Weapon System - Hardware: 123ABM50503-1, 123AV12050-7, 123BM10510-2
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| 123ABM50503-1 123ABM505031 | 5342-01-291-9179 | Mount, bar | General Characteristics Item Description: Steel, ams 5659 15-5PH, passivate MIL-S-5002; 1.750 in. lg; 1.185 in. w; one hole 0.376 in. min and 0.379 in. max dia | Northrop Grumman Systems Corporation (26512) | |
| 123ABP10027-21 123ABP1002721 | 5342-01-493-6588 | Fairlead, Block | III End Item Identification: Aircraft model E-2C III Part Name Assigned By Controlling Agency: Fairlead | Northrop Grumman Systems Corporation (26512) | |
| 123AMM12187-1 123AMM121871 | 5342-00-075-0714 | Bracket, Crank | General Characteristics Item Description: Aluminum alloy, 4.500 in. lg, 3.250 in. wd. 1 in. thk, six holes 0.130 in. dia, one hole 0.375 in. dia, radjius on four corners 0.375 in. | Northrop Grumman Systems Corporation (26512) | |
| 123AMM12310-511 123AMM12310511 | 5342-00-172-2354 | Latch, Handle, Entrance Door | General Characteristics Item Description: Aluminum alloy, QQ-A-225/9, 7075-T7351, 2.812 in. O/a lg, 1.860 in. O/a W | Northrop Grumman Systems Corporation (26512) | |
| 123AMM41143-1 123AMM411431 | 5342-01-195-2380 | Crank, Torque Tube | General Characteristics Item Description: Aluminum, per ams 4050, alloy 7050-T73651 III End Item Identification: Aircraft model C-2A | Northrop Grumman Systems Corporation (26512) | |
| 123AMM41143-11 123AMM4114311 | 5342-01-195-2380 | Crank, Torque Tube | General Characteristics Item Description: Aluminum, per ams 4050, alloy 7050-T73651 III End Item Identification: Aircraft model C-2A | Northrop Grumman Systems Corporation (26512) | |
| 123AMM41143-611 123AMM41143611 | 5342-01-195-2380 | Crank, Torque Tube | General Characteristics Item Description: Aluminum, per ams 4050, alloy 7050-T73651 III End Item Identification: Aircraft model C-2A | Northrop Grumman Systems Corporation (26512) | |
| 123AMM41145-1 123AMM411451 | 5342-01-195-2381 | Crank, Special | General Characteristics Item Description: Aluminum, per QQ-A-200/11, alloy 7075-T73511; 2.310 in. eff lg III End Item Identification: Aircraft model C-2A | Northrop Grumman Systems Corporation (26512) | |
| 123AMM41145-611 123AMM41145611 | 5342-01-195-2381 | Crank, Special | General Characteristics Item Description: Aluminum, per QQ-A-200/11, alloy 7075-T73511; 2.310 in. eff lg III End Item Identification: Aircraft model C-2A | Northrop Grumman Systems Corporation (26512) | |
| 123AMN12187-1 123AMN121871 | 5342-00-075-0714 | Bracket, Crank | General Characteristics Item Description: Aluminum alloy, 4.500 in. lg, 3.250 in. wd. 1 in. thk, six holes 0.130 in. dia, one hole 0.375 in. dia, radjius on four corners 0.375 in. | Northrop Grumman Systems Corporation (61174) | |
| 123AV12050-1 123AV120501 | 5342-00-066-7528 | Bracket, Junction Bo | Northrop Grumman Systems Corporation (26512,61174) | ||
| 123AV12050-7 123AV120507 | 5342-00-066-7529 | Bracket, Junction Bo | Northrop Grumman Systems Corporation (26512,61174) | ||
| 123B10045-503 123B10045503 | 5342-01-139-2126 | Door, Access, Weapon System | End Item Identification: Aircraft model E-2B, E-2C | Northrop Grumman Systems Corporation (26512) | |
| 123B10418-3 123B104183 | 5342-01-237-2670 | Door, Access, Weapon System | Material: Aluminum alloy 7075 Surface Treatment: Anodize Material Document and Classification: QQ-A-250/13, T6 fed spec single material response | Northrop Grumman Systems Corporation (26512) | |
| 123B10991-13 123B1099113 | 5342-01-259-4171 | Plate, Stop | General Characteristics Item Description: Steel, MIL-S-6758, comp 4130; epoxy polyamide primer, MIL-P-23377; 1.406 in. lg; 0.375 in. w; 0.375 in. thk; chamfer 0.125 in. by 45.0 deg; two mtg holes 0.190 in. min 0.196 in. max dia spaced 0.375 in. from chamfered edge and 0.625 in. apart; one corner radius 0.313 in.; hardness rockwell C27 min C32 max | Northrop Grumman Systems Corporation (26512,61174) | |
| 123B50242-11 123B5024211 | 5342-01-458-7233 | Door, Access, Weapon System | Material: Aluminum alloy 2024 | Northrop Grumman Systems Corporation (26512,61174) | |
| 123BM10013-2 123BM100132 | 5342-00-580-4113 | Leaf, Hinge, Extruded | General Characteristics Item Description: Aluminum alloy QQ-A-200/11 composition 7075 temper T6511, anodize MIL-A-8625 type 2 cl 2 III End Item Identification: Aircraft model E-2C | Northrop Grumman Systems Corporation (26512) | |
| 123BM10013-512 123BM10013512 | 5342-00-580-4113 | Leaf, Hinge, Extruded | General Characteristics Item Description: Aluminum alloy QQ-A-200/11 composition 7075 temper T6511, anodize MIL-A-8625 type 2 cl 2 III End Item Identification: Aircraft model E-2C | Aircraft Hinge Inc. (0CD56) GKN Aerospace Bandy Machining Inc. (22176) Northrop Grumman Systems Corporation (26512) | |
| 123BM10362-1 123BM103621 | 5342-00-075-0870 | Hinge, Door | Northrop Grumman Systems Corporation (26512) | ||
| 123BM10510-2 123BM105102 | 5342-00-066-9503 | Hinge, Nose Gear Doo | Northrop Grumman Systems Corporation (26512) |