Airframe Structural Components: 371517-13, 371548-1, 371558-7
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 371517-13 37151713 | 1560-01-438-8782 | Tube Assy, Flap | Material: Steel | Lockheed Martin Corporation (98897) | |
| 371517-7 3715177 | 1560-01-258-3139 | Shaft Assy, Flap Drive Torque out | General Characteristics Item Description: Consists of 2 rivets P/N NAS529-8-16 and 2 rivets P/N NAS529-8-18 and 4 collars P/N NAS528-A8 and 1 -13 tube assy and 1 joint P/N MS20271B16 and 1 spline fitting P/N 389709-5 | Lockheed Martin Corporation (98897) | |
| 371518-1 3715181 | 1560-00-623-6518 | Shaft, Flap Drive | III End Item Identification: Aircraft model C130 General Characteristics Item Description: 81.650 in. lg | A and M Aerospace Inc. (6Z800) Lockheed Martin Corporation (98897) | |
| 371520-5 3715205 | 1560-00-659-0367 | Shaft, Flap Drive | End Item Identification: Aircraft model C130 General Characteristics Item Description: Steel, 9.690 in. lg | Lockheed Martin Corporation (98897) | |
| 371520-7 3715207 | 1560-00-659-0368 | Shaft, Flap Drive | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Steel, 68.800 in. lg | International Precision Inc. (3H683) Lockheed Martin Corporation (98897) | |
| 371522-11 37152211 | 1560-01-438-8793 | Control Assy, Flap | III End Item Identification: Lockheed C130J hercules aircraft | Lockheed Martin Corporation (98897) | |
| 371522-5 3715225 | 1560-00-886-4855 | Control Assy, Flap D | Lockheed Martin Corporation (98897) | ||
| 371522-601 371522601 | 1560-00-652-9685 | Control Assembly, Flap Drive | End Item Identification: Aircraft model C-130 | Lockheed Martin Corporation (98897) | |
| 371522-9 3715229 | 1560-01-521-0556 | Control Assembly, Flap Drive | III End Item Identification: C130J | Lockheed Martin Corporation (98897) | |
| 371523-1 3715231 | 1560-01-438-8799 | Support Assy, Torque Shaft | Material: Aluminum alloy Overall Length: 7.420 inches nominal Overall Width: 3.720 inches nominal | Lockheed Martin Corporation (98897) | |
| 371523-2 3715232 | 1560-01-008-4320 | Support Assembly, Torque Shaft | General Characteristics Item Description: 3.820 in. W, 7.420 in. lg | Lockheed Martin Corporation (98897) | |
| 371524-1 3715241 | 1560-00-623-6521 | Cover Assembly, Flap Drive Contro | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Aluminum alloy, QQ-A-250/11, 7.025 in. dia, 2.540 in. D | Lockheed Martin Corporation (98897) | |
| 371529-3 3715293 | 1560-00-659-1298 | Coupling Assembly, Flap Drive | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) Tect Aerospace Inc. (34336) | |
| 371536-11 37153611 | 1560-01-010-3450 | Retainer Assembly, Control cable | General Characteristics Item Description: 2.000 in. lg, 2.000 in. W | Aero Engineering & Manufacturing (17772) Lockheed Martin Corporation (98897) | |
| 371536-5 3715365 | 1560-00-772-1554 | Retainer Assembly, Center Wing Co | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Plastic, MIL-P-15035, 2.000 in. lg, 2.000 in. W, 0.250 in. thk, 1 hole 0.284 in. dia, 4 holes 0.267 in. dia | A and M Aerospace Inc. (6Z800) Aero Engineering & Manufacturing (17772) Falcon Manufacturing Corp. (0HM72) Lockheed Martin Corporation (98897) | |
| 371548-1 3715481 | 1560-00-772-1553 | Retainer Assembly, Center Wing Co | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Plastic, MIL-P-15035, 2.300 in. lg, 1.660 in. W, 0.250 in. thk, 1 hole 0.284 in. dia, 4 holes 0.267 in. dia | Lockheed Martin Corporation (98897) | |
| 371548-11 37154811 | 1560-01-010-3451 | Retainer Assembly, Control cable | General Characteristics Item Description: 2.500 in. lg, 1.660 in. W | Lockheed Martin Corporation (98897) | |
| 371548-5 3715485 | 1560-00-772-1553 | Retainer Assembly, Center Wing Co | III End Item Identification: Aircraft model C130 General Characteristics Item Description: Plastic, MIL-P-15035, 2.300 in. lg, 1.660 in. W, 0.250 in. thk, 1 hole 0.284 in. dia, 4 holes 0.267 in. dia | Lockheed Martin Corporation (98897) | |
| 371558-5 3715585 | 1560-01-385-3160 | Channel, Aircraft | III End Item Identification: SC-130B and C-130B hercules airplane. Special Features: Trough used as a fuel drain passage at center wing area Material: Aluminum alloy 5052 | Lockheed Martin Corporation (98897) | |
| 371558-7 3715587 | 1560-01-384-1405 | Trough-Fuel Drain | III End Item Identification: SC-130B and C-130B Special Features: Matt spec QQ-A-318, nha 371576-1, 370505-1, located center wing General Characteristics Item Description: Aluminum alloy 5052-0, 74.990 in. lg, | Lockheed Martin Corporation (98897) |