Part Details | DIFFERENTIAL RECEIVER SYNCHRO
5990-00-079-5406 A synchro, the rotor of which is free to turn, which will assume a position in accordance with the sum or difference of the electrical angular information received from two transmitter synchros. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: AY232S3B, AY232S-3-B, AY232S3B, AY232S-3-B, 5265073, 526507-3, 99380, 99380, 5990-00-079-5406, 00-079-5406, 5990000795406, 000795406
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-079-5406 | 02070 ( SYNCHRO, DIFFERENTIAL RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 Y-STATOR
Cross Reference | NSN 5990-00-079-5406
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY232S-3-B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY232S-3-B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 526507-3 | 22525 | INSTRUMENTS AND FLIGHT RESEARCH INC. |
| 99380 | 1PQF4 | L3 TECHNOLOGIES, INC.DBA LINK SIMULATION & TRAINING |
| 99380 | 36378 | RAYTHEON TECHNICAL SERVICES COMPANY |
Technical Data | NSN 5990-00-079-5406
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 130.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 320.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 15.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 63.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 14.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 77.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 16.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 8.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 14.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.80 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 6.000 OUTPUT TO INPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.4440 INCHES NOMINAL |
| FLANGE DIAMETER | 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 | 1.6310 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0010 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 Y-STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |