NSN 5990-01-110-1979
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-01-110-1979 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: 11CT01236, 11CT-0123-6, ZV2A, ZV2-A, 20685970701, 2068597-0701, TTH11H4B402, TTH-11-H-4/B402, 5990-01-110-1979, 01-110-1979, 5990011101979, 011101979
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 27, 1981 | 01-110-1979 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-01-110-1979
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 11CT-0123-6 | 51761 | CDA INTERCORP LLC |
| ZV2-A | 51761 | CDA INTERCORP LLC |
| 2068597-0701 | 27914 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| TTH-11-H-4/B402 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-110-1979
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 18.2 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 30.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 650.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 3000.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 90.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 550.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 605.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 295.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 59.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 OUTPUT TO INPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1150 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | AN/APS133 |
