| Mfg Part Number: VRW11-4CF-53L | Alternate P/N: VRW114CF53L | Manufacturer: General Dynamics Global Imaging |
| NSN : 5990-00-851-4363 | Item Name : resolver electrical | CAGE Code : 10112 |
| FSC : 5990 Synchros and Resolvers |
Thank you for your continued interest in parts like VRW11-4CF-53L with the NSN 5990-00-851-4363 currently available for purchase on Zippy Purchasing. The Resolver Electrical item associated with the part number VRW11-4CF-53L, by General Dynamics Global Imaging, is currently available in our database; as such, we ask that you please fill out and submit an Instant RFQ form detailing your requirements on parts needed. This includes desired quantities, target prices, expected shipping time frames, and more, as applicable. Upon receival, our representatives will harness your provided information and formulate a solution which satisfies your operational needs in just 15 minutes or less.
With our global supply chain stretching across the United States, Zippy Purchasing can provide expedited shipping on select NSN 5990-00-851-4363 orders for entities facing an Aircraft on Ground (AOG) situation or a variety of additional unique time constraints. Operating with a strict NO CHINA Sourcing pledge, all orders are shipped alongside their applicable manufacturer trace documentation or qualifying certifications, ensuring that customers can feel confident in every purchase made. With cost savings and rapid lead times bolstering every order, experience all we have to offer by submitting your RFQ for Resolver Electrical parts with part number VRW11-4CF-53L with the CAGE Code 10112 by General Dynamics Global Imaging, today!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-851-4363 Item Description: Resolver Electrical | 5990 | 008514363 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Vrw11-4cf-53l | 2 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL, STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND C |
| AAVH | SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 2.3950 INCHES MINIMUM AND 2.4250 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0470 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.1871 INCHES MINIMUM SINGLE SHAFT AND 0.1873 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.4850 INCHES MINIMUM SINGLE SHAFT AND 0.5150 INCHES MAXIMUM SINGLE SHAFT |
| AJSL | BODY SIZE | 11 |
| AJSP | STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES MAXIMUM |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 145.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 91.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 6.600 INPUT TO OUTPUT NOMINAL |
| AJVJ | INTERAXIS ERROR ANGULAR RANGE IN MINUTES | -5.0/+5.0 |
| AJVK | OUTPUT VOLTAGE FUNCTIONAL ERROR RANGE IN PERCENT | -0.1/+0.1 |
| AJWQ | PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| AJWR | SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.9100 INCHES MAXIMUM |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 880.00 NOMINAL |
| CRSJ | SHAFT TYPE | ROUND SINGLE SHAFT |
| TTQY | TERMINAL TYPE AND QUANTITY | 12 WIRE LEAD |
| ABKK | FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| ABPA | UNDERCUT DIAMETER | 0.9720 INCHES MINIMUM AND 0.9780 INCHES MAXIMUM |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 MAXIMUM |
| AJSW | ZRO RESISTANCE IN OHMS | 160.00 NOMINAL |
| AJTX | COMPENSATION METHOD | WINDING COMPENSATED |
| AJVC | COMPENSATOR DC RESISTANCE IN OHMS | 370.00 NOMINAL |
| AJVD | COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 0.985 ROTOR TO COMPENSATOR NOMINAL |
| CQTM | TERMINAL LOCATION | REAR |
| CSJY | TRANSFORMATION RATIO | 0.980 ROTOR TO STATOR NOMINAL |
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