NSN 5990-00-090-3461

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-090-3461 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: 508312S9L, 508-312S9L, 99924SCEE1011, 99924SCEE101-1, 5990-00-090-3461, 00-090-3461, 5990000903461, 000903461

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59NOV 29, 197200-090-346115289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

SYNCHRO,CONTROL TRA | 5990-00-090-3461, 000903461
Cross Reference | NSN 5990-00-090-3461
Part Number Cage Code Manufacturer
508-312S9L99473HAWKER PACIFIC AEROSPACELANDING GEAR AND COMPONENTS MFG AND
99924SCEE101-126512NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS
Technical Data | NSN 5990-00-090-3461
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING35.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING85.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS470.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS1770.00 NOMINAL
ZSO RESISTANCE IN OHMS81.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS330.00 NOMINAL
ZRS RESISTANCE IN OHMS11.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS2.00 NOMINAL
ZRS IMPEDANCE MAGNITUDE IN OHMS830.00 MINIMUM AND 940.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG16.00 MINIMUM AND 20.00 MAXIMUM
ROTOR DC RESISTANCE IN OHMS365.00 NOMINAL
STATOR DC RESISTANCE IN OHMS64.00 NOMINAL
TRANSFORMATION RATIO2.203 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG10.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE12.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT25.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM5.0/P5.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS6.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.4050 INCHES MAXIMUM
FLANGE DIAMETER0.7500 INCHES NOMINAL
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.7470 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.0150 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING