NSN 5990-00-686-4899
Part Details | TRANSMITTER SYNCHRO
5990-00-686-4899 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 10TX300B1, 10TX304B1, 10TX-304-B-1, 327664, 327-664, CL40912003, 40733402, 4073-34-02, 229013400, 229-0134-00, 10407319, 10-4073-19, CGH10AS4A412, 229013400, 229-0134-00, 5990-00-686-4899, 00-686-4899, 5990006864899, 006864899
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-686-4899 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-686-4899
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10TX300B1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 10TX-304-B-1 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 327-664 | 90073 | CMC ELECTRONICS INC |
| CL40912003 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 4073-34-02 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-0134-00 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 10-4073-19 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CGH10AS4A412 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-0134-00 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 5990-00-686-4899
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.3 AMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 33.8 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 27.50 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 174.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 30.50 NOMINAL |
| ZRS RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 16.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.20 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 17.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.5/P7.5 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7270 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0630 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8370 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2810 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |