Miscellaneous Aircraft Accessories and Components: A51A20101V2-125, A51A9125-23, A51AM1121-3
| MFG SKU | NSN | Item Name | Details | Manufacturer (CAGE) | RFQ |
|---|---|---|---|---|---|
| A51A20101V2-125 A51A20101V2125 | 1680-01-068-7740 | Switching Assembly, | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A72002T | 1680-01-109-0866 | Panel Assembly, Electrical | III End Item Identification: Aircraft model F-14 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A72002T-1 A51A72002T1 | 1680-01-109-0866 | Panel Assembly, Electrical | III End Item Identification: Aircraft model F-14 | Naval Air Systems Command (30003) | |
| A51A9001-33 A51A900133 | 1680-01-253-9196 | Actuator, Electro-Mechanical, Rota | Current Type: Ac and dc Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. Current Rating in Amps: 0.6 and 4.5 and 0.06 and 0.25 | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9005-7 A51A90057 | 1680-01-581-7981 | Mids, Uhf Ant, Aircra | EDO Corp. (00752) | ||
| A51A9019-63 A51A901963 | 1680-01-296-6172 | Panel, Fault-Function Indicator, a | III End Item Identification: F-14 acft Special Features: 6.790 in. lg, 5.750 in. W Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Northrop Grumman Systems Corporation (26512) | |
| A51A9019-79 A51A901979 | 1680-01-462-1460 | Panel, Fault-Function Indicator, a | III End Item Identification: Fighter aircraft F14 III Part Name Assigned By Controlling Agency: Indicator, caution-advisory id Criticality Code Justification: AGAV | Northrop Grumman Systems Corporation (26512) | |
| A51A9065-7 A51A90657 | 1680-00-536-4695 | Adapter-Plate, Servo | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: Aluminum alloy casting, QQ-A-591, alloy no. A380, 0.810 in.nom O/a H, 2.802 in. nom O/a dia | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9125-17 A51A912517 | 1680-00-042-7163 | Panel, Fault-Function Indicator, Aircraft | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9125-19 A51A912519 | 1680-00-042-7163 | Panel, Fault-Function Indicator, Aircraft | Northrop Grumman Systems Corporation (26512,61174) | ||
| A51A9125-23 A51A912523 | 1680-00-332-3690 | Panel, Fault-Function Indicator, a | Special Features: 6.790 in. lg, 3.250 in. W, 4.625 in. H | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9125-29 A51A912529 | 1680-01-296-6173 | Panel, Fault-Function Indicator, a | III End Item Identification: F-14 acft Special Features: Input voltage 28VDC;6.875 in. LG;4.625 in. W;3.250 in. h;four 0.168 in. dia mtg holes spaced on 2.875 X 3.437 in. mtg cntrs Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9203-1 A51A92031 | 1680-01-137-7397 | Detector, Ratio-Engine Stall | III End Item Identification: Aircraft model F-14A General Characteristics Item Description: 7.500 in. lg, 4.000 in. W, 3.000 in. H Reference Number Differentiating Characteristics: As differentiated by the source control dwg. no. | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9216-1 A51A92161 | 1680-01-253-6989 | Panel, Flight Maintenance | III End Item Identification: Aircraft model F-14 Reference Number Differentiating Characteristics: As differentiated by the source control dwg no. | Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9216-5 A51A92165 | 1680-01-343-8976 | Panel, Control, Electrical-Electro | III End Item Identification: F-14 acft Special Features: Components include microcircuit, display, alphanumeric, four matrices of light emitting diodes, with logic, monostable multivibrater, duel precision retriggerable/resettable microcircuit, made of monolithic silicon, indicator, fault locating flag, mechanical reset, filter, radio frequency interference hermetically sealed, insulation sleeving, electrical, polytetraflouroethylene resin, non rigid, connector mounting block, plug-in module, circuit card assy-display, printed wiring board-display, circuit card assy switch a/b, printed wiring board assy switch a/b Reference Number Differentiating Characteristics: As differentiated by source control no. | Northrop Grumman Field Support (08DR5) Northrop Grumman Systems Corporation (26512,61174) | |
| A51A9287-21 A51A928721 | 1680-01-476-2619 | Panel, Control, Electrical-Electro | III Part Name Assigned By Controlling Agency: (Inavy) panel, control, elect | Northrop Grumman Field (1DDP5) Northrop Grumman Systems Corporation (26512) | |
| A51A9287-23 A51A928723 | 1680-01-476-9359 | Panel, Control, Electrical-Electro | III End Item Identification: Panel, control, electrical-electronic equipment: indicator, digital display: arr list code- F14 vdig-R, A51A17636-1. III Part Name Assigned By Controlling Agency: Panel, control, electrical. | Northrop Grumman Field (1DDP5) Northrop Grumman Systems Corporation (26512) | |
| A51A9287-25 A51A928725 | 1680-01-476-2622 | Panel, Control, Electrical-Electro | III End Item Identification: F-14 Reference Number Differentiating Characteristics: As differentiated by source control drawing | Northrop Grumman Field (1DDP5) Northrop Grumman Systems Corporation (26512) | |
| A51A9287-27 A51A928727 | 1680-01-476-2621 | Panel, Control, Electrical-Electro | III End Item Identification: F-14 fighter aircraft Reference Number Differentiating Characteristics: As differentiated by source conrtol drawing | Northrop Grumman Field (1DDP5) Northrop Grumman Systems Corporation (26512) | |
| A51AM1121-3 A51AM11213 | 1680-01-471-4236 | Switching Assembly | Northrop Grumman Field Support (9G864) |