5990-00-504-6031 SYNCHRO,TRANSMITTER Index 5990-00-504-6035 SYNCHRO,DIFFERENTIAL TRANSMITTER

National Stock Number:
5990-00-504-6032

Federal Supply Class:
5990

National Item Identification Number:
005046032

Description:
SYNCHRO,TRANSMITTER

Detail:
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.


Manufacturer Information:
104729359364HONEYWELL INTERNATIONAL INC.
104729377068ALLIED-SIGNAL INC DBA ALLIED-SIGNAL AEROSPACE CO ELECTRODYNAMICS DIV
15TX504-60322X130MOTION DEVICES TECHNOLOGY, INC.
3563150-030455972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
3563150-030496774HONEYWELL INTERNATIONAL INC.
4022-0299932MOOG INC.
70656019315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
7411380P294271LOCKHEED MARTIN CORP
986804-110001NAVAIR AND NAVSEA MANAGED ORIGINAL DESIGN ACTIVITY DWG NOT MATERIAL/PARTS SUPPLIER
986804-14K539POLYTECH DEFENSE SPARES LLC
AY201S-1-B98897LOCKHEED MARTIN CORP
AY201S-1B19315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
AY201S102987HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX FLIGHT SYSTEMS FIV MONTROSE OPNS
AY201S1B02987HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX FLIGHT SYSTEMS FIV MONTROSE OPNS
AY201S1B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY201S1B7Y670INSTRUMENT SUPPORT INC
AY201S1B96774HONEYWELL INTERNATIONAL INC.
AY201S1B155972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
AY201S1B196774HONEYWELL INTERNATIONAL INC.
D785671-1255972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
D785671-1296774HONEYWELL INTERNATIONAL INC.


Techincal Specification:
ROTOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
ROTOR INPUT CURRENT RATING250.0 MILLIAMPERES MAXIMUM
ROTOR INPUT ELECTRICAL POWER RATING1.1 WATTS MAXIMUM
FREQUENCY IN HERTZ400.0 NOMINAL
TERMINAL TYPE AND QUANTITY5 WIRE LEAD
BODY SIZE15
BODY MATERIALALUMINUM
ZRO RESISTANCE IN OHMS9.00 NOMINAL
PLUS J ZRO REACTANCE IN OHMS134.00 NOMINAL
ZSO RESISTANCE IN OHMS5.10 NOMINAL
PLUS J ZSO REACTANCE IN OHMS22.10 NOMINAL
ZRS RESISTANCE IN OHMS2.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS13.00 NOMINAL
TRANSFORMATION RATIO0.454 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG4.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE30.0 DEG CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-1.0 TO 1.0
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS30.0 CENTIMETER-GRAMS MAXIMUM
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS10.0 CENTIMETER-GRAMS MAXIMUM
TORQUE GRADIENT PER ANGULAR DEG3000.0 MILLIMETER-MILLIGRAMS MINIMUM
BODY STYLESTANDARD ROUND C
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND
1.3120 INCHES MAXIMUM
PILOT DIAMETER0.4995 INCHES MINIMUM AND
0.5000 INCHES MAXIMUM
OVERALL LENGTH2.1310 INCHES NOMINAL
FLANGE DIAMETER1.4360 INCHES MINIMUM AND
1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
UNDERCUT DIAMETER1.3120 INCHES NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
SHOULDER LENGTH0.1320 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.5910 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8750 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT DIAMETER0.1195 INCHES MINIMUM AND
0.1200 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.5400 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0210 INCHES MINIMUM AND
0.0310 INCHES MAXIMUM SINGLE SHAFT
SHAFT SLOT WIDTH0.0210 INCHES MINIMUM AND
0.0310 INCHES MAXIMUM SINGLE SHAFT
TERMINAL LOCATIONREAR
FRAGILITY FACTORMODERATELY RUGGED
THE MANUFACTURERS DATA
MANUFACTURERS CODE96774
DESIGN CONTROL REFERENCEAY201S1B


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