Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-150-6979 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: 35630800201, 3563080-0201, 14978630000, 1497863-0000, 35630800201, 3563080-0201, 14978630000, 1497863-0000, 1497863, AY080AA36A1, 5990-00-150-6979, 00-150-6979, 5990001506979, 001506979
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | OCT 26, 1970 | 00-150-6979 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-150-6979
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563080-0201 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1497863-0000 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0201 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497863-0000 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497863 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY080AA36A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-150-6979
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 70.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 475.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1780.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 65.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 28.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 553.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 157.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 325.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 62.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 125.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M3.5/P3.5 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6150 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| PILOT LENGTH | 0.0390 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.5730 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| 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 | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |