comp 4130 Aircraft Location: Crew entry door | Lockheed Martin Corporation (98897) | |
| 353626-3 3536263 | 1560-00-523-8578 | Tube Assy, Crew Door | Lockheed Martin Corporation (98897) | ||
| 353626-4 3536264 | 1560-00-536-3530 | Tube Assembly, Crew | General Characteristics Item Description: 21.310 in. O/a lg, consists of steel alloytube, MIL-T-6736 type 1 cond N, and two sleeves | Lockheed Martin Corporation (98897) | |
| 353626-6 3536266 | 1560-01-393-6946 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel Aircraft Location: Crew entry door fuselage | Lockheed Martin Corporation (98897) | |
| 353626-7 3536267 | 1560-01-393-8876 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel Aircraft Location: Crew entry door | Lockheed Martin Corporation (98897) | |
| 353626-8 3536268 | 1560-01-393-9171 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130H Material: Steel Aircraft Location: Crew entry door | Aero Engineering & Manufacturing (17772) Airborne Technologies Inc. (58730) Lockheed Martin Corporation (98897) |