Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-022-2957 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: 10CT0133T, 10CT-0133-T, 10CT0133, 10CT-0133, 53484, 5990-00-022-2957, 00-022-2957, 5990000222957, 000222957
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAY 17, 1968 | 00-022-2957 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 5990-00-022-2957
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10CT-0133-T | 51761 | CDA INTERCORP LLC |
| 10CT-0133 | 51761 | CDA INTERCORP LLC |
| 53484 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
Technical Data | NSN 5990-00-022-2957
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 35.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 300.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |