Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-045-4705 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: 663402, 66340-2, AY50338A6, AY503-38A6, AY100AZ59A6, AY50338A6, AY503-38A6, AY100AZ59A6, 663402, 66340-2, AY50338A6, AY503-38A6, 10CT300E2820, 10CT300E28/20, 5990-00-045-4705, 00-045-4705, 5990000454705, 000454705
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-045-4705 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-045-4705
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 66340-2 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| AY503-38A6 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY100AZ59A6 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY503-38A6 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY100AZ59A6 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 66340-2 | 07421 | INTERSTATE ELECTRONICS CORPORATIONDBA L-3 INTERSTATE ELECTRONICS |
| AY503-38A6 | 06845 | RAYTHEON COMPANYDBA RAYTHEON |
| 10CT300E28/20 | 06986 | WHITECRAFT RATTAN INC |
Technical Data | NSN 5990-00-045-4705
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 10.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 23.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 70.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 595.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2130.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 126.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 427.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 750.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 369.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 410.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 126.00 NOMINAL |
| TRANSFORMATION RATIO | 11.800 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 95.0 DEG CELSIUS |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 20.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8123 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8370 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |