NSN 5990-00-875-3642
Part Details | TRANSMITTER SYNCHRO
5990-00-875-3642 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: AY110AA40A1, AY110AA40A1, RS911, RS9111A, RS911-1A, 17753421, 1775342-1, 5990-00-875-3642, 00-875-3642, 5990008753642, 008753642
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 13, 1967 | 00-875-3642 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-875-3642
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY110AA40A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110AA40A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| RS911 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| RS911-1A | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 1775342-1 | 06401 | L3 TECHNOLOGIES, INC.DBA COMMUNICATION SYSTEMS-WEST |
Technical Data | NSN 5990-00-875-3642
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 280.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.4 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 15.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 118.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 4.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 20.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 22.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 11.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.50 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 30.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 3000.0 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 | 2.1430 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0520 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7680 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1120 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
