NSN 5990-00-683-1090

Part Details | TRANSMITTER SYNCHRO

5990-00-683-1090 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: AY5038A1, AY503-8A1, AY5038A1, AY503-8A1, 8803903, 5990-00-683-1090, 00-683-1090, 5990006831090, 006831090

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-683-109002073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-683-1090
Part Number Cage Code Manufacturer
AY503-8A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY503-8A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
880390319203PICATINNY ARSENAL
Technical Data | NSN 5990-00-683-1090
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING180.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING1.7 WATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS35.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS145.00 NOMINAL
ZSO RESISTANCE IN OHMS10.40 NOMINAL
PLUS J ZSO REACTANCE IN OHMS33.00 NOMINAL
ZRS RESISTANCE IN OHMS62.50 NOMINAL
PLUS J ZRS REACTANCE IN OHMS26.00 NOMINAL
ZSO-90 RESISTANCE IN OHMS9.10 NOMINAL
PLUS J ZSO-90 REACTANCE IN OHMS10.70 NOMINAL
ROTOR DC RESISTANCE IN OHMS26.00 NOMINAL
STATOR DC RESISTANCE IN OHMS10.90 NOMINAL
PHASE SHIFT ANGLE IN DEG10.500 INPUT TO OUTPUT NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM15.0/P15.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS4.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6540 INCHES NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8370 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0780 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM