NSN 5990-00-777-0413
Part Details | RECEIVER SYNCHRO
5990-00-777-0413 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: RS931014M0D, RS931-014M0D, CR40931081, CR40931037, JWH11RS1A709, JWH11QES1B883, JWH-11-QES-1/B883, 2297019000, 229-7019-000, 229701900, 229-7019-00, 229701800, 229-7018-00, 5990-00-777-0413, 00-777-0413, 5990007770413, 007770413
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-777-0413 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-777-0413
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| RS931-014M0D | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CR40931081 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CR40931037 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| JWH11RS1A709 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| JWH-11-QES-1/B883 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-7019-000 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
| 229-7019-00 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
| 229-7018-00 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 5990-00-777-0413
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 0.2 NOMINAL |
| ROTOR INPUT CURRENT RATING | 500.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 200.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 135.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 580.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1150.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 850.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 180.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 600.00 NOMINAL |
| TRANSFORMATION RATIO | 0.213 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 25.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS 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 | 2.3370 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7820 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
