Part Details | RECEIVER SYNCHRO
5990-00-909-4335 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 35631030010, 3563103-0010, AY103AZ58A6, AY103AZ58A6, AY103AZ58A6, 35631030010, 3563103-0010, 5990-00-909-4335, 00-909-4335, 5990009094335, 009094335
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-909-4335 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-909-4335
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563103-0010 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY103AZ58A6 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY103AZ58A6 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY103AZ58A6 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563103-0010 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-909-4335
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 146.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 630.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 29.90 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 176.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 6.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 29.60 NOMINAL |
| ZRS RESISTANCE IN OHMS | 36.40 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 14.10 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 15.20 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 5.10 NOMINAL |
| TRANSFORMATION RATIO | 0.485 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 40.00 INPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M14.0/P14.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8123 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.6570 INCHES MAXIMUM |
| 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 | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |