NSN 5990-00-913-4155

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-913-4155 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.

Alternate Parts: 10CT300E2810, 10CT300E28-10, 663401, 66340-1, AY100FZ59A6, AY100FZ59A6, 5990-00-913-4155, 00-913-4155, 5990009134155, 009134155

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-913-415515289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

Cross Reference | NSN 5990-00-913-4155
Part Number Cage Code Manufacturer
10CT300E28-1006989API HAROWE INCDBA API MOTION DIV API
66340-193322GE AVIATION SYSTEMS LLCDBA GE AVIATION
AY100FZ59A696774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY100FZ59A655972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-913-4155
Characteristic Specifications
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
STATOR INPUT CURRENT RATING27.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING74.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS595.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS2130.00 NOMINAL
ZSO RESISTANCE IN OHMS126.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS427.00 NOMINAL
ZRS RESISTANCE IN OHMS750.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS369.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS409.00 NOMINAL
STATOR DC RESISTANCE IN OHMS126.00 NOMINAL
TRANSFORMATION RATIO0.685 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG6.000 INPUT TO OUTPUT NOMINAL
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT30.00 INPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT70.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS16.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS6.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER0.8123 INCHES NOMINAL
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.6540 INCHES MAXIMUM
FLANGE DIAMETER0.9370 INCHES NOMINAL
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING