FSC 5342 Weapon System - Hardware: 5342-01-015-9789, 5342-01-016-3095, 5342-01-016-6657
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5342-01-015-9789 5342010159789 | 11684157 5340010159789 | Fairlead half, Tubular | Special Features: Plastic, laminated thermosetting ty 2 grade le or plastic, laminated /micarta grade 262/, 1.380 in.lg, 0.750 in.W, 0.420 in.H, 0.330 in.min 0.350 in.max dia mtg hole, accommodates two tubes, 0.244 in.min 0.250 in.max dia; | E.C.A Etablissement Central DES (SCY13) U S Army Tank Automotive Command (19207) | |
| 5342-01-016-0432 5342010160432 | 5340010160432 5145429 PC5145429 | CLIP | MTU Detroit Diesel Inc. (72582) E.C.A Etablissement Central DES (SCY13) General Motors Corp. (24617) | ||
| 5342-01-016-1332 5342010161332 | 63A73-020 35323 | Clamp | Walker MFG Co. (79260) TLD ACE Corporation (00365) | ||
| 5342-01-016-1334 5342010161334 | 1560-UH-1-755-1 | Fairlead, Tubular | Special Features: UH-1 series helicopter | U S Army Aviation and Missile (81996) | |
| 5342-01-016-1585 5342010161585 | 66-1361 | Arm, Galley Door | General Characteristics Item Description: Steel MIL-S-5000, 3.47 in. lg, 4.20 in. H III Fsc Application Data: Used on P-N 50-7983-182 appl E3A aircraft | The Boeing Company (81205, 17765) | |
| 5342-01-016-1591 5342010161591 | 69-47791-1 | Clevis, Nose Gear Door | General Characteristics Item Description: Steel, 2.990 in. lg, 0.500 in. W III Fsc Application Data: Airframe structural components | The Boeing Company (81205) | |
| 5342-01-016-1603 5342010161603 | 50-5316-21 | Angle, Door | The Boeing Company (81205) | ||
| 5342-01-016-1604 5342010161604 | 50-5316-22 | Angle, Door | The Boeing Company (17765, 81205) | ||
| 5342-01-016-1605 5342010161605 | 65-3792-7 | PLUG | General Characteristics Item Description: Steel wire QQ-W-423, comp FS-316; 0.250 in. lg; 0.135 in. dia min, 0.138 in. dia max | The Boeing Company (81205, 17765) | |
| 5342-01-016-3055 5342010163055 | 28002902 | Plug, Special | General Characteristics Item Description: Aluminum alloy QQ-A-225/6 alloy 2024 temper T351, 0.131 in. min 0.135 in. max lg, 0.107 in. min 0.108 in. max dia, 0.046 in. min 0.048 in. max dia groove, 0.050 in. min 0.055 in. max W groove | Woodward HRT Inc. (81873) | |
| 5342-01-016-3093 5342010163093 | 702630 | Bracket, Combustion Chamber Duct | General Characteristics Item Description: Nickel alloy AMS5596 III End Item Identification: Engine model TF30 | United Technologies Corporation (77445) | |
| 5342-01-016-3094 5342010163094 | 702632 | Bracket, Combustion Chamber Duct | General Characteristics Item Description: Nickel alloy AMS5596 III End Item Identification: Engine model TF30 | United Technologies Corporation (77445) | |
| 5342-01-016-3095 5342010163095 | 705270 | Bracket, Combustion Chamber Duct | General Characteristics Item Description: Nickel alloy AMS5596 III End Item Identification: Engine model TF30 | United Technologies Corporation (77445) | |
| 5342-01-016-3096 5342010163096 | 705340 | Bracket, Combustion Chamber Duct | General Characteristics Item Description: Nickel alloy AMS5596 III End Item Identification: Engine model TF30 | United Technologies Corporation (77445) | |
| 5342-01-016-3232 5342010163232 | D2320-300 GC550EM300 | Coupling, Clamp, Grooved | Inside Diameter: 3.350 inches nominal Material and Location: Steel, ams 5596 segment or steel ams 5597 segment iron alloy, ams 5525, comp 660 bolt or iron alloy, ams 5732, comp 660 bolt iron alloy, ams 5525, comp 660 nut or iron alloy, ams 5732, comp 660 nut Shape: Round | Northrop Grumman Systems Corporation (26512) Eaton Corporation (15284) | |
| 5342-01-016-3233 5342010163233 | GC550EM450 D2320-450 | Coupling, Clamp, Grooved | Inside Diameter: 4.850 inches nominal Material and Location: Steel, ams 5596 segment or steel ams 5597 segment iron alloy, ams 5525, comp 660 bolt or iron alloy, ams 5732, comp 660 bolt iron alloy, ams 5525, comp 660 nut or iron alloy, ams 5732, comp 660 nut Shape: Round | Eaton Corporation (15284) Northrop Grumman Systems Corporation (26512) | |
| 5342-01-016-3404 5342010163404 | BVD101-14-1 | Lock, cam | General Characteristics Item Description: Nickel plated, shell 0.625 in. lg by 0.625 in. across flats of shell, shell tapped W 3/4-24 thd, 5 disc tumblers, removable cam, 90 deg rotation to left, furnished with 2 keys | Ilco Unican Corp. (30399) | |
| 5342-01-016-4235 5342010164235 | 6888618 | Bracket | Rolls-Royce Corporation (63005) Allison Transmission Inc. (73342) | ||
| 5342-01-016-6520 5342010166520 | 460608-1 | Cap, End | General Characteristics Item Description: 0.820 in. dia, 0.060 in. thk III End Item Identification: Aircraft model E-2C | BAE Systems Information and (80249) | |
| 5342-01-016-6657 5342010166657 | 7540850-10 | Fairlead, Block | Features Provided: Split design Mounting Facility Quantity: 1 Section Quantity: 2 | Sacramento Air Logistics Center (98749) |