NSN 5990-00-504-9009
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-504-9009 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: AY5033A1, AY503-3A1, AY5033A1, AY503-3A1, 7140542, 714054-2, 5990-00-504-9009, 00-504-9009, 5990005049009, 005049009
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-504-9009 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-504-9009
Part Number | Cage Code | Manufacturer |
---|---|---|
AY503-3A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY503-3A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
714054-2 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
Technical Data | NSN 5990-00-504-9009
Characteristic | Specifications |
---|---|
BODY SIZE | 10 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 80.0 MILLIAMPERES NOMINAL |
STATOR INPUT ELECTRICAL POWER RATING | 300.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 250.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 575.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 50.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 120.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 315.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 114.50 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 45.00 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 14.000 INPUT TO OUTPUT NOMINAL |
MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 50.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.5/P7.5 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.6540 INCHES NOMINAL |
FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0380 INCHES NOMINAL |
SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2790 INCHES NOMINAL |
ALIGNMENT HOLE DEPTH | 0.0620 INCHES NOMINAL |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 3 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
FRAGILITY FACTOR | MODERATELY RUGGED |