NSN 5990-00-067-6791
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-067-6791 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: 08CT14021, 08CT1402-1, 8CT300B1B15, 8CT-300-B-1B/15, CTH8A4L150, CTH-8-A-4/L150, 13703001, 137030-01, CM010029C8, HTC8A4L150, CTH8A4L150, 5990-00-067-6791, 00-067-6791, 5990000676791, 000676791
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 29, 1967 | 00-067-6791 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-067-6791
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 08CT1402-1 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 8CT-300-B-1B/15 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| CTH-8-A-4/L150 | 1HUX5 | DIMO CORP. |
| 137030-01 | 35351 | GE AVIATION SYSTEMS LLC |
| CM010029C8 | 09301 | KEARFOTT CORP SOMA FORWARDING DIV |
| HTC8A4L150 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH8A4L150 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-067-6791
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 0.1 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 470.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1770.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 81.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 330.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 590.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 190.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
| TRANSFORMATION RATIO | 2.1465 ROTOR TO STATOR MINIMUM AND 2.2165 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 6.000 INPUT TO OUTPUT MINIMUM AND 12.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 6.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M16.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6310 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| FRAGILITY FACTOR | MODERATELY RUGGED |