ASAP Aviation Procurement is pleased to announce that part number 11RC26 of NSN 5990-00-967-3793 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number 11RC26 is a Resolver Electrical manufactured by General Dynamics Global Imaging under CAGE Code 10112. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. 11RC26 General Dynamics Global Imaging is in stock.
Are you interested in learning more about part number 11RC26? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-967-3793 Item PartTypeName: RESOLVER,ELECTRICAL | 5990 | 009673793 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| VRP11-4D9-50 | 6 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL,STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND C |
| AAVH | SHOULDER DIAMETER | 0.9700 INCHES MINIMUM AND 0.9800 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.6250 INCHES NOMINAL |
| ABHP | OVERALL LENGTH | 2.4200 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 1.0610 INCHES MINIMUM |
| ABKU | FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| ABPA | UNDERCUT DIAMETER | 0.9995 INCHES MINIMUM |
| ABPC | UNDERCUT WIDTH | 0.0470 INCHES MINIMUM AND 0.0530 INCHES MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.1873 INCHES NOMINAL SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.3900 INCHES MINIMUM SINGLE SHAFT AND 0.4200 INCHES MAXIMUM SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSL | BODY SIZE | 11 |
| AJSN | STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 MAXIMUM |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 605.00 NOMINAL |
| AJSY | ZSO RESISTANCE IN OHMS | 400.00 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 300.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 250.00 NOMINAL |
| AJTX | COMPENSATION METHOD | WINDING COMPENSATED |
| AJVC | COMPENSATOR DC RESISTANCE IN OHMS | 440.00 NOMINAL |
| AJVD | COMPENSATOR TRANSFORMATION RATIO IN PERCENT | 1.000 ROTOR TO COMPENSATOR NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 7.000 INPUT TO OUTPUT NOMINAL |
| AJVJ | INTERAXIS ERROR ANGULAR RANGE IN MINUTES | -5.0 TO 5.0 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.33 INCH-OUNCES MAXIMUM |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.11 INCH-OUNCES MAXIMUM |
| AJVW | ALIGNMENT HOLE QUANTITY | 4 |
| 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 | 2.0000 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 220.00 NOMINAL |
| CQZS | SHAFT SLOT DEPTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
| CRGZ | PLUS J ZSO REACTANCE IN OHMS | 2000.00 NOMINAL |
| CRHN | SHAFT SLOT WIDTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
| CRSY | ALIGNMENT HOLE DEPTH | 0.4045 INCHES MINIMUM AND 0.4075 INCHES MAXIMUM |
| CSJY | TRANSFORMATION RATIO | 0.980 ROTOR TO STATOR NOMINAL |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| TTQY | TERMINAL TYPE AND QUANTITY | 8 SCREW |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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