NSN 5990-00-503-0386
Part Details | TRANSMITTER SYNCHRO
5990-00-503-0386 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.
Alternate Parts: 31TX4AMK35, 31TX4A, 31TX4A, MILS16892, MIL-S-16892, LD267400, 988651, 878447, 1480407, 0S3883TYPE31TX4, LD413194, LD273384, E11360, 121F2A, 10515526, 5990-00-503-0386, 00-503-0386, 5990005030386, 005030386
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-503-0386 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-503-0386
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 31TX4AMK35 | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 31TX4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 31TX4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-16892 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| LD267400 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 988651 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 878447 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 1480407 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 0S3883TYPE31TX4 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| LD413194 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| LD273384 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| E11360 | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 121F2A | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 10515526 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-503-0386
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 31 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.76 AMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 17.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| TRANSFORMATION RATIO | 0.783 STATOR TO ROTOR NOMINAL |
| MAXIMUM TEMP RISE | 60.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 75.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 100.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.50 INCH-OUNCES MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.20 INCH-OUNCES MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 0.670 INCH-OUNCES MINIMUM |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.3120 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 2.7500 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| OVERALL LENGTH | 5.2000 INCHES MAXIMUM |
| FLANGE DIAMETER | 3.1000 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 2.7000 INCHES MAXIMUM |
| PILOT LENGTH | 0.0300 INCHES NOMINAL |
| SHOULDER LENGTH | 0.6150 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 2.7500 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 4.4300 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| TEST DATA DOCUMENT | 81349-MIL-S-16892 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--16892-31TX4A GOVERNMENT SPECIFICATION |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES MAXIMUM |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 16.0 OUNCES |
| SHAFT END PLAY | 0.0040 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 48.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0005 INCHES |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| FRAGILITY FACTOR | MODERATELY RUGGED |