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) |
---|---|---|---|
59 | MAR 11, 1970 | 00-977-8096 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A

Cross Reference | NSN 5990-00-977-8096
Part Number | Cage Code | Manufacturer |
---|---|---|
26V08CDX4C | 51761 | CDA INTERCORP LLC |
M20708/80-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
M20708-80D001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
MIL-S-20708/80 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
126V08CDX4C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
M20708/80-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
26V-08CDX4C/80-01C | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
26V-08CDX4C/80-01C | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
AS20708/80 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
M20708/80-01C | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
AS20708/80 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-977-8096
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
STATOR INPUT CURRENT RATING | 108.0 MILLIAMPERES MAXIMUM |
STATOR INPUT ELECTRICAL POWER RATING | 240.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZSO IMPEDANCE MAGNITUDE IN OHMS | 95.00 MINIMUM AND 120.00 MAXIMUM |
ZSO IMPEDANCE ANGLE IN DEG | 74.00 MINIMUM AND 79.00 MAXIMUM |
ZRS IMPEDANCE MAGNITUDE IN OHMS | 35.00 MINIMUM AND 48.00 MAXIMUM |
ZRS IMPEDANCE ANGLE IN DEG | 15.00 MINIMUM AND 20.00 MAXIMUM |
TRANSFORMATION RATIO | 1.154 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT NOMINAL |
MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.04 INCH-OUNCES MAXIMUM |
BODY STYLE | STANDARD ROUND A |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.6150 INCHES NOMINAL |
FLANGE DIAMETER | 0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6870 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
TEST DATA DOCUMENT | 81349-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 DATA | 81349-MIL--20708 TO 80 GOVERNMENT SPECIFICATION |
FRAGILITY FACTOR | MODERATELY RUGGED |
END ITEM IDENTIFICATION | AIRCRAFT, STARLIFTER C-141 |