NSN 5990-00-321-8459
Part Details | RECEIVER SYNCHRO
5990-00-321-8459 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: AY110CL17A1, 14979790001, 1497979-0001, AY110CL17A1, 14979790001, 1497979-0001, 5990-00-321-8459, 00-321-8459, 5990003218459, 003218459
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 18, 1973 | 00-321-8459 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-321-8459
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY110CL17A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1497979-0001 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110CL17A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497979-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-321-8459
| 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 | 11.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 40.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 57.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 28.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.20 MINIMUM AND 19.80 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 8.37 MINIMUM AND 10.23 MAXIMUM |
| TRANSFORMATION RATIO | 0.441 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| 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 | 1.8780 INCHES NOMINAL |
| 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 NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |