Airframe Structural Components: 3943122-1, 3-94568, 394665-1
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 3943122-1 39431221 | 1560-01-078-7737 | Bell Crank | Bore Diameter: 0.374 inches minimum and 0.375 inches maximum Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 1.220 inches nominal 2ND end Center to Center Distance Between Fulcrum and Arm End Hole/Slot/Ball: 2.218 inches nominal 1ST end | Boeing Company, The (88277) | |
| 3943143-1 39431431 | 1560-01-082-7334 | Bracket, Support | III End Item Identification: A-4B aircraft General Characteristics Item Description: Aluminum QQ-A-250/11, alloy 6061-0 | Boeing Company, The (88277) | |
| 3943143-2 39431432 | 1560-01-082-7333 | Bracket, Support | III End Item Identification: A-4B aircraft General Characteristics Item Description: Aluminum QQ-A-250/11, alloy 6061-0 | Boeing Company, The (88277) | |
| 3943177-1 39431771 | 1560-01-057-4363 | Support, Landing Gear | III End Item Identification: Aircraft model A-4 General Characteristics Item Description: Aluminum alloy | Boeing Company, The (88277) | |
| 3943177-2 39431772 | 1560-01-057-4364 | Support, Landing Gear | III End Item Identification: Aircraft model A-4 General Characteristics Item Description: Aluminum alloy | Boeing Company, The (88277) | |
| 3943177-501 3943177501 | 1560-01-057-4365 | Support, Landing Gea | Boeing Company, The (88277) | ||
| 3-94328 394328 | 1560-01-465-4463 | Filler, Plate | III End Item Identification: Bo mmac | The Boeing Company (82918) | |
| 3-94351 394351 | 1560-00-334-5858 | Plate, Structural, Aircraft | The Boeing Company (81205) | ||
| 3-94352 394352 | 1560-01-050-5137 | Plate, Serrated | III End Item Identification: Aircraft model KC-135 | The Boeing Company (81205) | |
| 39-4408-1 3944081 | 1560-01-190-4982 | Former, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Overall Length: 1.150 inches nominal | The Boeing Company (81205,82918) | |
| 39-4408-2 3944082 | 1560-01-190-4981 | Former, Aircraft | Aircraft Mission Design Series: B-52 Material: Aluminum alloy 2024 Overall Length: 1.150 inches nominal | The Boeing Company (82918) | |
| 39-4409-1 3944091 | 1560-01-190-0583 | Support, Structural Component, Air | III End Item Identification: Acft model B-52 Special Features: Al alloy clad sheet 2024-T3 per QQ-A-362; finish F-2.115; 4.100 in. lg, 2.000 in. W, 0.064 in. thk; nha 35-2635 and 35-2689 III Supplementary Features: Functional description:used as spoiler stiffener bracket | Allfab Aerospace Corporation (30819) Machine Tool Enterprises Inc. (6Z375) Manufacturing Development Inc. (3U186) MIL-Craft Mfg. Inc. (50036) The Boeing Company (81205,82918) | |
| 39-4409-2 3944092 | 1560-01-190-0582 | Support, Structural Component, Air | III End Item Identification: Acft model B-52 Special Features: Al alloy clad sheet 2024-T3 per QQ-A-362; finish F-2.115; 3.70 in. lg, 2.000 in. W, 0.064 in. thk; nha 35-2635 and 35-2689 III Supplementary Features: Functional description:used as spoiler siffener bracket | The Boeing Company (82918) | |
| 394539-1 3945391 | 1560-00-790-4518 | Fitting, Cargo Floor | III End Item Identification: Aircraft model C130 | Lockheed Martin Corporation (98897) | |
| 3-94566-1 3945661 | 1560-01-543-3158 | Plate, Structural, Aircraft | III End Item Identification: KC-135 Aircraft Mission Design Series: KC-135 Special Features: Heat treat T3; opposite -2 | The Boeing Company (81205) | |
| 3-94566-2 3945662 | 1560-01-543-3166 | Plate, Structural, Aircraft | III End Item Identification: KC-135 Aircraft Mission Design Series: KC-135 Special Features: Opposite -1; heat treat T3 | The Boeing Company (81205) | |
| 3-94568 394568 | 1560-01-580-9425 | Support, Structural Component, Air | III End Item Identification: KC-135 Aircraft Mission Design Series: KC-135 acft Special Features: T6 extr BAC-1514-487 X 2.4; optional 2024 -T4 extr QQ-A-267 T4 temper; finish F-2.30 | The Boeing Company (81205) | |
| 39-4605 394605 | 1560-00-778-5383 | Drain Assembly, Flange | III End Item Identification: Aircraft model B52 General Characteristics Item Description: Aluminum alloy, QQ-A-250/2 comp 3003 temper H14, 2.160 in. O/a od, 0.365 in. min, 0.385 in. max id, 1.030 in. O/a lg | The Boeing Company (81205,82918) | |
| 39-4644-501 394644501 | 1560-00-650-5074 | Link Assembly, Tank Strap | General Characteristics Item Description: Aluminum alloy, QQ-A-250/13, 2.010 in. lg, 0.437 in. min, 0.439 in. max dia hole 1 in line 2 places first end, 0.437 in. min, 0.439 in. max dia hole 1 in line 2 places second end | The Boeing Company (81205,82918) | |
| 394665-1 3946651 | 1560-01-311-0447 | Guard Assembly | Airborne Technologies Inc. (58730) | ||
| 394665-1 3946651 | 1560-01-472-3482 | Bracket, Structural Component, Air | Lockheed Martin Corporation (98897) |