NSN 5990-00-114-1570

Part Details | CONTROL TRANSFORMER SYNCHRO

5990-00-114-1570 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.

Alternate Parts: 7901416, AY100UY82A1, 35631000301, 3563100-0301, AY100UY82A1, 35631000301, 3563100-0301, EGH10CKS5, EGH-10-CKS-5, EGH10CKS5, 5990-00-114-1570, 00-114-1570, 5990001141570, 001141570

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59SEP 20, 196800-114-157015289 ( SYNCHRO, CONTROL TRANSFORMER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND B

SYNCHRO,CONTROL TRA | 5990-00-114-1570, 001141570
Cross Reference | NSN 5990-00-114-1570
Part Number Cage Code Manufacturer
790141693322GE AVIATION SYSTEMS LLCDBA GE AVIATION
AY100UY82A196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
3563100-030196774HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
AY100UY82A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
3563100-030155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
EGH-10-CKS-599932MOOG INC.DBA MOOG COMPONENTS GROUP
EGH10CKS586917VWR SCIENTIFIC INC
Technical Data | NSN 5990-00-114-1570
Characteristic Specifications
BODY SIZE10
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
STATOR INPUT CURRENT RATING78.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING310.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS250.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS575.00 NOMINAL
ZSO RESISTANCE IN OHMS50.00 NOMINAL
PLUS J ZSO REACTANCE IN OHMS120.00 NOMINAL
ZRS RESISTANCE IN OHMS315.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS115.00 NOMINAL
ROTOR DC RESISTANCE IN OHMS176.00 NOMINAL
STATOR DC RESISTANCE IN OHMS45.00 NOMINAL
PHASE SHIFT ANGLE IN DEG14.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT40.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM14.0/P14.0
BODY STYLE STANDARD ROUND B
SHOULDER DIAMETER0.8123 INCHES NOMINAL
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.7120 INCHES MAXIMUM
FLANGE DIAMETER0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2410 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY7 SCREW
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
FRAGILITY FACTOR MODERATELY RUGGED