NSN 5990-00-295-8235

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-295-8235 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: 7856712, 785671-2, 785671REVADPT2, 7856712, 785671-2, 785671REVADPT2, 5990-00-295-8235, 00-295-8235, 5990002958235, 002958235

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196300-295-823515289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

SYNCHRO,CONTROL TRA | 5990-00-295-8235, 002958235
Cross Reference | NSN 5990-00-295-8235
Part Number Cage Code Manufacturer
785671-296774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
785671REVADPT219315HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND
785671-255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
785671REVADPT255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-295-8235
Characteristic Specifications
BODY SIZE15
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING650.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING330.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO RESISTANCE IN OHMS18.30 NOMINAL
PLUS J ZSO REACTANCE IN OHMS85.00 NOMINAL
TRANSFORMATION RATIO1.600 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG7.000 INPUT TO OUTPUT NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM10.0/P10.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH2.4310 INCHES NOMINAL
FLANGE DIAMETER1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 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, STAINLESS
FRAGILITY FACTOR MODERATELY RUGGED