Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-115-5851 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: AY100UY59A6, AY100UY-59-A6, 10CT302E3610, 10CT-302-E-36/10, 55139, 79015212, 7901521-2, AY100UY59A6, AY100UY-59-A6, ETH10CKS004A004, ETH-10-CKS-004/A004, 5990-00-115-5851, 00-115-5851, 5990001155851, 001155851
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 20, 1968 | 00-115-5851 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-115-5851
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY100UY-59-A6 | 83298 | ALLIED SIGNAL INCAEROSPACE EQUIPMENT SYSTEMS |
| 10CT-302-E-36/10 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 55139 | 99479 | BOWMAR, LLC |
| 7901521-2 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| AY100UY-59-A6 | 64547 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| ETH-10-CKS-004/A004 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-115-5851
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 12.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 80.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 595.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2130.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 126.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 427.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 750.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 369.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 410.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 126.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 20.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8370 INCHES NOMINAL |
| 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 |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 1.411 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 3.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |