NSN 5990-01-043-9006

Part Details | RECEIVER SYNCHRO

5990-01-043-9006 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: 755140081, 75514008-1, 755140081, 75514008-1, CRH8RB1F098, CRH-8-RB-1/F098, CRH8RB1F098, CRH-8-RB-1/F098, 5990-01-043-9006, 01-043-9006, 5990010439006, 010439006

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JUL 02, 197701-043-900602072 ( SYNCHRO, RECEIVER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-01-043-9006
Part Number Cage Code Manufacturer
75514008-199932MOOG INC.DBA MOOG COMPONENTS GROUP
75514008-11K426MOOG INC.DBA MOOG COMPONENTS GROUP
CRH-8-RB-1/F09899932MOOG INC.DBA MOOG COMPONENTS GROUP
CRH-8-RB-1/F0984H618MOOG INC.DBA MOOG COMPONENTS GROUP
Technical Data | NSN 5990-01-043-9006
Characteristic Specifications
BODY SIZE8
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING100.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING540.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS54.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS260.00 NOMINAL
ZSO RESISTANCE IN OHMS10.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS45.00 NOMINAL
ZRS RESISTANCE IN OHMS88.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS22.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS37.00 NOMINAL
STATOR DC RESISTANCE IN OHMS10.40 NOMINAL
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM30.0/P30.0
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.5000 INCHES MAXIMUM
FLANGE DIAMETER0.7500 INCHES NOMINAL
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6910 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0430 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL ALUMINUM ALLOY
FRAGILITY FACTOR MODERATELY RUGGED