NSN 5990-00-539-7329

Part Details | TRANSMITTER SYNCHRO

5990-00-539-7329 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: AY4011, AY401-1, AYA4011A, AYA401-1A, AY4011, AY401-1, AYA4011A, AYA401-1A, AY4011A, AY401-1A, 5990-00-539-7329, 00-539-7329, 5990005397329, 005397329

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-539-732902073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-539-7329
Part Number Cage Code Manufacturer
AY401-196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AYA401-1A96774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY401-119315HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND
AYA401-1A19315HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND
AY401-1A55972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-539-7329
Characteristic Specifications
BODY SIZE22
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING900.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING5.0 WATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ROTOR DC RESISTANCE IN OHMS0.60 NOMINAL
STATOR DC RESISTANCE IN OHMS0.26 NOMINAL
PHASE SHIFT ANGLE IN DEG50.000 INPUT TO OUTPUT NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS45.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.9990 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM
PILOT DIAMETER0.7495 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
OVERALL LENGTH3.1720 INCHES NOMINAL
FLANGE DIAMETER2.1600 INCHES MINIMUM AND 2.1610 INCHES MAXIMUM
FLANGE THICKNESS0.1230 INCHES MINIMUM AND 0.1270 INCHES MAXIMUM
UNDERCUT DIAMETER1.9970 INCHES MINIMUM AND 2.0030 INCHES MAXIMUM
UNDERCUT WIDTH0.1000 INCHES NOMINAL
PILOT LENGTH0.0600 INCHES NOMINAL
SHOULDER LENGTH0.1980 INCHES MINIMUM AND 0.2020 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE2.6120 INCHES NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ANY ACCEPTABLE
FRAGILITY FACTOR MODERATELY RUGGED