R920-1A by Kearfott Corp with NSN 5990008270684 - Submit a Quote
| Part No. : R920-1A | Alternate P/N: R9201A | Manufacturer : Kearfott Corp | NSN : 5990-00-827-0684 |
| Item Name : Synchro Receiver | CAGE Code : 88818 | FSC : 5990 Synchros and Resolvers |
ASAP Aviation Procurement is pleased to announce that part number R920-1A of NSN 5990008270684 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number R920-1A is a synchro receiver manufactured by kearfott corp under CAGE Code 88818. 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. R920-1A kearfott corp is in stock.
Are you interested in learning more about part number R920-1A? If so, feel free to contact us by phone at +1-714-705-4780, or by email at sales@asap-aviationprocurement.com. And if you are interested in an even faster and more convenient purchasing platform, check out the ASAP Semiconductor App from Google Play or the App Store.
NSN Information for Part Number R920-1A with NSN 5990-00-827-0684, 5990008270684
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-827-0684 Item Description: Synchro Receiver | 5990 | 008270684 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| R920-1a | 2 | 2 | 5 |
Characteristics Data of NSN 5990-00-827-0684, 5990008270684MRC Criteria Characteristic AAFZ BODY MATERIAL STEEL, STAINLESS AAQL BODY STYLE STANDARD ROUND C AAVH SHOULDER DIAMETER 0.9750 INCHES NOMINAL AAVL PILOT DIAMETER 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM ABHP OVERALL LENGTH 2.2240 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM ABKK FLANGE DIAMETER 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM ABKU FLANGE THICKNESS 0.0930 INCHES NOMINAL ABPC UNDERCUT WIDTH 0.0500 INCHES NOMINAL ABXF SHAFT LENGTH 0.3620 INCHES MINIMUM SINGLE SHAFT AND 0.3880 INCHES MAXIMUM SINGLE SHAFT AJSL BODY SIZE 11 AJSR ROTOR INPUT VOLTAGE RATING IN VOLTS 26.0 NOMINAL AJSS FREQUENCY IN HERTZ 400.0 NOMINAL AJTJ ZSO IMPEDANCE MAGNITUDE IN OHMS 18.10 NOMINAL AJTS ROTOR DC RESISTANCE IN OHMS 9.00 NOMINAL AJTT STATOR DC RESISTANCE IN OHMS 3.00 NOMINAL AJVF PHASE SHIFT ANGLE IN DEG 5.000 INPUT TO OUTPUT NOMINAL AJVL ELECTRICAL ERROR ANGULAR RANGE IN MINUTES -15.0/+15.0 AJWQ PILOT LENGTH 0.0620 INCHES NOMINAL AJWR SHOULDER LENGTH 0.0620 INCHES NOMINAL AJWX MOUNTING SURFACE TO TERMINAL END DISTANCE 1.7960 INCHES NOMINAL CQTM TERMINAL LOCATION REAR CRHN SHAFT SLOT WIDTH 0.0250 INCHES NOMINAL SINGLE SHAFT CRSJ SHAFT TYPE ROUND, SLOTTED SINGLE SHAFT TTQY TERMINAL TYPE AND QUANTITY 5 SCREW ABPA UNDERCUT DIAMETER 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM ABWV SHAFT DIAMETER 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT AJST ROTOR INPUT CURRENT RATING 280.0 MILLIAMPERES NOMINAL AJSV ROTOR INPUT ELECTRICAL POWER RATING 910.0 MILLIWATTS NOMINAL AJTG ZRO IMPEDANCE MAGNITUDE IN OHMS 107.00 NOMINAL AJTH ZRO IMPEDANCE ANGLE IN DEG 81.70 NOMINAL AJTK ZSO IMPEDANCE ANGLE IN DEG 79.50 NOMINAL CQZS SHAFT SLOT DEPTH 0.0300 INCHES NOMINAL SINGLE SHAFT CSJY TRANSFORMATION RATIO 0.454 ROTOR TO STATOR MINIMUM
| MRC | Criteria | Characteristic |
|---|---|---|
| AAFZ | BODY MATERIAL | STEEL, STAINLESS |
| AAQL | BODY STYLE | STANDARD ROUND C |
| AAVH | SHOULDER DIAMETER | 0.9750 INCHES NOMINAL |
| AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| ABHP | OVERALL LENGTH | 2.2240 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| ABPC | UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| ABXF | SHAFT LENGTH | 0.3620 INCHES MINIMUM SINGLE SHAFT AND 0.3880 INCHES MAXIMUM SINGLE SHAFT |
| AJSL | BODY SIZE | 11 |
| AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJTJ | ZSO IMPEDANCE MAGNITUDE IN OHMS | 18.10 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 9.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 3.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -15.0/+15.0 |
| AJWQ | PILOT LENGTH | 0.0620 INCHES NOMINAL |
| AJWR | SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7960 INCHES NOMINAL |
| CQTM | TERMINAL LOCATION | REAR |
| CRHN | SHAFT SLOT WIDTH | 0.0250 INCHES NOMINAL SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 SCREW |
| ABPA | UNDERCUT DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| AJST | ROTOR INPUT CURRENT RATING | 280.0 MILLIAMPERES NOMINAL |
| AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 910.0 MILLIWATTS NOMINAL |
| AJTG | ZRO IMPEDANCE MAGNITUDE IN OHMS | 107.00 NOMINAL |
| AJTH | ZRO IMPEDANCE ANGLE IN DEG | 81.70 NOMINAL |
| AJTK | ZSO IMPEDANCE ANGLE IN DEG | 79.50 NOMINAL |
| CQZS | SHAFT SLOT DEPTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR MINIMUM |
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