Part Details | TRANSMITTER SYNCHRO
5990-00-010-1413 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: 9011805, 14970150001, 1497015-0001, 1497015, 14865571, 1486557-1, AY110615B1, AY1106-15B1, U219478, U-219478, 5990-00-010-1413, 00-010-1413, 5990000101413, 000101413
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-010-1413 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-010-1413
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9011805 | 97151 | AIR FORCE LIFECYCLE MANAGEMENTCENTER ELECTRONIC COMPONENTS |
| 1497015-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497015 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1486557-1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY1106-15B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| U-219478 | 82686 | TRANSICOIL LLCDBA ADS/TRANSICOIL |
Technical Data | NSN 5990-00-010-1413
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 120.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 44.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 243.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 57.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 28.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 18.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 9.30 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 25.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 1.8 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.6 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2000.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 1.9800 INCHES MINIMUM AND 2.0100 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6200 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0900 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |