Part Details | RECEIVER SYNCHRO
5990-00-321-8458 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: 35631004039, 3563100-4039, 35631003049, 3563100-3049, 14979800001, 1497980-0001, 35631003049, 3563100-3049, 14979800001, 1497980-0001, 10134462, 5990-00-321-8458, 00-321-8458, 5990003218458, 003218458
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 18, 1973 | 00-321-8458 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-321-8458
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563100-4039 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563100-3049 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1497980-0001 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563100-3049 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497980-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 10134462 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
Technical Data | NSN 5990-00-321-8458
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| 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 | 42.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 243.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 9.20 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 41.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 49.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 19.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 18.90 MINIMUM AND 23.10 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 5.85 MINIMUM AND 7.15 MAXIMUM |
| TRANSFORMATION RATIO | 0.441 ROTOR TO STATOR MINIMUM AND 0.467 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 1.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2500.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.3190 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0730 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |