NSN 5990-00-983-7530
Part Details | RECEIVER SYNCHRO
5990-00-983-7530 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 105C2E7, AY150FA5B3, 1470060001 MOD BY SRS 27823, 147-006-0001 MOD BY SRS 27823, 1470060001, 147-006-0001, 105C2E5, 5990-00-983-7530, 00-983-7530, 5990009837530, 009837530
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-983-7530 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-983-7530
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 105C2E7 | 99479 | BOWMAR, LLC |
| AY150FA5B3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 147-006-0001 MOD BY SRS 27823 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 147-006-0001 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 105C2E5 | 97497 | UNITED AIRCRAFT CORPNORDEN DIVISION KETAY DEPT |
Technical Data | NSN 5990-00-983-7530
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 200.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 3.1 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 675.50 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 83.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 53.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 44.00 NOMINAL |
| TRANSFORMATION RATIO | 0.767 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.600 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M3.0/P3.0 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M45.0/P45.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.05 INCH-OUNCES NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 0.030 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3114 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.8745 INCHES MINIMUM AND 0.8750 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4890 INCHES MINIMUM AND 2.5150 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.4340 INCHES MINIMUM AND 1.4400 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 1.3090 INCHES MINIMUM AND 1.3150 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0370 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.1290 INCHES MINIMUM AND 0.1350 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7690 INCHES MINIMUM AND 1.7750 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.1030 INCHES NOMINAL |
| SECURING HOLE QUANTITY | 4 |
| MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR | UNC |
| MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER | 0.112 INCHES |
| TERMINAL TYPE AND QUANTITY | 5 TAB, SOLDER LUG |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
