FSC 5342 Weapon System - Hardware: 5342-01-035-1321, 5342-01-035-3394, 5342-01-035-6984
| NSN | MFG SKU | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 5342-01-035-1321 5342010351321 | 10281359-2 | Ring, Rubber | General Characteristics Item Description: Material silicone, rubber, grade 60 DIAMETER5.280 inches | Precision Specialty Corp. (8A549) U S Army Aviation and Missile (18876) | |
| 5342-01-035-1497 5342010351497 | 6711 | Boot, Sound Coupling | Longwood Elastomers Inc. (6T589) | ||
| 5342-01-035-1755 5342010351755 | A-A-52506SLTB82 A-A-52506 94143-0400 5147911 PC5147911 | Clamp | MTU Detroit Diesel Inc. (72582) Power Components Deutschland GMBH (C7432) Clampco Products Inc. (54646) | ||
| 5342-01-035-1762 5342010351762 | 6600004-502 | Bracket | Gichner Systems Group Inc. (16128) | ||
| 5342-01-035-1763 5342010351763 | 5600266-501 | Strut Assembly | Gichner Systems Group Inc. (16128) | ||
| 5342-01-035-1765 5342010351765 | 1848L019 | Shaft | Goodrich Corp. (17576) | ||
| 5342-01-035-1999 5342010351999 | 758109 | Plate, Airframe Bracket | General Characteristics Item Description: Steel, ams 5504, 0.790 in. H, 2.394 in. W, 0.128 in. min, 0.152 in. maxthk, 2 mtg holes, 0.276 in. min, 0.286IN. max dia of holes, 1.400 in. C to cmtg holes | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 5342-01-035-2012 5342010352012 | 762798 | Bracket, Engine | General Characteristics Item Description: Steel, corrosion resistant, ams 5663, hardness rc 36 III End Item Identification: Acft engine TF-30 | United Technologies Corporation (77445) Turbo Power & Marine System Inc. (11449) | |
| 5342-01-035-2543 5342010352543 | 02245-4016 | Bracket, Double Pulley | General Characteristics Item Description: Aluminum alloy, QQ-A-601, 5.500 1N. W O/a | Science Applications International (79343) Harsco Corp. (93568) | |
| 5342-01-035-2948 5342010352948 | CRN2545-1 21A25029 2613242-1 | Adapter, Panel | General Characteristics Item Description: Aluminum 2011-T3, components O-rings 2, lock ring 1, panel adapter 1, 1.460 in. O/a lg, 0.860 in. O/a W, connecting end 1.188 in. 18 UNEF-2A thread | Joslyn Sunbank Company LLC (07418) Icore International Inc. (05593) Alliant Techsystems Inc. (06424) | |
| 5342-01-035-3394 5342010353394 | A24626-1 | Rod Turnbuckle | Tiffin Parts LLC (13841) | ||
| 5342-01-035-4264 5342010354264 | 8352257 | Mount, Resilient, Weapon System | Height: 2.750 inches nominal Style Designator: 77 round W/one threaded stud Maximum Load Rating: 1840.0 pounds | U S Army Tank Automotive Command (19207) | |
| 5342-01-035-4747 5342010354747 | 1274161-1 127416-1 | Clip, Special | Honeywell Intl Inc. Defense Avionics (19315) Honeywell International Inc. (96774) Honeywell Intl Inc. (55972) | ||
| 5342-01-035-5574 5342010355574 | 767831 | Bracket, Support | General Characteristics Item Description: Cres AMS5613, 2.875 in. lg | United Technologies Corporation (77445) | |
| 5342-01-035-5578 5342010355578 | 768765 | Bracket, Fuel Pump | General Characteristics Item Description: Cres ams 5613, 5.825 in. min, 5.835 in. max lg | United Technologies Corporation (77445) | |
| 5342-01-035-5586 5342010355586 | 768773 | Clevis, Fuel Pump Inlet | General Characteristics Item Description: Cres AMS5613, cadmium plate ams 2400, rockwell scale C 30-38, 2.942 IN9 lg, 0.680 in. W | United Technologies Corporation (77445) | |
| 5342-01-035-5587 5342010355587 | 768772 | Clevis, Fuel Pump Inlet | General Characteristics Item Description: Cres AMS5613, cadmium plate ams 2400, 2.592 in. lg, 2.368 in. W | United Technologies Corporation (77445) | |
| 5342-01-035-6388 5342010356388 | 332 | Hinge, Pivot | General Characteristics Item Description: Steel, 1.719 in. lg 0.750 in. W first leaf, 2.188 in. lg 0.958 in. W second leaf, 0.083 in. matl thk, for 0.750 in. or 0.875 in. doors that completely overlap the frame, elongated screw holes on all leaves for vertical and horizontal adjustment, use with vertical stile | Stanley Hardware Co. Inc. (87541) | |
| 5342-01-035-6431 5342010356431 | 4371-712M N4401S1-712M 234-514-9008 | Coupling, Clamp, Grooved | Height: 0.280 inches nominal Inside Diameter: 7.120 inches nominal Cross-Sectional Shape Style: 1 grooved retainer | Eaton Corporation (00624) V I J Corporation (94581) Northrop Grumman Systems Corporation (26512) | |
| 5342-01-035-6984 5342010356984 | 1706-236 | Bracket, Landing Gear | General Characteristics Item Description: Steel AMS6350 comp 4130, 0.218 in. min, 0.222 in. max dia 2 holes III End Item Identification: EA-6B aircraft | Goodrich Corporation (13002) |