Part Details | TRANSMITTER SYNCHRO
5990-00-065-3081 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: 14197401, 141974-01, 5990-00-065-3081, 00-065-3081, 5990000653081, 000653081
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 27, 1967 | 00-065-3081 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-065-3081
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 141974-01 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-00-065-3081
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 25.7 MINIMUM AND 26.3 MAXIMUM |
| ROTOR INPUT CURRENT RATING | 163.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 720.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 396.0 MINIMUM AND 404.0 MAXIMUM |
| ZRO RESISTANCE IN OHMS | 22.00 MINIMUM AND 33.00 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 147.90 MINIMUM AND 200.10 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 5.70 MINIMUM AND 9.70 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 25.92 MINIMUM AND 35.08 MAXIMUM |
| ZRS RESISTANCE IN OHMS | 37.60 MINIMUM AND 56.40 MAXIMUM |
| PLUS J ZRS REACTANCE IN OHMS | 13.60 MINIMUM AND 18.40 MAXIMUM |
| ROTOR DC RESISTANCE IN OHMS | 14.11 MINIMUM AND 19.09 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 6.80 MINIMUM AND 7.80 MAXIMUM |
| TRANSFORMATION RATIO | 0.440 ROTOR TO STATOR MINIMUM AND 0.468 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 3.000 INPUT TO OUTPUT MINIMUM AND 5.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 125.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 INPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
| 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 |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8128 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7360 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1840 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |