NSN 5990-00-904-0324

Part Details | TRANSMITTER SYNCHRO

5990-00-904-0324 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: AY100SA49A1, AY100SA49A1, CGH10AS9, CGH-10-AS-9, 5990-00-904-0324, 00-904-0324, 5990009040324, 009040324

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-904-032402073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-904-0324
Part Number Cage Code Manufacturer
AY100SA49A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY100SA49A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
CGH-10-AS-999932MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-00-904-0324
Characteristic Specifications
BODY SIZE10
ROTOR INPUT VOLTAGE RATING IN VOLTS115.0 NOMINAL
ROTOR INPUT CURRENT RATING33.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING780.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS725.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS3410.00 NOMINAL
ZSO RESISTANCE IN OHMS7.70 NOMINAL
PLUS J ZSO REACTANCE IN OHMS30.50 NOMINAL
ROTOR DC RESISTANCE IN OHMS500.00 NOMINAL
STATOR DC RESISTANCE IN OHMS7.30 NOMINAL
TRANSFORMATION RATIO0.103 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG8.500 INPUT TO OUTPUT NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM6.0/P6.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS9.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.00 CENTIMETER-GRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG3000.0 MILLIMETER-MILLIGRAMS 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 LENGTH1.6160 INCHES NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0630 INCHES NOMINAL
UNDERCUT DIAMETER0.8370 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0500 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
FRAGILITY FACTOR MODERATELY RUGGED