Airframe Structural Components: 362537-7L, 362546-1, 362550-1L
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 362537-7L 3625377L | 1560-01-461-1146 | Rib, Stiffener, Aircraft | Aircraft Mission Design Series: C-130B-H Material: Steel corrosion resisting Aircraft Location: Lower firewall | Lockheed Martin Corporation (98897) | |
| 362537-7R 3625377R | 1560-01-453-5654 | Stiffener, Aircraft | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) Lockheed Martin Services Inc. (1WL60) | |
| 362537-8L 3625378L | 1560-01-453-5988 | Web, Structural Component, Aircraf | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) Lockheed Martin Services Inc. (1WL60) | |
| 362537-8R 3625378R | 1560-01-453-5991 | Web, Structural Component, Aircraf | III End Item Identification: C-130 | Lockheed Martin Corporation (98897) Lockheed Martin Services Inc. (1WL60) | |
| 362537-9 3625379 | 1560-01-203-7196 | Former, Aircraft | Aircraft Mission Design Series: C-130 Special Features: 17-7PH lac 1-595 cond a Material: Steel | Lockheed Martin Corporation (98897) | |
| 362538-1L 3625381L | 1560-01-282-3695 | Longeron | Aircraft Mission Design Series: C-139 Special Features: Nha 362535-1; heat treat T4 Material: Aluminum alloy 2024 | Airborne Technologies Inc. (58730) Lockheed Martin Corporation (98897) | |
| 362538-1R 3625381R | 1560-01-374-6475 | Longeron | Aircraft Mission Design Series: C-130 Special Features: Heat treat to -T4 Material: Aluminum alloy 2024 | Lockheed Martin Corporation (98897) | |
| 362538-4 3625384 | 1560-01-453-1574 | Longeron | III End Item Identification: C130 hercules acft | Lockheed Martin Corporation (98897) | |
| 362539-1 3625391 | 1560-00-621-1234 | Door Assembly, Tank Access | III End Item Identification: Acft model C130 | Aero Engineering & Manufacturing (17772) Frazier Aviation Inc. (23162) Lockheed Martin Corporation (98897) Rohr Inc. (51563) | |
| 362539-1 3625391 | 1560-00-899-5997 | Adapter, Tube, Exhaust Duct | General Characteristics Item Description: Flange end data, cres, ams 5386, duct data, hastelloy, ams 5536, insulated, 1ST end 3.070 in. W, 6.160 in. lg outside dim., 2ND end plain tube connection 3.850 in. min, 3.910 in. max dia, 17.0 deg angle to 1ST end | Honeywell International Inc. (59364,99193) | |
| 362539-1 3625391 | 1560-01-476-2693 | Door, Aircraft | Lockheed Martin Aeronautical Systems (74703) | ||
| 362539-4 3625394 | 1560-01-481-9909 | Half Hinge | Lockheed Martin Corporation (56232) | ||
| 362540-1 3625401 | 1560-00-657-9584 | Diffuser Assembly, Preheat | General Characteristics Item Description: Aluminum alloy, QQ-A-250/5, 5.920 in. lg, 5.000 in. dia, 0.750 in. dia hole thru 8 places | Lockheed Martin Corporation (98897) Tect Aerospace Inc. (34336) | |
| 362544-1L 3625441L | 1560-00-632-0043 | Cowling | III End Item Identification: C-130 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) Mancro Aircraft Co. (31556) | |
| 362544-1R 3625441R | 1560-00-632-0044 | Cowling | III End Item Identification: C-130 Material: Aluminum alloy Material Document and Classification: QQ-A-250/5 fed spec single material response | Lockheed Martin Corporation (98897) | |
| 362544-501 362544501 | 1560-00-716-2653 | Door, Cowl, Airframe | Lockheed Martin Corporation (98897) | ||
| 362545-1 3625451 | 1560-00-652-1138 | Flange, Fireseal | General Characteristics Item Description: Cres MIL-S-5059, 30.640 in. od | Lockheed Martin Corporation (98897) | |
| 362546-1 3625461 | 1560-00-628-5482 | Spar, Aircraft | Aircraft Mission Design Series: C-130 Aircraft Location: Upper cowling Criticality Code Justification: CZEK | G. S. E. Dynamics Inc. (29183) Lockheed Martin Corporation (98897) Mancro Aircraft Co. (31556) Maven Engineering Corporation (65273) Rohr Inc. (51563) | |
| 362547-1 3625471 | 1560-00-652-7784 | Flange, Fireseal | General Characteristics Item Description: Cres MIL-S-5059, 30.930 in. od | Lockheed Martin Corporation (98897) | |
| 362549-3R 3625493R | 1560-00-657-9586 | Fitting, Hinge, Cowl Panel | General Characteristics Item Description: CRES | Lockheed Martin Corporation (98897) | |
| 3625-5 36255 | 1560-00-020-2673 | Housing, Pinion | III End Item Identification: Acft model C-7A General Characteristics Item Description: Aluminum alloy, 2014-T6, QQ-A-367 | Goodrich Aerospace Canada LTD (02121) | |
| 362550-1L 3625501L | 1560-01-204-7518 | Support, Structural Component, Air | End Item Identification: C-130 acft Special Features: Aluminum alloy 2024-T3 clad; lower firewall | A and M Aerospace Inc. (6Z800) Airborne Technologies Inc. (58730) At Aerospace Inc. (1Q1N5) Lockheed Martin Corporation (98897) |