NSN 5990-00-870-8310
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-870-8310 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: 73707302, 737073-02, ETH10NS3, 5990-00-870-8310, 00-870-8310, 5990008708310, 008708310
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 01, 1967 | 00-870-8310 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-870-8310
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 737073-02 | 35351 | GE AVIATION SYSTEMS LLC |
| ETH10NS3 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-870-8310
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 85.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 292.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 210.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 650.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 41.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 126.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 300.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 90.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 160.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 41.00 NOMINAL |
| TRANSFORMATION RATIO | 2.029 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 13.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.5/P7.5 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.00 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.00 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5340 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8400 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 TURRET |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
