NSN 5990-00-402-0564

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-402-0564 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: 10CT4DILIS001, 10CT4DILIS-001, 6299071, 629907-1, 6299071, 629907-1, 6299071, 629907-1, 6299071, 629907-1, 6299071, 629907-1, 5990-00-402-0564, 00-402-0564, 5990004020564, 004020564

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59APR 01, 197000-402-056415289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

1 Y-ROTOR, 1 STATOR

Cross Reference | NSN 5990-00-402-0564
Part Number Cage Code Manufacturer
10CT4DILIS-00106989API HAROWE INCDBA API MOTION DIV API
629907-110112GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC.
629907-107217HONEYWELL LIMITEDDBA SYSTEMS SENSOR CANADA
629907-188818KEARFOTT CORPORATIONDBA KEARFOTT
629907-199932MOOG INC.DBA MOOG COMPONENTS GROUP
629907-11K426MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-00-402-0564
Characteristic Specifications
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING24.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING34.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS695.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2600.00 NOMINAL
ZSO RESISTANCE IN OHMS115.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS447.00 NOMINAL
ZRS RESISTANCE IN OHMS874.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS286.00 NOMINAL
TRANSFORMATION RATIO2.203 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 OUTPUT TO INPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT25.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM15.0/P15.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS9.00 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.00 CENTIMETER-GRAMS MAXIMUM
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 LENGTH2.4100 INCHES MINIMUM AND 2.4700 INCHES MAXIMUM
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0630 INCHES MAXIMUM
UNDERCUT DIAMETER0.8300 INCHES MINIMUM AND 0.8500 INCHES MAXIMUM
UNDERCUT WIDTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
PILOT LENGTH0.0350 INCHES MINIMUM AND 0.0410 INCHES MAXIMUM
SHOULDER LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0700 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6750 INCHES MINIMUM AND 0.6810 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY3
SECURING HOLE QUANTITY3
MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR UNF
MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER0.0860 INCHES
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0005 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0010 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
SCHEMATIC DIAGRAM DESIGNATOR 1 Y-ROTOR, 1 STATOR
FRAGILITY FACTOR MODERATELY RUGGED
END ITEM IDENTIFICATION4920-00-400-3818