NSN 5990-00-858-8782
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-858-8782 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 1034708, N20884141, N2088414-1, AY193T1, AY113AC43A1, N20884141, N2088414-1, AY193T1, AY113AC43A1, AY113AA43A1, 7370991, 413901, 4139-01, TDH11E04B954, TDH-11-E-04/B954, C45413901, C45-4139-01, 5990-00-858-8782, 00-858-8782, 5990008588782, 008588782
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-858-8782 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 Y-STATOR
Cross Reference | NSN 5990-00-858-8782
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1034708 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| N2088414-1 | 11272 | BENDIX CORP THERESEARCH LABORATORIES DIV |
| AY193T1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY113AC43A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| N2088414-1 | 27914 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| AY193T1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY113AC43A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY113AA43A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 7370991 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 4139-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TDH-11-E-04/B954 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| C45-4139-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-858-8782
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 135.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 400.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 15.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 64.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 17.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 73.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 15.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 9.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 14.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 12.10 NOMINAL |
| TRANSFORMATION RATIO | 1.112 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 7.000 OUTPUT TO INPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 7.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.0950 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9000 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6870 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| 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 | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 Y-STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |
