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)
59JAN 01, 196300-504-900915289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-504-9009
Part Number Cage Code Manufacturer
AY503-3A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY503-3A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
714054-256232LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN
Technical Data | NSN 5990-00-504-9009
Characteristic Specifications
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING80.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING300.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS250.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS575.00 NOMINAL
ZSO RESISTANCE IN OHMS50.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS120.00 NOMINAL
ZRS RESISTANCE IN OHMS315.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS114.50 NOMINAL
STATOR DC RESISTANCE IN OHMS45.00 NOMINAL
PHASE SHIFT ANGLE IN DEG14.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT50.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.5/P7.5
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6540 INCHES NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2790 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0620 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
FRAGILITY FACTOR MODERATELY RUGGED