Airframe Structural Components: 3-84405, 385036-1, 385038-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3-84405 384405 | 1560-01-032-1974 | Plunger, Lock Suppor | The Boeing Company (81205) | ||
| 3-84438 384438 | 1560-01-004-1786 | Former, Aircraft | Overall Diameter: 1.250 inches nominal Opening Inside Diameter for Which Designed: 0.90 inches nominal Part Name Assigned BY Controlling Agency: Plug-actuator seal rudder trim control | The Boeing Company (81205,82918) | |
| 3844713-1 38447131 | 1560-01-579-1982 | Insulation, Thermal, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 | Honeywell International Inc. (99193) | |
| 3844891-2 38448912 | 1560-01-579-1984 | Insulation, Thermal, Aircraft | III End Item Identification: F-22 raptor Aircraft Mission Design Series: F-22 | Honeywell International Inc. (99193) | |
| 3-84667 384667 | 1560-01-523-5498 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: This part is 5.2" in dia.; this is for recon conversion kit unit no. 1 &on; U/O drawing number 5-62186 Material: Aluminum alloy 2024 | The Boeing Company (82918) | |
| 3-84805 384805 | 1560-00-302-5637 | Spacer, Flap link Wing Flap Drive | General Characteristics Item Description: Steel, MIL-S-18729, 1.120 in. od, 0.696 in. min, 0.716 in. max id | The Boeing Company (81205) | |
| 385018-25 38501825 | 1560-01-490-0405 | Rudder, Aircraft | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) | |
| 385019-115 385019115 | 1560-01-455-9355 | Aileron Assembly | III End Item Identification: Aircraft, model C-130J | Lockheed Martin Corporation (98897) | |
| 385019-117 385019117 | 1560-01-455-9351 | Aileron Assembly | III End Item Identification: Aircraft, model C-130J | Lockheed Martin Corporation (98897) | |
| 385019-51 38501951 | 1560-01-455-9353 | Door, Aircraft | III End Item Identification: Aircraft, model C-130J | Lockheed Martin Corporation (98897) | |
| 385029-1 3850291 | 1560-01-472-3370 | Support, Structural Component, Air | Aircraft Mission Design Series: C-130J Special Features: Opposite -2;NEXT higher assembly 385018;MAKE from material LS7055, national stock number 9540-01-437-8540;CONSIST of 2 (-3, -5) angle mount, 3 (-7, -11, -12) angle, 1 (-9) channel, 2 (-13, -15) web, 4 (-17, -19, -21, -23) brackets, 4 (-25, -27, -29, -31) clips, 4 nutplate, 4 screw, 4 washer, 4 nut, 4 lockbolt, 4 collar Aircraft Location: Used as rudder tab actuator mount assembly | Lockheed Martin Corporation (98897) | |
| 385031-1 3850311 | 1560-01-455-9684 | Fork, Aileron tab rod End | III End Item Identification: Aircraft, model C-130J General Characteristics Item Description: 4130 steel bar; tab length 0.920 in; tab width 0.620 in; rod end length 1.550 in; 0.500-20UNF-3A threaded end; slot length 0.560 in; slot width 0.190 in | Lockheed Martin Corporation (98897) | |
| 385032-1 3850321 | 1560-01-472-3369 | Tab, Trim, Aircraft | Aircraft Mission Design Series: C-130J Special Features: Next higher assembly 385018;REWORKED under part number 342241 with national stock number 1560-00-098-7964;CONSIST of 1 (-3) channel, 2 (-5, -7) splice, 2 (-9) doubler, 1 (-11) hinge, 1 (-13) weld assembly, 2 (-15, -17) beam, 1 bracket, 1 rib, 6 screw, 2 nutplate, 12 lockbolt, 12 collar, 44 rivet, 1 laminated shim Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 385033-1 3850331 | 1560-01-441-8604 | Bracket, Structural Component, Air | III End Item Identification: C-130 aircraft | Lockheed Martin Corporation (98897) | |
| 385036-1 3850361 | 1560-01-455-9356 | Rod Assembly, Aileron | III End Item Identification: Aircraft, model C-130J General Characteristics Item Description: Steel, 4130; 19.800 inch length; 0.500-20UNF-3B threaded end; 0.755/0.768 inch dia. rod end; steel bearing 0.8125 in O/a dia. at oppostite end | Lockheed Martin Corporation (98897) | |
| 385036-3 3850363 | 1560-01-534-9970 | Rod, Actuator | III End Item Identification: C130J hercules fixed wing aircraft III Part Name Assigned BY Controlling Agency: Rod, actuator control rudder | Lockheed Martin Corporation (98897) | |
| 3-85036-501 385036501 | 1560-01-149-6429 | Support, Structural Component, Air | III End Item Identification: B-52 acft (Non-Core Data) FSC Application Data: Aircraft structural component | The Boeing Company (81205) | |
| 385037-1 3850371 | 1560-01-455-9354 | Mount Assembly | III End Item Identification: Aircraft, model C-130J General Characteristics Item Description: Consists of 2 angles, 1 support, 2 clips, 1 collar, and 1 lockbolt | Lockheed Martin Corporation (98897) | |
| 385037-25 38503725 | 1560-01-455-9362 | Mount Assembly | III End Item Identification: Aircraft, model C-130J General Characteristics Item Description: Consists of 1 angle, 1 support, 3 channels, 1 collar, and 1 lockbolt | Lockheed Martin Corporation (98897) | |
| 385038-1 3850381 | 1560-01-477-3025 | Tab, Trim, Aircraft | III End Item Identification: Hercules C130J, fixed wing aircraft Special Features: Reworked from tab assy | Lockheed Martin Corporation (98897) |