NIIN Output Data
NIIN:
NSN:
Item Name:
SYNCHRO , TRANSMITTER
Definition:
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.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
531500-1 | 96214 | A | C | 1 | 5 | TX | AF | |
AS20708/78 | 0VH01 | A | 5 | 1 | E | ZZ | ||
MIL-S-20708/78 | 81349 | M | 5 | 9 | E | TX | ||
26V-08CX4C/78-01C | 99932 | A | 5 | 1 | 5 | ZZ | ||
M20708/78-001 | 81349 | M | 5 | 9 | E | TX | ||
7101901 | 93322 | A | 5 | 1 | 5 | ZZ | ||
M20708-78D001 | 81349 | M | 5 | 9 | E | TX | ||
M20708/78-01C | 81349 | M | 2 | 2 | E | TX | ||
26V-08CX4C | 81349 | M | 5 | 9 | E | TX |
CAGE Information
Code | Company |
---|---|
0VH01 | SAE CUSTOMER SERVICE DEPT 2045 |
96214 | RAYTHEON COMPANY |
81349 | MILITARY SPECIFICATIONS PROMULGATED |
99932 | MOOG INC. DBA MOOG COMPONENTS GROUP |
93322 | GE AVIATION SYSTEMS LLC DBA GE AVIAT |
Federal Supply Class
Title
SYNCHROS AND RESOLVERS
Inclusions:
Exclusions:
EXCLUDES SYNCHRO SYSTEMS; SERVO MECHANISMS.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
CQTM | TERMINAL LOCATION | REAR |
CRHN | SHAFT SLOT WIDTH | 0.0200 INCHES NOMINAL SINGLE SHAFT |
AJSV | ROTOR INPUT ELECTRICAL POWER RATING | 700.0 MILLIWATTS NOMINAL |
AFJN | FRAGILITY FACTOR | MODERATELY RUGGED |
ABHP | OVERALL LENGTH | 1.6050 INCHES NOMINAL |
ABPA | UNDERCUT DIAMETER | 0.6920 INCHES NOMINAL |
ABWV | SHAFT DIAMETER | 0.0895 INCHES MINIMUM SINGLE SHAFT AND 0.0900 INCHES MAXIMUM SINGLE SHAFT |
ABXF | SHAFT LENGTH | 0.3650 INCHES NOMINAL SINGLE SHAFT |
AJVG | MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 20.00 OUTPUT |
AAQL | BODY STYLE | STANDARD ROUND A |
AGAV | END ITEM IDENTIFICATION | T-37 SUPPORT EQUIPMENT; T-38 SUPPORT EEQUIPMENT; AIRCRAFT, VIKING S-3B; PROWLER EA-6B AIRCRAFT; P-3 ORION; AVIONICS SHOP TEST SYSTEM; CUSTOMER FOCUS POOL; AIR TRAFFIC CONTROL |
ABKK | FLANGE DIAMETER | 0.7470 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
CRSJ | SHAFT TYPE | ROUND, SLOTTED SINGLE SHAFT |
AJST | ROTOR INPUT CURRENT RATING | 153.0 MILLIAMPERES MAXIMUM |
CSJY | TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
TEST | TEST DATA DOCUMENT | 81349-MIL-S-20708 SPECIFICATION |
ABKU | FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
AJWQ | PILOT LENGTH | 0.0400 INCHES NOMINAL |
AJSL | BODY SIZE | 8 |
AJTP | ZSS IMPEDANCE ANGLE IN DEG | 9.00 MINIMUM AND 15.00 MAXIMUM |
AJWX | MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2400 INCHES MAXIMUM |
AJVF | PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
AJVH | MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
AJSS | FREQUENCY IN HERTZ | 400.0 NOMINAL |
AAFZ | BODY MATERIAL | STEEL, CORROSION RESISTING |
FEAT | SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
AAVL | PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
TTQY | TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
AJVT | ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.04 INCH-OUNCES MAXIMUM |
AHCG | MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
AJSR | ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
AJTN | ZSS IMPEDANCE MAGNITUDE IN OHMS | 11.00 MINIMUM AND 15.00 MAXIMUM |
CQZS | SHAFT SLOT DEPTH | 0.0250 INCHES NOMINAL SINGLE SHAFT |
ZZZK | SPECIFICATION/STANDARD DATA | 81349-MIL-S-20708/78 GOVERNMENT SPECIFICATION |
ABPC | UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
AJTG | ZRO IMPEDANCE MAGNITUDE IN OHMS | 170.00 MINIMUM AND 215.00 MAXIMUM |
AJTH | ZRO IMPEDANCE ANGLE IN DEG | 77.50 MINIMUM AND 80.50 MAXIMUM |
AJVL | ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | -7.0/+7.0 |
Similar Parts
AS20708/78 ,
AS2070878 ,
5990-00-465-4829 ,
5990004654829 ,
004654829
,
531500-1 ,
AS20708/78 ,
MIL-S-20708/78 ,
26V-08CX4C/78-01C ,
M20708/78-001 ,
7101901 ,
M20708-78D001 ,
M20708/78-01C ,
26V-08CX4C ,