NSN 5990-00-970-1179

Part Details | TRANSMITTER SYNCHRO

5990-00-970-1179 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.

Alternate Parts: ZD1, AY308HD28A1, AY-308H-D-28-A1, 106077001, 10607700-1, 5990-00-970-1179, 00-970-1179, 5990009701179, 009701179

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59JAN 01, 196200-970-117902073 ( SYNCHRO, TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-970-1179
Part Number Cage Code Manufacturer
ZD151761CDA INTERCORP LLC
AY-308H-D-28-A155972HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS
10607700-118876U S ARMY AVIATION AND MISSILECOMMAND
Technical Data | NSN 5990-00-970-1179
Characteristic Specifications
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING83.0 MILLIAMPERES NOMINAL
ROTOR INPUT ELECTRICAL POWER RATING150.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZRO RESISTANCE IN OHMS70.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS305.00 NOMINAL
ZSO RESISTANCE IN OHMS16.50 NOMINAL
PLUS J ZSO REACTANCE IN OHMS50.00 NOMINAL
ZRS RESISTANCE IN OHMS127.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS23.00 NOMINAL
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS20.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.5000 INCHES NOMINAL
OVERALL LENGTH1.6410 INCHES MAXIMUM
FLANGE DIAMETER0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6880 INCHES MINIMUM AND 0.6900 INCHES MAXIMUM
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 STEEL, CORROSION RESISTING
FRAGILITY FACTOR MODERATELY RUGGED