Airframe Structural Components: 371915-7, 371949-1, 371988-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 371915-7 3719157 | 1560-01-386-4923 | Plate, Structural, Aircraft | III End Item Identification: C-130 hercules airplane. Aircraft Mission Design Series: C-130B and SC-130B Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 371915-8 3719158 | 1560-01-386-4857 | Plate, Structural, Aircraft | III End Item Identification: C-130 hercules airplane. Aircraft Mission Design Series: C-130B and SC-130B Special Features: Doubler, heat treat per T3, color; medium gray-federal standard 595 color 36231 | Lockheed Martin Corporation (98897) | |
| 371915-9 3719159 | 1560-01-386-5016 | Panel, Structural, Aircraft | III End Item Identification: C-130 hercules airplane. Aircraft Mission Design Series: C-130B and SC-130B Special Features: Heat treat per T4, nha; 382996, 370463-3 | Lockheed Martin Corporation (98897) | |
| 371920-1 3719201 | 1560-00-671-8971 | Bracket Assy, Power | Lockheed Martin Corporation (98897) | ||
| 371945-1 3719451 | 1560-00-621-7822 | Bracket, Upper Control Pulley | General Characteristics Item Description: Magnesium alloy, QQ-M-56, 15.230 in. lg | Lockheed Martin Corporation (98897) | |
| 371945-3 3719453 | 1560-00-283-8475 | Bracket Assembly, Upper Control P | General Characteristics Item Description: Aluminum alloy, alloy 356, temper T6, QQ-A-601 | Lockheed Martin Corporation (98897) | |
| 371949-1 3719491 | 1560-01-438-8194 | Bracket, Structural Component, Air | Aircraft Location: Flap control, rear beam Side FOR Which Designed: Left side | Lockheed Martin Corporation (98897) | |
| 371950-2 3719502 | 1560-00-612-8035 | Tube Assembly, Rudder | General Characteristics Item Description: Applicable to model C-130 aircraft | Lockheed Martin Corporation (98897) | |
| 371950-3 3719503 | 1560-00-611-9377 | Tube Assembly, Rudder | General Characteristics Item Description: Applicable to model C-130 aircraft | Lockheed Martin Corporation (98897) | |
| 371960-2 3719602 | 1560-00-625-8547 | Latch, Idler, Rudder Pedal | General Characteristics Item Description: Steel, MIL-S-6050, 0.190 in. min, 0.192 in. max dia hole 1 end, 0.385 in. min, 0.392 in. max dia hole thru opposite end | Lockheed Martin Corporation (98897) | |
| 371967-1 3719671 | 1560-00-612-8070 | Piston, Rudder Pedal | General Characteristics Item Description: Plastic, MIL-P-79 type fbg, 1.125 in. dia, 0.64 in. lg | Lockheed Martin Corporation (98897) | |
| 371968-1 3719681 | 1560-00-612-8071 | Guide, Rudder Pedal | Lockheed Martin Corporation (98897) | ||
| 371969-1 3719691 | 1560-00-612-8072 | Rod Assy, Rudder Ped | Lockheed Martin Corporation (98897) | ||
| 371970-1 3719701 | 1560-00-612-8096 | Support, Structural Component, Air | Special Features: Aluminum alloy, QQ-A-225/6, 2.200 in. lg, 1.400 in. W, 1.020 in. H, 4 holes 0.221 in. dia, 2 holes 0.189 in. dia | Lockheed Martin Corporation (98897) | |
| 371971-1 3719711 | 1560-00-621-7829 | Support, Structural Component, Air | III End Item Identification: Aircraft model C130 Special Features: Aluminum alloy, QQ-A-225/6, 4.180 in. lg | Lockheed Martin Corporation (98897) | |
| 371976-1 3719761 | 1560-00-612-8094 | Rod, Guide, Rudder Pedal | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Steel, MIL-S-6050, 6.446 in. lg, 0.313 in. dia, both ends threaded 1/4-28UNF-3A | Frazier Aviation Inc. (23162) Lockheed Martin Corporation (98897) | |
| 371985-1L 3719851L | 1560-00-611-0333 | Lever, Rudder Brake Pedal | General Characteristics Item Description: Aluminum alloy, QQ-A-367, AN201KP4A pivot bearing pressed in 1 place, AN200K54 bearing pressed in 1 end | Lockheed Martin Corporation (98897) | |
| 371985-1R 3719851R | 1560-00-611-0334 | Lever, Rudder Brake | Lockheed Martin Corporation (98897) | ||
| 371986-1 3719861 | 1560-00-611-0335 | Bracket Assy, Parkin | Lockheed Martin Corporation (98897) | ||
| 371988-1 3719881 | 1560-00-611-0324 | Lever, Rudder Pedal Brake | General Characteristics Item Description: Aluminum alloy, QQ-A-367, 11.190 in. lg, 0.314 in. min, 0.315 in. max dia hole thru 1 end | Lockheed Martin Corporation (98897) |