Airframe Structural Components: 373114-2, 373138-1, 3-73143-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 373114-2 3731142 | 1560-01-268-0923 | Insulation, Thermal, Special Purpo | Width: 17.300 inches nominal Thickness: 0.188 inches minimum and 0.312 inches maximum Length: 21.800 inches nominal | Lockheed Martin Corporation (98897) | |
| 373114-3 3731143 | 1560-01-434-8399 | Insulation, Thermal, Special Purpo | Width: 11.100 inches nominal Thickness: 0.250 inches nominal Length: 13.600 inches nominal | Lockheed Martin Corporation (98897) | |
| 373114-300 373114300 | 1560-00-608-1524 | Insulation, Thermal, Special Purpo | Width: 22.800 inches nominal Thickness: 0.188 inches minimum and 0.312 inches maximum Length: 39.700 inches nominal | Lockheed Martin Corporation (98897) | |
| 373114-4 3731144 | 1560-01-434-8402 | Insulation, Thermal, Special Purpo | Width: 13.600 inches nominal Thickness: 0.250 inches nominal Length: 17.200 inches nominal | Lockheed Martin Corporation (98897) | |
| 373114-5 3731145 | 1560-01-265-8329 | Insulation, Thermal, Special Purpo | Width: 21.800 inches nominal Thickness: 0.187 inches minimum and 0.313 inches maximum Length: 39.700 inches nominal | Lockheed Martin Corporation (98897) | |
| 373118-1L 3731181L | 1560-01-045-4478 | Plate, Chine, Flight Deck | III End Item Identification: C-130 acft General Characteristics Item Description: Matl 7075-T6 plate, 92.0 in. lg, 12.0 in. W, 0.312 in. H, QQ-A-283 CONDT6 | Lockheed Martin Corporation (98897) | |
| 373118-1R 3731181R | 1560-01-045-4479 | Plate, Chine, Flight Deck | III End Item Identification: C-130 acft General Characteristics Item Description: Matl 7075-T6 plate, 92.0 in. lg, 12.0 in. W, 0.312 in. H, QQ-A-283 CONDT6 | Lockheed Martin Corporation (98897) | |
| 3-73123-1 3731231 | 1560-00-071-6249 | Bell Crank | Counterbore Diameter: 0.623 inches minimum and 0.624 inches maximum Counterbore Depth: 0.244 inches minimum and 0.254 inches maximum Bore Diameter: 0.560 inches nominal | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) Tect Aerospace Inc. (34336) | |
| 373126-2 3731262 | 1560-01-332-5287 | Former, Aircraft | III End Item Identification: Hercules C130E acft Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 3-73127-5 3731275 | 1560-00-682-5226 | Bracket, Bob Weight | General Characteristics Item Description: Bracket data, aluminum alloy 2024, QQ-A-250/5, angle data, aluminum alloy 7075, QQ-A-200/11 | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 373128-2 3731282 | 1560-01-332-5333 | Ring Segment, Aircraft | III End Item Identification: Hercules C130E acft General Characteristics Item Description: Aluminum alloy, QQ-A-362, 2024, cond o; size .050 X 15 X 65 in. | Lockheed Martin Corporation (98897) | |
| 373132-2 3731322 | 1560-01-332-5332 | Ring Segment, Aircraft | III End Item Identification: Hercules C130E acft General Characteristics Item Description: Aluminum alloy, QQ-A-362, 2024, cond o; size .050 X 13 X 68 | Lockheed Martin Corporation (98897) | |
| 373135-2 3731352 | 1560-01-559-2130 | Skin, Aircraft | Aircraft Mission Design Series: C-130 Material: Aluminum alloy Aircraft Location: Main landing gear wheel well panel | Lockheed Martin Corporation (98897) | |
| 373135-3 3731353 | 1560-01-559-3631 | Skin, Aircraft | III End Item Identification: C-130 acft Aircraft Mission Design Series: C-130 acft Special Features: Final cond T76511; L560345-1 X 49. | Lockheed Martin Corporation (98897) | |
| 373138-1 3731381 | 1560-00-611-9354 | Panel, Structural, Aircraft | Overall Length: 28.120 inches nominal Overall Width: 19.649 inches nominal | Lockheed Martin Corporation (98897) | |
| 373139-1 3731391 | 1560-00-611-9353 | Panel, Structural, Aircraft | III End Item Identification: C-130 Special Features: Impregnated paper, honeycomb core with laminated fiber glass facing Material: Plastic phenolic | Lockheed Martin Corporation (98897) | |
| 373140-1 3731401 | 1560-00-611-9352 | Panel, Structural, Aircraft | III End Item Identification: C-130 Special Features: Impregnated paper, honeycomb core with laminated fiber glass facing Material: Plastic phenolic | Lockheed Martin Corporation (98897) | |
| 373141-1 3731411 | 1560-01-013-4624 | Bracket Assembly, Heat Deflector | General Characteristics Item Description: 1.500 in. lg, 1.250 in. W | International Precision Inc. (3H683) Lockheed Martin Corporation (98897) | |
| 373142-1 3731421 | 1560-01-370-3953 | Bracket, Structural Component, Air | Lockheed Martin Corporation (98897) | ||
| 3-73143-1 3731431 | 1560-00-797-5475 | Link Assembly, Differential Mecha | III End Item Identification: Acft model T38 General Characteristics Item Description: Magnesium alloy, AZ91C-T6, QQ-M-56, 5.090 in. lg, 0.880 in. min, 0.920 in. max W, 0.980 in. H | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) |