NSN 5990-00-021-5061
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-021-5061 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 14273901, 142739-01, 5990-00-021-5061, 00-021-5061, 5990000215061, 000215061
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAY 02, 1967 | 00-021-5061 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-021-5061
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 142739-01 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-00-021-5061
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.7 MINIMUM AND 11.9 MAXIMUM |
| STATOR INPUT CURRENT RATING | 43.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 120.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 340.00 MINIMUM AND 460.00 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 1207.00 MINIMUM AND 1633.00 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 51.00 MINIMUM AND 69.00 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 216.00 MINIMUM AND 292.00 MAXIMUM |
| ZRS RESISTANCE IN OHMS | 692.00 MINIMUM |
| PLUS J ZRS REACTANCE IN OHMS | 127.50 MINIMUM AND 172.50 MAXIMUM |
| ROTOR DC RESISTANCE IN OHMS | 328.50 MINIMUM AND 401.50 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 57.60 MINIMUM AND 70.40 MAXIMUM |
| TRANSFORMATION RATIO | 127.500 ROTOR TO STATOR MINIMUM AND 172.500 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 10.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 10.50 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M5.0/P5.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 INCH-OUNCES NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5980 INCHES MINIMUM AND 1.6280 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0570 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |