NSN 5990-00-977-8096

Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO

5990-00-977-8096 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.

Alternate Parts: 26V08CDX4C, M2070880001, M20708/80-001, M2070880D001, M20708-80D001, MILS2070880, MIL-S-20708/80, 126V08CDX4C, M207088001C, M20708/80-01C, 26V08CDX4C8001C, 26V-08CDX4C/80-01C, 26V08CDX4C8001C, 26V-08CDX4C/80-01C, AS2070880, AS20708/80, M207088001C, M20708/80-01C, AS2070880, AS20708/80, 5990-00-977-8096, 00-977-8096, 5990009778096, 009778096

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
59MAR 11, 197000-977-809602071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER )
REFERENCE DRAWINGS & PICTURES

STANDARD ROUND A

Cross Reference | NSN 5990-00-977-8096
Part Number Cage Code Manufacturer
26V08CDX4C51761CDA INTERCORP LLC
M20708/80-00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708-80D00181349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
MIL-S-20708/8081349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
126V08CDX4C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
M20708/80-01C81349MILITARY SPECIFICATIONSPROMULGATED BY MILITARY
26V-08CDX4C/80-01C99932MOOG INC.DBA MOOG COMPONENTS GROUP
26V-08CDX4C/80-01C4H618MOOG INC.DBA MOOG COMPONENTS GROUP
AS20708/800VH01SAE CUSTOMER SERVICEDEPT 2045
M20708/80-01C81343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AS20708/8081343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 5990-00-977-8096
Characteristic Specifications
BODY SIZE8
STATOR INPUT VOLTAGE RATING IN VOLTS11.8 NOMINAL
STATOR INPUT CURRENT RATING108.0 MILLIAMPERES MAXIMUM
STATOR INPUT ELECTRICAL POWER RATING240.0 MILLIWATTS NOMINAL
FREQUENCY IN HERTZ400.0 NOMINAL
ZSO IMPEDANCE MAGNITUDE IN OHMS95.00 MINIMUM AND 120.00 MAXIMUM
ZSO IMPEDANCE ANGLE IN DEG74.00 MINIMUM AND 79.00 MAXIMUM
ZRS IMPEDANCE MAGNITUDE IN OHMS35.00 MINIMUM AND 48.00 MAXIMUM
ZRS IMPEDANCE ANGLE IN DEG15.00 MINIMUM AND 20.00 MAXIMUM
TRANSFORMATION RATIO1.154 ROTOR TO STATOR NOMINAL
PHASE SHIFT ANGLE IN DEG9.500 INPUT TO OUTPUT NOMINAL
MAXIMUM TEMP RISE20.0 DEG CELSIUS
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT20.00 OUTPUT
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT30.00
ELECTRICAL ERROR ANGULAR RANGE IN MINUTESM7.0/P7.0
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS0.04 INCH-OUNCES MAXIMUM
BODY STYLE STANDARD ROUND A
PILOT DIAMETER0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM
OVERALL LENGTH1.6150 INCHES NOMINAL
FLANGE DIAMETER0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM
FLANGE THICKNESS0.0620 INCHES NOMINAL
UNDERCUT DIAMETER0.6870 INCHES NOMINAL
UNDERCUT WIDTH0.0620 INCHES NOMINAL
PILOT LENGTH0.0400 INCHES NOMINAL
MOUNTING SURFACE TO TERMINAL END DISTANCE1.2400 INCHES MAXIMUM
TERMINAL TYPE AND QUANTITY6 WIRE LEAD
TERMINAL LOCATION REAR
BODY MATERIAL STEEL, CORROSION RESISTING
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.).
SPECIFICATION/STANDARD DATA81349-MIL--20708 TO 80 GOVERNMENT SPECIFICATION
FRAGILITY FACTOR MODERATELY RUGGED
END ITEM IDENTIFICATIONAIRCRAFT, STARLIFTER C-141