Part Details | TRANSMITTER SYNCHRO
5990-00-436-7766 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: 8TX200A3, 327601, 327-601, CM91014025, 5990-00-436-7766, 00-436-7766, 5990004367766, 004367766
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 05, 1969 | 00-436-7766 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND, ROTATABLE HOUSING
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-436-7766
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8TX200A3 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 327-601 | 90073 | CMC ELECTRONICS INC |
| CM91014025 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
Technical Data | NSN 5990-00-436-7766
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 170.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 930.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 2800.000 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND, ROTATABLE HOUSING |
| SHOULDER DIAMETER | 0.4995 INCHES MINIMUM AND 0.7510 INCHES MAXIMUM |
| OVERALL LENGTH | 1.9380 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| BODY DIAMETER | 0.7470 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.3060 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 TURRET |
| BODY MATERIAL | ANY ACCEPTABLE |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |