NSN 5990-01-016-9256

Part Details | RECEIVER SYNCHRO

5990-01-016-9256 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: 35630800222, 3563080-0222, 2277177, 35630800222, 3563080-0222, 2277177, 08TR0169256, 08TR016-9256, 5990-01-016-9256, 01-016-9256, 5990010169256, 010169256

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59FEB 26, 197601-016-925602072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-01-016-9256
Part Number Cage Code Manufacturer
3563080-022296774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
227717796774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
3563080-022255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
227717755972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
08TR016-92562X130MOTION DEVICES TECHNOLOGY, INC.
Technical Data | NSN 5990-01-016-9256
Characteristic Specifications
BODY SIZE8
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING110.0 AMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING564.0 MILLIWATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS47.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS256.00 NOMINAL
ZSO RESISTANCE IN OHMS11.20 NOMINAL
PLUS J ZSO REACTANCE IN OHMS44.00 NOMINAL
ZRS RESISTANCE IN OHMS83.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS19.00 NOMINAL
PHASE SHIFT ANGLE IN DEG7.600 INPUT TO OUTPUT NOMINAL
RECEIVER ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS0.27 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.54 CENTIMETER-GRAMS NOMINAL
TORQUE GRADIENT PER ANGULAR DEG2200.0 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.7900 INCHES MAXIMUM
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
UNDERCUT DIAMETER0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM
PILOT LENGTH0.0390 INCHES MINIMUM AND 0.0430 INCHES MAXIMUM
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM ALLOY
FRAGILITY FACTOR MODERATELY RUGGED