Weapon System - Hardware: 2320-450, 2321503, 23218-4
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 2320-450 2320450 | 5342-01-391-9639 | Coupling, Clamp, Grooved | Inside Diameter: 4.500 inches nominal Cross-Sectional Shape Style: 10A grooved retainer Material and Location: Iron alloy, ams 5732, comp 660 nut | Eaton Corporation (15284) | |
| 2320-500 2320500 | 5342-01-365-3319 | Coupling, Clamp, Grooved | Inside Diameter: 5.000 inches nominal Cross-Sectional Shape Style: 10A grooved retainer Material and Location: Nickel alloy, ams 5662 alloy 718, retainer | Eaton Corporation (15284) | |
| 232064PC4 | 5342-00-379-8124 | Clamp, cable | Navair and Navsea Managed (10001) | ||
| 232088 | 5342-01-018-5221 | Retainer Spring | III End Item Identification: 2420-66-148-7692, hmee (high mobility engineer excavator) | Clark Equipment Co. (12603) Dana Corp. (77237) | |
| 232089 | 5342-01-019-1948 | Retainer Spring | General Characteristics Item Description: Steel alloy III End Item Identification: 2420-66-148-7692, hmee (high mobility engineer excavator) | Clark Equipment Co. (12603) Dana Corp. (77237) | |
| 2321073 | 5342-01-193-4625 | Bracket, Control Sha | Fairbanks Morse Engine (50024) | ||
| 2321073-1 23210731 | 5342-01-193-4625 | Bracket, Control Sha | Fairbanks Morse Engine (50024) | ||
| 232-11841-1 232118411 | 5342-01-130-6500 | STUD | The Boeing Company (81205) | ||
| 232-12433-5 232124335 | 5342-01-195-5440 | Rod Assembly | The Boeing Company (81205) | ||
| 23213710 | 5342-01-470-0950 | Control rod | III End Item Identification: Engine ALCO251 | Fairbanks Morse Engine (50024) | |
| 23213713 | 5342-01-470-0948 | Control rod | III End Item Identification: Engine ALCO251 | Fairbanks Morse Engine (50024) | |
| 2321503 | 5342-00-817-0834 | Mount, Resilient, Weapon System | Material: Aluminum overall Height: 1.120 inches nominal (Non-Core Data) Resilient Member Material: Rubber, synthetic | Cooper Industries Inc. (94988) | |
| 23217-1 232171 | 5342-01-059-3555 | Mount, Resilient, Weapon System | Flange Thickness: 0.800 inches nominal Thread Size: 0.190-32 all threaded portions Distance Between Mounting Hole Centers: 1.402 inches minimum and 1.410 inches maximum | Barry Wright Corporation (81860) | |
| 23217-2 232172 | 5342-01-061-7086 | Mount, Resilient, Weapon System | Distance Between Mounting Hole Centers: 1.406 inches nominal Flange Length: 1.810 inches nominal Flange Width: 1.330 inches nominal | Barry Wright Corporation (81860) | |
| 23217-3 232173 | 5342-01-061-7086 | Mount, Resilient, Weapon System | Distance Between Mounting Hole Centers: 1.406 inches nominal Flange Length: 1.810 inches nominal Flange Width: 1.330 inches nominal | Barry Wright Corporation (81860) | |
| 23217-3/04 23217304 | 5342-01-061-7086 | Mount, Resilient, Weapon System | Distance Between Mounting Hole Centers: 1.406 inches nominal Flange Length: 1.810 inches nominal Flange Width: 1.330 inches nominal | Barry Wright Corporation (81860) | |
| 232-1789 2321789 | 5342-01-551-0487 | Dashpot | III End Item Identification: Multi-terrain loader; 3805-01-539-3925 III Part Name Assigned By Controlling Agency: Spring, gas | Caterpillar Inc. (11083) Finning UK LTD (U8468) | |
| 23218-1 232181 | 5342-01-050-4862 | Mount, Resilient, Weapon System | Distance Between Mounting Hole Centers: 1.380 inches nominal Flange Length: 1.810 inches nominal Shortest Distance Between Mounting Hole Centers: 1.380 inches nominal | Barry Wright Corporation (81860) | |
| 23218-3 232183 | 5342-01-284-0342 | Mount, Resilient, Weapon System | Flange Length: 1.810 inches nominal Flange Width: 1.810 inches nominal Distance between Mounting Hole Centers: 1.190 inches minimum and 1.370 inches maximum | Barry Wright Corporation (81860) | |
| 23218-4 232184 | 5342-01-301-0320 | Mount, Resilient, Weapon System | Flange Thickness: 0.100 inches minimum and 0.140 inches maximum Distance Between Mounting Hole Centers: 1.370 inches minimum and 1.390 inches maximum Flange Length: 1.810 inches minimum | Barry Wright Corporation (81860) |