NSN 5990-00-539-7080
Part Details | RECEIVER SYNCHRO
5990-00-539-7080 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: AY200S2B, AY200S-2-B, 7905524, 790552-4, AY200S2B, AY200S-2-B, 7905524, 790552-4, E394241PC103, E39424-1PC103, E394231PC103, E39423-1PC103, 5990-00-539-7080, 00-539-7080, 5990005397080, 005397080
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-539-7080 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-539-7080
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY200S-2-B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 790552-4 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY200S-2-B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 790552-4 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| E39424-1PC103 | 27847 | UNICONTROL INCHAYS CLEVELAND DIV |
| E39423-1PC103 | 27847 | UNICONTROL INCHAYS CLEVELAND DIV |
Technical Data | NSN 5990-00-539-7080
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 450.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 45.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 255.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 6.70 NOMINAL |
| TRANSFORMATION RATIO | 1.000 ROTOR TO STATOR MINIMUM AND 2.200 ROTOR TO STATOR MAXIMUM |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M40.0/P40.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 2.0 CENTIMETER-GRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2250.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.8810 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.5000 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |