NSN 5990-00-835-5211
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-835-5211 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: AY50336A1, AY503-36A1, AY50336A1, AY503-36A1, 5078771, 507877-1, 5990-00-835-5211, 00-835-5211, 5990008355211, 008355211
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-835-5211 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-835-5211
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY503-36A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY503-36A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 507877-1 | 37695 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-835-5211
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 10.2 NOMINAL |
| STATOR INPUT CURRENT RATING | 85.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 350.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 225.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 695.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 43.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 141.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 307.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 115.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 135.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 36.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 50.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0620 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
