NSN 5990-01-105-4953

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-01-105-4953 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: CR40928002, CR40928002, 854340, 854340, 5990-01-105-4953, 01-105-4953, 5990011054953, 011054953

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59DEC 23, 198001-105-495302071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND C

1 ROTOR, 1 STATOR

Cross Reference | NSN 5990-01-105-4953
Part Number Cage Code Manufacturer
CR4092800288818KEARFOTT CORPORATIONDBA KEARFOTT
CR4092800205088KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS
8543401PQF4L3 TECHNOLOGIES, INC.DBA LINK SIMULATION & TRAINING
85434036378RAYTHEON TECHNICAL SERVICES COMPANY
Technical Data | NSN 5990-01-105-4953
Characteristic Specifications
BODY SIZE11
STATOR INPUT VOLTAGE RATING IN VOLTS10.0 NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
STATOR DC RESISTANCE IN OHMS180.00 NOMINAL
TORQUE GRADIENT PER ANGULAR DEG1600.0 MILLIMETER-MILLIGRAMS NOMINAL
BODY STYLE STANDARD ROUND C
SHOULDER DIAMETER1.0000 INCHES MAXIMUM
PILOT DIAMETER0.6250 INCHES MAXIMUM
OVERALL LENGTH1.8940 INCHES NOMINAL
FLANGE DIAMETER1.0620 INCHES NOMINAL
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER0.9750 INCHES NOMINAL
UNDERCUT WIDTH0.0500 INCHES NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHOULDER LENGTH0.0620 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.3820 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY4 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
SHAFT RADIAL PLAY DETERMINING WEIGHT4.0 OUNCES
SHAFT END PLAY0.0020 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM
SHAFT MAXIMUM RUNOUT0.0008 INCHES
SCHEMATIC DIAGRAM DESIGNATOR 1 ROTOR, 1 STATOR
FRAGILITY FACTOR MODERATELY RUGGED