NSN 5990-00-773-9771

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-773-9771 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: 35630809043, AY305S15A1, AY305S-15A1, 35630809043, AY305S15A1, AY305S-15A1, 5990-00-773-9771, 00-773-9771, 5990007739771, 007739771

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-773-977115289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-773-9771
Part Number Cage Code Manufacturer
3563080904396774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY305S-15A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
3563080904355972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
AY305S-15A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-773-9771
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS10.2 NOMINAL
STATOR INPUT CURRENT RATING94.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING250.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO RESISTANCE IN OHMS28.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS105.00 NOMINAL
ZRS RESISTANCE IN OHMS36.10 NOMINAL
PLUS J ZRS REACTANCE IN OHMS17.40 NOMINAL
STATOR DC RESISTANCE IN OHMS25.00 NOMINAL
TRANSFORMATION RATIO2.250 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS9.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.7840 INCHES NOMINAL
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
FRAGILITY FACTOR MODERATELY RUGGED