Airframe Structural Components: 37914, 37E52560-2, 37E52561-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 37914 | 1560-00-204-6273 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | American Fuel Cell and Coated (05476) | |
| 37915 | 1560-00-204-6266 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | American Fuel Cell and Coated (05476) | |
| 37916 | 1560-00-204-6267 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | American Fuel Cell and Coated (05476) | |
| 37917 | 1560-00-204-6269 | Foam Assembly, Fuel Tank | III End Item Identification: Aircraft model F4 | American Fuel Cell and Coated (05476) | |
| 37943 | 1560-00-446-6332 | Cap, Filler Opening | Gripping Accommodation Type: Handle Outside Diameter: 3.471 inches nominal Overall Height: 2.000 inches nominal | Parker-Hannifin Corporation (99321) | |
| 37945 | 1560-00-009-2295 | Tank, Fuel, Aircraft | III End Item Identification: OH-58A and OH-58C | American Fuel Cell and Coated (05476) | |
| 37945 | 1560-00-152-3455 | Tank, Fuel, Aircraft | Special Features: Rubber, 31.310 in. H, 32.510 I, N. lg, 51.120 in. W Reference Number Differentiating Characteristics: As differentiated by source control dwg no. 206-062-602 | American Fuel Cell and Coated (05476) | |
| 37965 | 1560-00-235-4584 | Tank, Fuel, Aircraft | Special Features: Self-sealing portion per MIL-T-5578, non self-sealing portion per MIL-T-6396 | American Fuel Cell and Coated (05476) | |
| 3797270 | 1560-01-235-6866 | Support, Structural Component, Air | Material: Aluminum alloy 6061 Material Document and Classification: QQ-A-250/11 fed spec single material response Overall Length: 2.570 inches nominal | Raytheon Company (82577) Standard Metal Products Inc. (5P435) | |
| 37B61112-1 37B611121 | 1560-00-563-6671 | Plug, Generator Moun | III End Item Identification: Aircraft model F84 | Northrop Grumman Systems Corporation (26512) | |
| 37E50001-1 37E500011 | 1560-00-217-6627 | Door Assy | Northrop Grumman Systems Corporation (26512) | ||
| 37E52498-1 37E524981 | 1560-00-505-7502 | Bushing, Stabilizer | General Characteristics Item Description: Aluminum bronze, AMS4640, 0.940 in. lg, 1.760 in. od | Northrop Grumman Systems Corporation (26512) | |
| 37E52501-1 37E525011 | 1560-00-216-4591 | Stabilizer, Horizontal | Material: Aluminum alloy | Northrop Grumman Systems Corporation (26512) | |
| 37E52501-7 37E525017 | 1560-00-328-4337 | Stabilizer Assy, man | Northrop Grumman Systems Corporation (26512) | ||
| 37E52548-1 37E525481 | 1560-00-547-2666 | Strip, Trailing Edge | Northrop Grumman Systems Corporation (26512) | ||
| 37E52551-35 37E5255135 | 1560-00-327-3526 | Clip, Maneuvering St | General Characteristics Item Description: Aluminum alloy, QQ-A-281 | Northrop Grumman Systems Corporation (26512) | |
| 37E52560-1 37E525601 | 1560-00-216-4594 | Tip, Aircraft | Aircraft Mission Design Series: F-84 aircraft Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 37E52560-1-1 37E5256011 | 1560-00-313-0182 | Tip, Aircraft | Aircraft Mission Design Series: F-84 acft Material: Aluminum alloy 2024 Material Document and Classification: QQ-A-250/5 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 37E52560-2 37E525602 | 1560-00-216-4595 | Tip Assembly, Maneuv | Northrop Grumman Systems Corporation (26512) | ||
| 37E52560-2-1 37E5256021 | 1560-00-304-9853 | Tip Assembly, Maneuv | Northrop Grumman Systems Corporation (26512) | ||
| 37E52561-1 37E525611 | 1560-00-025-6031 | Tip, Aircraft | Aircraft Mission Design Series: F-84 aircraft Special Features: Made from molded plastic, MIL-M-14 | Northrop Grumman Systems Corporation (26512) |