NSN 5990-00-913-7052

Part Details | TRANSMITTER SYNCHRO

5990-00-913-7052 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: AY200S77T, AY200S77T, 5990-00-913-7052, 00-913-7052, 5990009137052, 009137052

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-913-705202073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-913-7052
Part Number Cage Code Manufacturer
AY200S77T96774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY200S77T55972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-913-7052
Characteristic Specifications
BODY SIZE15
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING250.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING1.4 WATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS18.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS112.00 NOMINAL
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG4.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT18.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.8810 INCHES NOMINAL
FLANGE DIAMETER1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER1.3120 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.5910 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8750 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
FRAGILITY FACTOR MODERATELY RUGGED