NSN 5990-00-901-1358

Part Details | DIFFERENTIAL RECEIVER SYNCHRO

5990-00-901-1358 A synchro, the rotor of which is free to turn, which will assume a position in accordance with the sum or difference of the electrical angular information received from two transmitter synchros. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: AY330T15A3, AY330T15A3, 5990-00-901-1358, 00-901-1358, 5990009011358, 009011358

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196000-901-135802070 ( SYNCHRO, DIFFERENTIAL RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-901-1358
Part Number Cage Code Manufacturer
AY330T15A396774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY330T15A355972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-901-1358
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS10.2 NOMINAL
STATOR INPUT CURRENT RATING93.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING240.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO RESISTANCE IN OHMS28.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS105.00 NOMINAL
TRANSFORMATION RATIO1.160 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT70.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM20.0/P20.0
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.7220 INCHES NOMINAL
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0780 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.5000 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM ALLOY
FRAGILITY FACTOR MODERATELY RUGGED