NSN 5990-00-686-5277
Part Details | TRANSMITTER SYNCHRO
5990-00-686-5277 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: 12165661, 1216566-1, AY191A1, AY110AC43A1, 12165661, 1216566-1, AY191A1, AY110AC43A1, 256537, 5990-00-686-5277, 00-686-5277, 5990006865277, 006865277
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-686-5277 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-686-5277
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1216566-1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY191A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110AC43A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1216566-1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY191A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY110AC43A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 256537 | 36378 | RAYTHEON TECHNICAL SERVICES COMPANY |
Technical Data | NSN 5990-00-686-5277
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 70.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 73.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 420.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 16.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 76.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 79.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 57.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 35.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 12.10 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| 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 |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.0560 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9620 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6820 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |