NSN 5990-00-686-4902
Part Details | RECEIVER SYNCHRO
5990-00-686-4902 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: TRH11JS2, R92521N, R925-21N, R92521N, R925-21N, TRH11JS2, TRH11JS2, TRH-11-JS-2, TRC11JS2, 229017600, 229-0176-00, 5990-00-686-4902, 00-686-4902, 5990006864902, 006864902
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-686-4902 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-686-4902
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| TRH11JS2 | 83267 | CLIFTON MFG CO INC |
| R925-21N | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| R925-21N | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| TRH11JS2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TRH-11-JS-2 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TRC11JS2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-0176-00 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 5990-00-686-4902
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 110.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 430.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 42.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 270.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 46.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 50.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 21.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 20.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.800 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.3 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2100.0 MILLIMETER-MILLIGRAMS MINIMUM |
| 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 | 2.2020 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6400 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES MAXIMUM |
| 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 |
| FRAGILITY FACTOR | MODERATELY RUGGED |