5306-00-603-9309 BOLT,MACHINE Index 6220-00-603-9314 STOP LIGHT-TAILLIGHT,VEHICULAR

National Stock Number:
5990-00-603-9313

Federal Supply Class:
5990

National Item Identification Number:
006039313

Description:
SYNCHRO,DIFFERENTIAL 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:
11CDX4B81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708-81C-00281349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
M20708/81-02B0U583SAE INTERNATIONAL
SAE-AS20708/810U583SAE INTERNATIONAL
M20708/81-02B81349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
MIL-S-20708/8181349MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M


Techincal Specification:
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES-7.0 TO 7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.07 INCH-OUNCES MAXIMUM
ALIGNMENT HOLE BOLT CIRCLE DIAMETER0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM
ALIGNMENT HOLE QUANTITY4
ALIGNMENT HOLE DEPTH0.2500 INCHES MINIMUM
BODY STYLESTANDARD ROUND C
BODY SIZE11
FLANGE DIAMETER1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM
FLANGE THICKNESS0.0930 INCHES NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
LENGTH0.0620 INCHES NOMINAL SHOULDER
OVERALL LENGTH2.2460 INCHES MAXIMUM
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT60.00 OUTPUT
MAXIMUM TEMP RISE20.0 CELSIUS
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT90.00
MOUNTING SURFACE TO TERMINAL END DISTANCE1.8510 INCHES MAXIMUM
PILOT DIAMETER0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM
PHASE SHIFT ANGLE IN DEG4.000 INPUT TO OUTPUT NOMINAL
PILOT LENGTH0.0620 INCHES NOMINAL
SHAFT DIAMETER0.1198 INCHES MINIMUM AND 0.1200 INCHES MAXIMUM SINGLE SHAFT
SHAFT LENGTH0.3680 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT DEPTH0.0250 INCHES NOMINAL SINGLE SHAFT
SHAFT SLOT WIDTH0.0200 INCHES NOMINAL SINGLE SHAFT
SHAFT TYPEROUND, SLOTTED SINGLE SHAFT
SHOULDER DIAMETER0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG23.00 MINIMUM AND 33.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS470.00 MINIMUM AND 570.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG79.00 MINIMUM AND 85.00 MAXIMUM
ZSO IMPEDANCE MAGNITUDE IN OHMS1590.00 MINIMUM AND 2050.00 MAXIMUM
TERMINAL LOCATIONREAR
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TEST DATA DOCUMENT81349-MIL-S-20708 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
UNDERCUT DIAMETER0.9700 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL


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