5895-00-504-9005 AMPLIFIER,ELECTRONIC CONTROL Index 6615-00-504-9026 AMPLIFIER,ELECTRONIC CONTROL

National Stock Number:
5990-00-504-9009

Federal Supply Class:
5990

National Item Identification Number:
005049009

Description:
SYNCHRO,CONTROL TRANSFORMER

Detail:
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.


Manufacturer Information:
714054-256232LOCKHEED MARTIN CORPORATION
AY503-3A155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY503-3A196774HONEYWELL INTERNATIONAL INC.


Techincal Specification:
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING80.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING300.0 MILLIWATTS NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
BODY STYLESTANDARD ROUND C
FREQUENCY IN HERTZ400.0 NOMINAL
BODY SIZE10
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 OHMS114.50 NOMINAL
STATOR DC RESISTANCE IN OHMS45.00 NOMINAL
PHASE SHIFT ANGLE IN DEG14.000 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE10.0 DEG CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT50.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.5 TO 7.5
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS15.0 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS3.0 CENTIMETER-GRAMS NOMINAL
SHOULDER DIAMETER0.8118 INCHES MINIMUM AND
0.8123 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND
0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6540 INCHES NOMINAL
FLANGE DIAMETER0.9360 INCHES MINIMUM AND
0.9370 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.8350 INCHES MINIMUM AND
0.8400 INCHES MAXIMUM
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0380 INCHES NOMINAL
SHOULDER LENGTH0.0630 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2790 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.0620 INCHES NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.6780 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY3
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.0880 INCHES MINIMUM AND
0.0900 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.4130 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0310 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0270 INCHES NOMINAL SINGLE SHAFT
TERMINAL LOCATIONREAR
BODY MATERIALSTEEL, CORROSION RESISTING
FRAGILITY FACTORMODERATELY RUGGED
THE MANUFACTURERS DATA
MANUFACTURERS CODE96774
DESIGN CONTROL REFERENCEAY503-3A1


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