NSN 5990-00-010-1413

Part Details | TRANSMITTER SYNCHRO

5990-00-010-1413 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: 9011805, AY110615B1, AY1106-15B1, 14970150001, 1497015-0001, 1497015, 14865571, 1486557-1, U219478, U-219478, 5990-00-010-1413, 00-010-1413, 5990000101413, 000101413

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-010-141302073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

SYNCHRO,TRANSMITTER | 5990-00-010-1413, 000101413
Cross Reference | NSN 5990-00-010-1413
Part Number Cage Code Manufacturer
901180597151AIR FORCE LIFECYCLE MANAGEMENTCENTER ELECTRONIC COMPONENTS
AY1106-15B155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
1497015-000155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
149701555972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
1486557-155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
U-21947882686TRANSICOIL LLCDBA ADS/TRANSICOIL
Technical Data | NSN 5990-00-010-1413
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING120.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING600.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS44.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS243.00 NOMINAL
ZSO RESISTANCE IN OHMS57.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS28.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS18.00 NOMINAL
STATOR DC RESISTANCE IN OHMS9.30 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 VOLT25.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM15.0/P15.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS1.8 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.6 CENTIMETER-GRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG2000.0 MILLIMETER-MILLIGRAMS MINIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
OVERALL LENGTH1.9800 INCHES MINIMUM AND 2.0100 INCHES MAXIMUM
FLANGE DIAMETER1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
SHOULDER LENGTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.6200 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0900 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, STAINLESS
FRAGILITY FACTOR MODERATELY RUGGED