Part Details | RECEIVER-TRANSMITTER SYNCHRO
5990-00-898-1393 A synchro having a dual purpose. It may be used in applications requiring either a receiver or transmitter. For synchros having a single purpose, see SYNCHRO, RECEIVER and SYNCHRO, TRANSMITTER.
Alternate Parts: 31TX4D, E10362717, E103627-17, 31TRX4, VTRX314N1, VTRX31-4N1, VTRX314A1, VTRX31-4A1, M207086201A, M20708/62-01A, 31TX4A, AY3101B4E2, 7755582P001, M20708162001, M20708162-001, M2070862C001, M20708/62C-001, M207086201A, M20708/62-01A, M207086201, M20708/62-01, M2070862001, M20708/62-001, MILS2070862001, MIL-S-20708/62-001, MILS2070862, MIL-S-20708/62, E10362717, E103627-17, AS2070862, AS20708/62, 4509049829, 450904-9829, AS2070862, AS20708/62, AS2070862, AS20708/62, M207086201A, M20708/62-01A, 5990-00-898-1393, 00-898-1393, 5990008981393, 008981393
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 03, 1967 | 00-898-1393 | 27218 ( SYNCHRO, RECEIVER-TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-898-1393
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 31TX4D | 08160 | BOWEN & COMPANY INC.DBA |
| E103627-17 | 16603 | CONTROL FLOW, INC.DBA WESTECH HEAVY MACHINERY DIVISION |
| 31TRX4 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VTRX31-4N1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| VTRX31-4A1 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| M20708/62-01A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 31TX4A | 98853 | HAMILTON STANDARD ELECTRONICSSYSTEMS INC |
| AY3101B4E2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 7755582P001 | 03538 | LOCKHEED MARTIN CORPORATIONDIV RMS |
| M20708162-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/62C-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/62-01A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/62-01 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/62-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/62-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/62 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| E103627-17 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AS20708/62 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 450904-9829 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| AS20708/62 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| AS20708/62 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| M20708/62-01A | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-898-1393
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 31 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.7 AMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 14.4 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 2.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 60.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 35.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 170.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M36.0/P36.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.670 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 2.6950 INCHES MINIMUM AND 2.7000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.3000 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 2.7490 INCHES MINIMUM AND 2.7500 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| OVERALL LENGTH | 5.1000 INCHES NOMINAL |
| FLANGE DIAMETER | 3.0990 INCHES MINIMUM AND 3.1000 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT LENGTH | 0.0300 INCHES NOMINAL |
| SHOULDER LENGTH | 0.5950 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 2.7490 INCHES MINIMUM AND 2.7500 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 4.3700 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SPECIAL FEATURES | WEAPON SYSTEM ESSENTIAL |
| 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 62 GOVERNMENT SPECIFICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| FRAGILITY FACTOR | MODERATELY RUGGED |
| END ITEM IDENTIFICATION | FORRESTAL CLASS CV; STURGEON CLASS SSN (637); LOS ANGELES CLASS SSN (688); TICONDEROGA CLASS CG (47); GUN FIRE CONTROL SYSTEM, MK 68; NIMITZ CLASS CVN; SPRUANCE CLASS DD (963); VIRGINIA CLASS CGN (41); WMIS, WIND MEASURING AND INDICATING SYSTEMS |