NSN 5990-00-810-1518

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-810-1518 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: 12485102, 124851-02, U904001D, U904-001-D, U904001, U904-001, 4640902, 464090-2, 5990-00-810-1518, 00-810-1518, 5990008101518, 008101518

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-810-151815289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-810-1518
Part Number Cage Code Manufacturer
124851-0235351GE AVIATION SYSTEMS LLC
U904-001-D88818KEARFOTT CORPORATIONDBA KEARFOTT
U904-00188818KEARFOTT CORPORATIONDBA KEARFOTT
464090-296214RAYTHEON COMPANYDBA RAYTHEON
Technical Data | NSN 5990-00-810-1518
Characteristic Specifications
BODY SIZE12
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING21.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING50.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS625.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS3280.00 NOMINAL
ZSO RESISTANCE IN OHMS93.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS570.00 NOMINAL
ZRS RESISTANCE IN OHMS570.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS330.00 NOMINAL
ZSS RESISTANCE IN OHMS106.00 NOMINAL
PLUS J ZSS REACTANCE IN OHMS68.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS385.00 NOMINAL
STATOR DC RESISTANCE IN OHMS60.00 NOMINAL
TRANSFORMATION RATIO2.203 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG4.200 OUTPUT TO INPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT34.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT53.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS120.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS30.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE2 STANDARD ROUND A
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6250 INCHES NOMINAL
OVERALL LENGTH2.9630 INCHES MINIMUM AND 3.0450 INCHES MAXIMUM
FLANGE DIAMETER1.1850 INCHES MINIMUM AND 1.1910 INCHES MAXIMUM
FLANGE THICKNESS0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM
UNDERCUT DIAMETER1.1050 INCHES MINIMUM AND 1.1130 INCHES MAXIMUM
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
SHOULDER LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE2.3110 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
SHAFT MAXIMUM RADIAL PLAY0.0050 INCHES
SHAFT RADIAL PLAY TEST POINT0.125 INCHES MAXIMUM
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0003 INCHES MINIMUM AND 0.0005 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT16.0 OUNCES
SHAFT MAXIMUM RUNOUT0.0010 INCHES
FRAGILITY FACTOR MODERATELY RUGGED