5990-00-295-9133 SYNCHRO,DIFFERENTIAL TRANSMITTER Index 1285-00-295-9138 CABLE ASSEMBLY,RADI

National Stock Number:
5990-00-295-9135

Federal Supply Class:
5990

National Item Identification Number:
002959135

Description:
SYNCHRO,DIFFERENTIAL TRANSMITTER

Detail:
A SYNCHRO, THE ROTOR OF WHICH IS MECHANICALLY POSITIONED FOR MODIFYING ELECTRICAL ANGULAR INFORMATION, RECEIVED FROM A TRANSMITTER SYNCHRO AND TRANSMITTING TO RECEIVER SYNCHRO OR CONTROL TRANSFORMER SYNCHRO ELECTRICAL INFORMATION CORRESPONDING TO THE SUM OR DIFFERENCE OF THE ELECTRICAL INPUT ANGLE AND ITS ROTOR POSITION ANGLE. DOES NOT INCLUDE VARIABLE RESISTORS, GONIOMETERS, VARIABLE TRANSFORMERS, OR ITEMS WITH DIALS.


Manufacturer Information:
22102836378RAYTHEON TECHNICAL SERVICES COMPANY
230-0076-0013499ROCKWELL COLLINS, INC.
230-0076-00013499ROCKWELL COLLINS, INC.
739436-319315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
AY231-4B19315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
AN3108-22-9S81352AIR FORCE-NAVY AERONAUTICAL SPECIFICATIONS PROMULGATED BY AERONAUTICAL STANDARDS GROUP
AY231S419315HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS FORMER BENDIX NAVIGATION AND CONTROL SYSTEMS
C180328-937695RAYTHEON COMPANY
AY231S4B55972HONEYWELL INTL INC DEFENSE AVIONICS SYSTEMS
PL024780063US ARMY COMMUNICATIONS & ELECTRONICS MATERIEL READINESS COMMAND LOGISTICS ENGINEERING DIR
AY231S4B96774HONEYWELL INTERNATIONAL INC.


Techincal Specification:
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS7.00 CENTIMETER-GRAMS NOMINAL
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS21.00 CENTIMETER-GRAMS NOMINAL
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8750 INCHES NOMINAL
ALIGNMENT HOLE DEPTH0.1250 INCHES NOMINAL
ALIGNMENT HOLE QUANTITY4
BODY MATERIALSTEEL CORROSION RESISTING
BODY SIZE15
BODY STYLESTANDARD ROUND B
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-12.0 TO 12.0
FLANGE DIAMETER1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
FRAGILITY FACTORMODERATELY RUGGED
FREQUENCY IN HERTZ400.0 NOMINAL
LENGTH0.1320 INCHES NOMINAL SHOULDER
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
PILOT LENGTH0.0400 INCHES NOMINAL
PLUS J ZRO REACTANCE IN OHMS38.00 NOMINAL
PLUS J ZRS REACTANCE IN OHMS5.60 NOMINAL
PLUS J ZSO REACTANCE IN OHMS39.00 NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.5910 INCHES NOMINAL
OVERALL LENGTH2.1310 INCHES NOMINAL
ROTOR DC RESISTANCE IN OHMS7.50 NOMINAL
SHAFT DIAMETER0.1195 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM 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
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHAFT LENGTH0.5400 INCHES NOMINAL SINGLE SHAFT
SHOULDER DIAMETER1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM
STATOR DC RESISTANCE IN OHMS6.10 NOMINAL
STATOR INPUT CURRENT RATING410.0 MILLIAMPERES NOMINAL
STATOR INPUT ELECTRICAL POWER RATING2.3 WATTS NOMINAL
STATOR INPUT VOLTAGE RATING IN VOLTS26.0 NOMINAL
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TRANSFORMATION RATIO1.000 ROTOR TO STATOR NOMINAL
UNDERCUT WIDTH0.0780 INCHES NOMINAL
ZRO RESISTANCE IN OHMS9.80 NOMINAL
ZRS RESISTANCE IN OHMS9.60 NOMINAL
ZSO RESISTANCE IN OHMS9.20 NOMINAL


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