To receive competitive purchasing options on part number 736470-03 by Ge Aviation Systems Ltd, look no further than NSN Direct. For your reference, this item has the NSN 5990-00-872-9370 and is listed with the description “Synchro Transmitter.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Ge Aviation Systems Ltd parts produced under the CAGE Code 35351, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number 736470-03, you can glean from the first four digits of its NSN 5990-00-872-9370 that it belongs to the FSC 5990 Synchros and Resolvers. This being said, do not hesitate to request quotes on part number 736470-03 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5990-00-872-9370 Item PartTypeName: SYNCHRO,TRANSMITTER | 5990 | 008729370 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 736470-03 | C | 2 | 7 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAVH | SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| AAVL | PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| ABKK | FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| ABKU | FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| ABPA | UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| ABXF | SHAFT LENGTH | 0.2110 INCHES MINIMUM AND 0.2290 INCHES MAXIMUM SINGLE SHAFT |
| AJSL | BODY SIZE | 11 |
| AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
| AJST | ROTOR INPUT CURRENT RATING | 136.0 MILLIAMPERES MAXIMUM |
| AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 450.0 MILLIWATTS NOMINAL |
| AJSY | ZSO RESISTANCE IN OHMS | 8.00 NOMINAL |
| AJTT | STATOR DC RESISTANCE IN OHMS | 5.75 NOMINAL |
| AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 46.00 |
| AJVS | ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS MAXIMUM |
| AJWQ | PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| AJWR | SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| CQRG | BODY MATERIAL | STEEL CORROSION RESISTING |
| CQXQ | PLUS J ZRO REACTANCE IN OHMS | 233.00 NOMINAL |
| CRGZ | PLUS J ZSO REACTANCE IN OHMS | 39.00 NOMINAL |
| TTQY | TERMINAL TYPE AND QUANTITY | 5 SCREW |
| AAQL | BODY STYLE | STANDARD ROUND C |
| ABHP | OVERALL LENGTH | 2.0280 INCHES MAXIMUM |
| ABPC | UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| ABWV | SHAFT DIAMETER | 0.1195 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM SINGLE SHAFT |
| AHCG | MAXIMUM TEMP RISE | 7.0 DEG CELSIUS |
| AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| AJSW | ZRO RESISTANCE IN OHMS | 37.00 NOMINAL |
| AJTS | ROTOR DC RESISTANCE IN OHMS | 19.00 NOMINAL |
| AJVF | PHASE SHIFT ANGLE IN DEG | 4.700 INPUT TO OUTPUT NOMINAL |
| AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 26.00 OUTPUT |
| AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -7.0 TO 7.0 |
| AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7990 INCHES MAXIMUM |
| CQTM | TERMINAL LOCATION | REAR |
| CQZS | SHAFT SLOT DEPTH | 0.0300 INCHES NOMINAL SINGLE SHAFT |
| CRHN | SHAFT SLOT WIDTH | 0.0250 INCHES NOMINAL SINGLE SHAFT |
| CRSJ | SHAFT TYPE | ROUND,SLOTTED SINGLE SHAFT |
| CSJY | TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
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