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Thank you for your interest in NSN part number AY110FA40A1 under NSN 5990005786254 on Click Aerospace. Click Aerospace is a website owned and operated by ASAP Semiconductor, offering customers access to an unparalleled inventory of premium parts that cater to a variety of industries and applications. Synchro Transmitter is an item listed with the part number AY110FA40A1, and FSC 5990 Synchros and Resolvers and it is manufactured by Viking Technologies Ltd having CAGE Code 95937. This item, alongside the rest of our listed NSN parts, is readily available for purchase through our website now. Get started on the purchasing process today by filling out and submitting an Instant RFQ as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to offer a personalized quote based on your individual needs.
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Click Aerospace is a leading independent distributor of NSN part AY110FA40A1, and we can help you procure NSN components such as 5990005786254 and many more. The quality of our inventory is of the utmost importance to us, and thus we choose to only source our parts from global manufacturers like Viking Technologies Ltd. Get started with a competitive quote today when you submit an Instant RFQ and experience how we are revolutionizing the parts procurement process.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-578-6254 Item Description: Synchro Transmitter | 5990 | 005786254 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Ay110fa40a1 | 5 | 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 | 1.9950 INCHES NOMINAL |
| ABKK | FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| ABPA | UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| ABPC | UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM SINGLE SHAFT AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| ABXF | SHAFT LENGTH | 0.3750 INCHES NOMINAL SINGLE SHAFT |
| AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
| AJSL | BODY SIZE | 11 |
| AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJST | ROTOR INPUT CURRENT RATING | 250.0 MILLIAMPERES MAXIMUM |
| AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 1.4 WATTS MAXIMUM |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 3.60 NOMINAL |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 26.00 |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -10.0/+10.0 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| AJVV | TORQUE GRADIENT PER ANGULAR DEG | 4200.0 MILLIMETER-MILLIGRAMS MINIMUM |
| AJVW | ALIGNMENT HOLE QUANTITY | 4 |
| AJWQ | PILOT LENGTH | 0.0620 INCHES NOMINAL |
| AJWR | SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6200 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CQZS | SHAFT SLOT DEPTH | 0.0210 INCHES MINIMUM SINGLE SHAFT AND 0.0310 INCHES MAXIMUM SINGLE SHAFT |
| CRHN | SHAFT SLOT WIDTH | 0.0270 INCHES NOMINAL SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
| CRSY | ALIGNMENT HOLE DEPTH | 0.0900 INCHES MAXIMUM |
| CSJY | TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| CTCW | ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.0250 INCHES NOMINAL |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
Glad You Chose Click Aerospace as Your Parts Distributor Website today. We Hope that You Will Remember Us the Next Time You’re Looking for Required Parts.
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