NSN 5990-00-253-0261

Part Details | RECEIVER SYNCHRO

5990-00-253-0261 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: AY110BC42B2, AY110BC42B2, 6028942, 602894-2, 413503, 4135-03, URH11CM4B531, URH11CM4/B531, URH11CM4F552, URH-11-CM-4/F552, URH11CM4B531, URH-11-CM-4/B531, 11TR2530261, 11TR253-0261, 5990-00-253-0261, 00-253-0261, 5990002530261, 002530261

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUL 18, 196900-253-026102072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

Cross Reference | NSN 5990-00-253-0261
Part Number Cage Code Manufacturer
AY110BC42B296774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY110BC42B255972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
602894-206401L3 TECHNOLOGIES, INC.DBA COMMUNICATION SYSTEMS-WEST
4135-0399932MOOG INC.DBA MOOG COMPONENTS GROUP
URH11CM4/B53199932MOOG INC.DBA MOOG COMPONENTS GROUP
URH-11-CM-4/F5524H618MOOG INC.DBA MOOG COMPONENTS GROUP
URH-11-CM-4/B5314H618MOOG INC.DBA MOOG COMPONENTS GROUP
11TR253-02612X130MOTION DEVICES TECHNOLOGY, INC.
Technical Data | NSN 5990-00-253-0261
Characteristic Specifications
BODY SIZE11
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING120.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING0.6 WATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS35.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS288.00 NOMINAL
ZSO RESISTANCE IN OHMS8.10 NOMINAL
PLUS J ZSO REACTANCE IN OHMS47.00 NOMINAL
ZRS RESISTANCE IN OHMS49.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS24.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS18.00 NOMINAL
STATOR DC RESISTANCE IN OHMS7.50 NOMINAL
PHASE SHIFT ANGLE IN DEG5.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE15.0 DEG CELSIUS
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
RECEIVER ERROR ANGULAR RANGE IN MINUTESM60.0/P60.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS5400.0 MILLIMETER-MILLIGRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS2700.0 MILLIMETER-MILLIGRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG2250.0 MILLIMETER-MILLIGRAMS MINIMUM
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH2.1860 INCHES MAXIMUM
FLANGE DIAMETER1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.9860 INCHES MAXIMUM
UNDERCUT WIDTH0.0500 INCHES MINIMUM
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.7490 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
SHAFT MAXIMUM RADIAL PLAY0.0010 INCHES
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0020 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM
SHAFT END PLAY DETERMINING WEIGHT8.0 OUNCES
FRAGILITY FACTOR MODERATELY RUGGED