Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-115-5849 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: AY100WY58A6, 55138, 79015202, 7901520-2, 7901520002, 7901520-002, AY100WY58A6, ETH10FMS03B799, 5990-00-115-5849, 00-115-5849, 5990001155849, 001155849
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | SEP 20, 1968 | 00-115-5849 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-115-5849
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY100WY58A6 | 83298 | ALLIED SIGNAL INCAEROSPACE EQUIPMENT SYSTEMS |
| 55138 | 99479 | BOWMAR, LLC |
| 7901520-2 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| 7901520-002 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| AY100WY58A6 | 64547 | HONEYWELL INTERNATIONAL INCDBA HONEYWELL |
| ETH10FMS03B799 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-115-5849
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 10.2 NOMINAL |
| STATOR INPUT CURRENT RATING | 70.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 200.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 225.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 695.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 43.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 141.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 265.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 111.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 135.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 36.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 10.000 INPUT TO OUTPUT MINIMUM AND 11.000 INPUT TO OUTPUT MAXIMUM |
| 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 | 0.8123 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.6920 INCHES MAXIMUM |
| 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 |
| ALIGNMENT HOLE DEPTH | 0.0620 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 6 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |