Part Details | TRANSMITTER SYNCHRO
5990-00-275-7819 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: AY50025A3, AY500-25A3, AY50025A3, AY500-25A3, 5990-00-275-7819, 00-275-7819, 5990002757819, 002757819
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) | 
|---|---|---|---|
| 59 | JAN 08, 1968 | 00-275-7819 | 02073 ( SYNCHRO, TRANSMITTER ) | 
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
 
					Cross Reference | NSN 5990-00-275-7819
| Part Number | Cage Code | Manufacturer | 
|---|---|---|
| AY500-25A3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL | 
| AY500-25A3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS | 
Technical Data | NSN 5990-00-275-7819
| Characteristic | Specifications | 
|---|---|
| BODY SIZE | 10 | 
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL | 
| ROTOR INPUT CURRENT RATING | 71.0 MILLIAMPERES NOMINAL | 
| ROTOR INPUT ELECTRICAL POWER RATING | 210.0 MILLIWATTS NOMINAL | 
| FREQUENCY IN HERTZ | 400.0 NOMINAL | 
| ZRO RESISTANCE IN OHMS | 78.00 NOMINAL | 
| PLUS J ZRO REACTANCE IN OHMS | 136.00 NOMINAL | 
| ZSO RESISTANCE IN OHMS | 44.00 NOMINAL | 
| PLUS J ZSO REACTANCE IN OHMS | 138.00 NOMINAL | 
| ZRS RESISTANCE IN OHMS | 88.00 NOMINAL | 
| PLUS J ZRS REACTANCE IN OHMS | 20.00 NOMINAL | 
| ROTOR DC RESISTANCE IN OHMS | 76.00 NOMINAL | 
| STATOR DC RESISTANCE IN OHMS | 36.00 NOMINAL | 
| TRANSFORMATION RATIO | 0.585 ROTOR TO STATOR NOMINAL | 
| PHASE SHIFT ANGLE IN DEG | 18.500 INPUT TO OUTPUT NOMINAL | 
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 INPUT | 
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 70.00 | 
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 | 
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL | 
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL | 
| BODY STYLE | STANDARD ROUND C | 
| SHOULDER DIAMETER | 0.9300 INCHES NOMINAL | 
| PILOT DIAMETER | 0.5000 INCHES NOMINAL | 
| OVERALL LENGTH | 1.6546 INCHES MAXIMUM | 
| FLANGE DIAMETER | 0.9370 INCHES NOMINAL | 
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL | 
| UNDERCUT DIAMETER | 0.9350 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 | 
