Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-778-3675 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: 113A2B, VCT23364B, VCT23364B, VCT23/36-4B, AY240BA2A1, AY2401C2D2, AY240BA2A1, AY2401C2D2, 113A2B, 5990-00-778-3675, 00-778-3675, 5990007783675, 007783675
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-778-3675 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-778-3675
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 113A2B | 99479 | BOWMAR, LLC |
| VCT23364B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VCT23/36-4B | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| AY240BA2A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY2401C2D2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY240BA2A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY2401C2D2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 113A2B | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
Technical Data | NSN 5990-00-778-3675
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| STATOR INPUT CURRENT RATING | 7.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 80.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 0.735 ROTOR TO STATOR NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5900 INCHES MINIMUM AND 0.6000 INCHES MAXIMUM |
| SECOND SHOULDER DIAMETER | 1.9980 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.1700 INCHES NOMINAL |
| OVERALL LENGTH | 4.2430 INCHES MINIMUM AND 4.2940 INCHES MAXIMUM |
| FLANGE DIAMETER | 2.2490 INCHES MINIMUM AND 2.2500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9850 INCHES MINIMUM AND 1.9900 INCHES MAXIMUM |
| PILOT LENGTH | 0.0460 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2470 INCHES MINIMUM AND 0.2520 INCHES MAXIMUM |
| AFT OF FIRST FLANGE DIAMETER | 1.9985 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.4300 INCHES MINIMUM AND 3.4430 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 7 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |