NSN 5990-00-013-1042
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-013-1042 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: 08CT1412, 101222, 10122-2, 08CT0123B, 08CT-0123-B, 35630800170, 3563080-0170, 17838472, 1783847-2, 35630800170, 3563080-0170, CM01004900, CM01002900, CM01004900, CMO1002900, 427701, 4277-01, T427701, T4277-01, 427701, 4277-01, 17838472, 1783847-2, T427701, T4277-01, CTH8A4A013, CTH-8-A-4/A013, CTH8A4A013, CTH-8-A-4/A013, 10392443, 5990-00-013-1042, 00-013-1042, 5990000131042, 000131042
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | APR 25, 1967 | 00-013-1042 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-013-1042
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 08CT1412 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 10122-2 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| 08CT-0123-B | 51761 | CDA INTERCORP LLC |
| 3563080-0170 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1783847-2 | 07187 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0170 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CM01004900 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM01002900 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM01004900 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| CMO1002900 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| 4277-01 | 58880 | MEGGITT (NEW HAMPSHIRE), INC |
| T4277-01 | 58880 | MEGGITT (NEW HAMPSHIRE), INC |
| 4277-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 1783847-2 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| T4277-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-8-A-4/A013 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-8-A-4/A013 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 10392443 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 5990-00-013-1042
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 30.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 73.0 MILLIWATTS NOMINAL |
| 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 |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| 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 | 0.0005 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 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |