FSC 5342 Weapon System - Hardware: 5342-01-128-8714, 5342-01-129-0220, 5342-01-129-0863
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5342-01-128-8714 5342011288714 | 11500GX 142433H1 1901D002 S-3067 | Latch | S & S Truck Parts Inc. (29637) Komatsu American Intl Co. (29510) Komatsu America Corp. (0SAT8) | ||
| 5342-01-128-8715 5342011288715 | M/32M-20003 1977-M/32M20003 | Support Assy | General Characteristics Item Description: Consists of front fender mtg and front bracket support | Wheeler Bros. Inc. (55683) AM General LLC (34623) | |
| 5342-01-128-8736 5342011288736 | 11500699-1 | Spacer, Hinge | III End Item Identification: 4935-01-216-6491 Test Data Document: 18876-11500699-1 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing) | Lockheed Martin Corporation (04939) U S Army Aviation and Missile (18876) | |
| 5342-01-128-8742 5342011288742 | 501-4675360 ITEM F51 | Connection | Naval Ship Systems Command (80064) | ||
| 5342-01-128-8784 5342011288784 | 2531007 | Bracket, Stop | Navair and Navsea Managed (10001) | ||
| 5342-01-128-9367 5342011289367 | J-5682-112 | Mount, Resilient, Weapon System | Height: 2.250 inches nominal (Non-Core Data) Resilient Member Material: Rubber, synthetic, btr iv, lord mfg co and steel Special Features: Internal stud 0.530 in. deep, 1/2-20 unf 2B thd | Lord Corporation (76005) | |
| 5342-01-128-9515 5342011289515 | 4692986-1 | Bracket, Ballast Tan | Naval SEA Systems Command (53711) | ||
| 5342-01-128-9527 5342011289527 | 12313106 | Mount, Muffler | U S Army Tank Automotive Command (19207) | ||
| 5342-01-128-9569 5342011289569 | 12269589 | Door, Access, Weapon System | Material: Aluminum alloy 5083 Cross-Sectional Shape Style: 26 flat End Item Identification: 1450-01-121-2122 | U S Army Tank Automotive Command (19207) | |
| 5342-01-129-0153 5342011290153 | 10236014 | Anode | Limco Airepair Inc. (16630) | ||
| 5342-01-129-0154 5342011290154 | 619-1431-001 | Bracket Assembly | General Characteristics Item Description: Consists of bracket, housing, con tact, adhesive and sleeve | Rockwell Collins Inc. (13499) | |
| 5342-01-129-0163 5342011290163 | 790-0852-001 | Cover Clamp | General Characteristics Item Description: 0.410 in. lg wall to wall; 0.130 in. w; 0.138 in. min and 0.140 in. max dia holes thru two walls; 0.337 in. h; | Rockwell Collins Inc. (13499) | |
| 5342-01-129-0183 5342011290183 | 3141650-130-1 | Handle | General Dynamics Armament and (04DG4) Nordam Group Inc., The (29957) | ||
| 5342-01-129-0190 5342011290190 | 68329CX-W | Mounting Assy | Oshkosh Corporation (45152) | ||
| 5342-01-129-0191 5342011290191 | 27160-802 | Yoke, Adjuster | UOP Inc. (71044) | ||
| 5342-01-129-0220 5342011290220 | JT139-100 | PLUG | Eaton Aviation Corporation (08118) | ||
| 5342-01-129-0222 5342011290222 | X2-10128K1105 | Button | TRW Assemblies and Fasteners Group (83058) | ||
| 5342-01-129-0469 5342011290469 | CB-1125-11 CB-1009-1 | Mount, Resilient, Weapon System | Material: Steel core (Non-Core Data) Resilient Member Material: Rubber, synthetic Maximum Load Rating: 1500.0 pounds | Lord Corporation (76005) | |
| 5342-01-129-0851 5342011290851 | 3903T72P01 | Bracket, Support | General Characteristics Item Description: Cres, ams 5540; 0.036 in. N0M thk, 0.500 in. nom W, one end, 0.250 in. nom W, other end III End Item Identification: Engine model TF34 housing | General Electric Company (99207) | |
| 5342-01-129-0863 5342011290863 | LW1764-4-1-155 3M975-4-1-155 52956A4-1-155 | Receptacle, Quick Release Pin | Special Features: Aluminum alloy QQ-A-225/9 alloy 7075-T73 or aluminum alloy QQ-A-200/11 alloy 7075-T73 or alloy 7075-T6511 body and mounting plate, aluminum alloy QQ-A-225/8 alloy 6061-T6 plunger, retaining disc and sleeve, steel QQ-W-470 spring, steel seat, anodize MIL-A-8625 body, mounting plate plunger, plunger, retaining disc and sleeve, cadmium and chromate QQ-P-416 ty 2 cl 2 spring and seat; mounting plate diamond shape 0.625 in. W by 0.062 in. thk, 1.000 in. C to C distance between two 0.128 in. dia mtg holes; 1.250 in. nom height; 0.371 in. min 0.376 in. max. dia.; for use in 0.155 in. skin W/a 0.250 in. dia pin quick release | Boeing Company, The (76301) Avibank MFG. Inc. (84256) Hartwell Corporation (83014) |