NSN 5990-00-853-1123
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-853-1123 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: AY986T1, AY986T1, 7371012, 737101-2, 410306, 4103-06, CTH11BN5A536, CTC11BN50, 5990-00-853-1123, 00-853-1123, 5990008531123, 008531123
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-853-1123 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-853-1123
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY986T1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY986T1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 737101-2 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 4103-06 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH11BN5A536 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTC11BN50 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-853-1123
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 54.00 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 500.00 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 75.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 405.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 16.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 75.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 80.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 55.00 NOMINAL |
| TRANSFORMATION RATIO | 2.160 ROTOR TO STATOR MINIMUM AND 2.180 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 7.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 0.04 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.2490 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9800 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6870 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
