NSN 5990-00-557-3668
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-557-3668 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: AY50025A1, AY500-25A1, AY50025A1, AY500-25A1, AY50325A1, AY503-25A1, AY50025A1, AY500-25A1, 6040267, 6040267, 6040267, 5990-00-557-3668, 00-557-3668, 5990005573668, 005573668
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-557-3668 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-557-3668
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY500-25A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY500-25A1 | 02987 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS |
| AY503-25A1 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY500-25A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 6040267 | 89264 | INTERNATIONAL BUSINESS MACHINES CORP |
| 6040267 | 30874 | INTERNATIONAL BUSINESS MACHINES CORP |
| 6040267 | 0B6S1 | INTERNATIONAL BUSINESS MACHINES CORPPARTS ORDER CENTER DEPT E - 54 |
Technical Data | NSN 5990-00-557-3668
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 70.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 200.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSO RESISTANCE IN OHMS | 43.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 141.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 36.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M1.0/P1.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.5290 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0630 INCHES NOMINAL |
| 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 |