NSN 5990-00-105-9575
Part Details | TRANSMITTER SYNCHRO
5990-00-105-9575 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 35630800071, 3563080-0071, 35630800071, 3563080-0071, AY080FA41A2, 5990-00-105-9575, 00-105-9575, 5990001059575, 001059575
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 15, 1968 | 00-105-9575 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-105-9575
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563080-0071 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0071 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY080FA41A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-105-9575
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 470.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 256.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.80 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 44.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 19.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 35.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 11.30 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 7.800 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 125.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2200.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.7300 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.0690 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| 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 | 8.0 OUNCES |
| FRAGILITY FACTOR | MODERATELY RUGGED |