NSN 5990-00-583-3254
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-583-3254 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: 12485101, 124851-01, 4245871A, 424587-1A, 4245871A, 424587-1A, 5990-00-583-3254, 00-583-3254, 5990005833254, 005833254
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-583-3254 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-583-3254
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 124851-01 | 35351 | GE AVIATION SYSTEMS LLC |
| 424587-1A | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 424587-1A | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
Technical Data | NSN 5990-00-583-3254
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 12 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 21.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 50.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 625.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 3280.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 93.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 570.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 570.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 330.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 106.00 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 68.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 385.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 60.00 NOMINAL |
| TRANSFORMATION RATIO | 2.203 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.700 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 53.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 80.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 32.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 8.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | 2 STANDARD ROUND A |
| SHOULDER DIAMETER | 1.1050 INCHES MINIMUM AND 1.1130 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES NOMINAL |
| OVERALL LENGTH | 2.9630 INCHES MINIMUM AND 3.0450 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.1850 INCHES MINIMUM AND 1.1910 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 1.1130 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.3050 INCHES MINIMUM AND 2.3110 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
