NSN 5990-00-835-8972

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-835-8972 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: AY63026A1, AY630-26A1, AY63026A1, AY630-26A1, 5078881, 507888-1, 078881, 07888-1, 5990-00-835-8972, 00-835-8972, 5990008358972, 008358972

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-835-897202071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-835-8972
Part Number Cage Code Manufacturer
AY630-26A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY630-26A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
507888-137695RAYTHEON COMPANYDBA RAYTHEON
07888-189212UNITED CAN CO
Technical Data | NSN 5990-00-835-8972
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING210.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING550.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS12.50 NOMINAL
PLUS J ZRO REACTANCE IN OHMS52.00 NOMINAL
ZSO RESISTANCE IN OHMS12.50 NOMINAL
PLUS J ZSO REACTANCE IN OHMS60.50 NOMINAL
ZRS RESISTANCE IN OHMS13.40 NOMINAL
PLUS J ZRS REACTANCE IN OHMS7.80 NOMINAL
ROTOR DC RESISTANCE IN OHMS10.10 NOMINAL
STATOR DC RESISTANCE IN OHMS9.10 NOMINAL
TRANSFORMATION RATIO1.160 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG8.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT25.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS30.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS10.0 CENTIMETER-GRAMS MAXIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH2.0560 INCHES NOMINAL
FLANGE DIAMETER1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6820 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0940 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8120 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING