Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-146-3534 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: EAS303, AY201S3B, AY201S3B, CTH15DS1B, 5990-00-146-3534, 00-146-3534, 5990001463534, 001463534
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 22, 1971 | 00-146-3534 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-146-3534
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| EAS303 | 99251 | CARLETON LIFE SUPPORT SYSTEMS INC.DBA COBHAM MISSION SYSTEM |
| AY201S3B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S3B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CTH15DS1B | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-146-3534
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 10.6 MINIMUM AND 12.0 MAXIMUM |
| STATOR INPUT CURRENT RATING | 115.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 170.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 MINIMUM AND 408.0 MAXIMUM |
| ZRO RESISTANCE IN OHMS | 64.60 MINIMUM AND 87.40 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 468.00 MINIMUM AND 572.00 MAXIMUM |
| ZSO RESISTANCE IN OHMS | 12.05 MINIMUM AND 14.95 MAXIMUM |
| PLUS J ZSO REACTANCE IN OHMS | 79.20 MINIMUM AND 96.80 MAXIMUM |
| ROTOR DC RESISTANCE IN OHMS | 38.80 MINIMUM AND 50.40 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 8.64 MINIMUM AND 11.88 MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 5.600 INPUT TO OUTPUT MINIMUM AND 8.500 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.00 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.00 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0680 INCHES MINIMUM AND 0.0880 INCHES MAXIMUM |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6320 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0950 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |