NSN 5990-00-503-0588
Part Details | RECEIVER SYNCHRO
5990-00-503-0588 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: IF, 512291J, 23301B, 2330-1B, 512291J, 512291J, 23301B, 2330-1B, MILS233581F, MIL-S-2335-8-1F, 512291J, 5990-00-503-0588, 00-503-0588, 5990005030588, 005030588
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-503-0588 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND, REAR MOUNTING FLANGE
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-503-0588
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| IF | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 512291J | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 2330-1B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 512291J | 27914 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| 512291J | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 2330-1B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| MIL-S-2335-8-1F | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 512291J | 23667 | SMITHS DETECTION, INC.DIV EDGEWOOD |
Technical Data | NSN 5990-00-503-0588
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 133.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 3.2 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 60.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 183.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 847.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 176.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 475.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 392.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 136.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 136.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 204.00 NOMINAL |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 25.0 DEG CELSIUS |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M90.0/P90.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.060 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND, REAR MOUNTING FLANGE |
| SHOULDER DIAMETER | 1.2500 INCHES NOMINAL |
| PILOT DIAMETER | 1.0625 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 1.9000 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.7000 INCHES NOMINAL |
| OVERALL LENGTH | 3.7330 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9500 INCHES NOMINAL |
| PILOT LENGTH | 0.1250 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0250 INCHES NOMINAL |
| SECOND SHOULDER FACE TO REAR FLANGE DISTANCE | 1.7000 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1560 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8440 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
| SHAFT END PLAY | 0.0150 INCHES MAXIMUM |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |