NSN 5990-00-136-7127

Part Details | RECEIVER SYNCHRO

5990-00-136-7127 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: AY110DL121B1, 1497781, AY110DL121B1, 1497781, 5990-00-136-7127, 00-136-7127, 5990001367127, 001367127

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 24, 196900-136-712702072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

SYNCHRO,RECEIVER | 5990-00-136-7127, 001367127
Cross Reference | NSN 5990-00-136-7127
Part Number Cage Code Manufacturer
AY110DL121B196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
149778196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY110DL121B155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
149778155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
Technical Data | NSN 5990-00-136-7127
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING95.0 MILLIAMPERES MINIMUM AND 100.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING600.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS44.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS43.00 NOMINAL
ZSO RESISTANCE IN OHMS11.70 NOMINAL
PLUS J ZSO REACTANCE IN OHMS40.50 NOMINAL
ZRS RESISTANCE IN OHMS57.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS28.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS18.00 NOMINAL
STATOR DC RESISTANCE IN OHMS9.30 NOMINAL
PHASE SHIFT ANGLE IN DEG4.000 INPUT TO OUTPUT NOMINAL
RECEIVER ERROR ANGULAR RANGE IN MINUTESM45.0/P45.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS5000.00 MILLIMETER-MILLIGRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG2000.000 MILLIMETER-MILLIGRAMS NOMINAL
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 LENGTH1.9380 INCHES NOMINAL
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 DISTANCE1.6820 INCHES MAXIMUM
ALIGNMENT HOLE DEPTH0.0900 INCHES MINIMUM
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, CORROSION RESISTING