NSN 5990-00-583-9594
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-583-9594 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: 5M4541A10, 5M454-1A10, 123101, 123-10-1, R10411A, R1041-1A, 5990-00-583-9594, 00-583-9594, 5990005839594, 005839594
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-583-9594 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-583-9594
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5M454-1A10 | 76301 | BOEING COMPANY, THEDBA BOEING |
| 123-10-1 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| R1041-1A | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 5990-00-583-9594
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 145.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 380.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 79.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 73.00 NOMINAL |
| ZSO IMPEDANCE MAGNITUDE IN OHMS | 110.00 NOMINAL |
| ZSO IMPEDANCE ANGLE IN DEG | 68.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 40.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 25.00 NOMINAL |
| TRANSFORMATION RATIO | 1.154 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 14.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 3.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 17.00 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 | 16.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7620 INCHES MINIMUM AND 1.7660 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2810 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |