NSN 5990-00-683-0020
Part Details | TRANSMITTER SYNCHRO
5990-00-683-0020 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: AY4012B, AY401-2-B, AY4012A1, AY401-2-A1, AY4012B, AY401-2-B, AY4012A1, AY401-2-A1, CG22A1A488, CG-22-A-1/A488, 90014111, 900141-11, 5990-00-683-0020, 00-683-0020, 5990006830020, 006830020
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-683-0020 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-683-0020
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY401-2-B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY401-2-A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY401-2-B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY401-2-A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CG-22-A-1/A488 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 900141-11 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 5990-00-683-0020
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 22 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.0 AMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 4.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 1.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 5.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 5.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 35.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 0.58 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 0.26 NOMINAL |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.500 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 19.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 26.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 45.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.9995 INCHES MAXIMUM |
| PILOT DIAMETER | 0.7500 INCHES MAXIMUM |
| OVERALL LENGTH | 3.2370 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.1610 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.1250 INCHES NOMINAL |
| UNDERCUT DIAMETER | 2.0000 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0950 INCHES MINIMUM |
| PILOT LENGTH | 0.0600 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2000 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6340 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0010 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0015 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
