NSN 5990-00-903-8672
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-903-8672 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 330541, 23231C, 2323-1C, 23231C, 2323-1C, 5990-00-903-8672, 00-903-8672, 5990009038672, 009038672
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-903-8672 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-903-8672
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 330541 | 80249 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION INC. |
| 2323-1C | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 2323-1C | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-903-8672
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 90.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 24.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 580.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 596.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 930.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 667.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 2030.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 850.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 310.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 435.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 465.00 NOMINAL |
| TRANSFORMATION RATIO | 0.720 ROTOR TO STATOR MINIMUM AND 0.750 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 14.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| SHOULDER DIAMETER | 1.0620 INCHES MINIMUM AND 1.0630 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6100 INCHES MINIMUM AND 0.6300 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.2400 INCHES MINIMUM AND 1.2600 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.0625 INCHES NOMINAL |
| OVERALL LENGTH | 3.9730 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1480 INCHES MINIMUM AND 0.1520 INCHES MAXIMUM |
| SECOND SHOULDER FACE TO REAR FLANGE DISTANCE | 1.7000 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| SHAFT END PLAY | 0.0150 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 48.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0020 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
