Airframe Structural Components: 364401-1, 364427-1, 364589-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 364401-1 3644011 | 1560-00-626-9592 | Clevis, Anchor cable | General Characteristics Item Description: Steel, MIL-S-6050, 5.35 in. lg, 1.00 in. W | Lockheed Martin Corporation (98897) | |
| 364415-1 3644151 | 1560-00-602-5439 | Window Panel, Aircraft | Special Features: Thermosetting cast Material: Plastic | Lockheed Martin Corporation (98897) | |
| 364423-1L 3644231L | 1560-00-503-8291 | Stop, Paratroop Door | General Characteristics Item Description: Aluminum alloy, condition 2024-T4, LS3262, fscm 98897, 8.580 in. LG1.350 in. W | Lockheed Martin Corporation (98897) | |
| 364423-1R 3644231R | 1560-00-503-8292 | Stop, Paratroop Door | General Characteristics Item Description: Aluminum alloy, condition 2024-T4, LS3262, fscm 98897, 8.580 in. LG1.350 in. W | Lockheed Martin Corporation (98897) | |
| 364424-1L 3644241L | 1560-00-503-8293 | Stop, Paratroop Door | III End Item Identification: Acft C130 General Characteristics Item Description: Bumper assembly | Lockheed Martin Corporation (98897) | |
| 364424-1R 3644241R | 1560-00-503-8294 | Stop, Paratroop Door | Lockheed Martin Corporation (98897) | ||
| 364426-1 3644261 | 1560-01-396-2790 | Channel, Aircraft | III End Item Identification: C-130 acft Special Features: U/O aft nose landing gear door Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 364427-1 3644271 | 1560-01-300-4242 | Plate, Structural, Aircraft | III End Item Identification: C-130 Special Features: T4 Material: Aluminum alloy 6061 | Lockheed Martin Corporation (98897) QMI Aerospace Inc. (21771) | |
| 36-4500 364500 | 1560-00-777-7827 | Seal, Ejection Door | General Characteristics Item Description: Rubber, silicone, 13.300 in. min, 13.500 in. max lg, 0.090 in. dia hole thru 8 places | The Boeing Company (81205,82918) | |
| 3-64501-1 3645011 | 1560-00-153-3163 | Cover, Indexer, Angle of Attack | General Characteristics Item Description: Aluminum alloy, 5052-0, QQ-A-250-8, 7.000 in. lg, 2.520 in. W, 2.950 in. H, 4 holes 0.188 in. dia | Northrop Grumman Systems Corporation (76823) Northrop Grumman Technical Services (0JRC1) | |
| 364564-1 3645641 | 1560-01-081-1899 | Bracket Assy, Mtg to | Lockheed Martin Corporation (98897) | ||
| 36-4575 364575 | 1560-00-779-3066 | Adapter, Cross Shaft | General Characteristics Item Description: 0.750 in. lg, 0.875 in. dia, 4340 steel bar, MIL&S&5000 normalized III FSC Application Data: Airframe structural components | The Boeing Company (81205,82918) | |
| 36-4576-1 3645761 | 1560-01-154-8859 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opposite 36-4576-2 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 36-4576-2 3645762 | 1560-01-154-8860 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Special Features: Opposite 36-4576-1 Material: Aluminum alloy 2024 | The Boeing Company (81205) | |
| 36-4577 364577 | 1560-00-783-7011 | Plate Assembly, Bearing, Cowl | General Characteristics Item Description: Aluminum alloy, 2.020 in. lg O/a, 1.120 in. W O/a, 1 bushing P/N NAS77A-5-31 | The Boeing Company (81205,82918) | |
| 36-4578-501 364578501 | 1560-00-731-3626 | Plate, Bearing, Engine Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, 1.840 in.lg, 1.780 in. W, 1.100 in. H | The Boeing Company (81205,82918) | |
| 36-4578-502 364578502 | 1560-00-731-3627 | Plate, Bearing, Engine Cowl | General Characteristics Item Description: Aluminum alloy, QQ-A-200/3, 1.840 in.lg, 1.780 in. W, 1.100 in. H | The Boeing Company (81205,82918) | |
| 364581-1 3645811 | 1560-00-876-1782 | Spacer | III End Item Identification: C-130A aircraft General Characteristics Item Description: Location-leading edge rib, wing sta 160.183L and 160.302R;LENGTH-1.36 in. | Lockheed Martin Corporation (98897) | |
| 36-4585-1 3645851 | 1560-01-151-8458 | Plate, Structural, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 7075 Aircraft Location: Outboard strut skin splice | The Boeing Company (81205) | |
| 364589-1 3645891 | 1560-00-608-7697 | Bracket Assembly, Tube Support, Nl | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5 COND-0, heat treat to T4 | Lockheed Martin Corporation (98897) |