NSN 5990-00-503-4126
Part Details | TRANSMITTER SYNCHRO
5990-00-503-4126 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: 591C273, 591C27-3, VTX23364A, VTX23/36-4A, 35632400503, 3563240-0503, AY240AA 4 A1, AY240AA 4 A1, 113F2A, C7378341, C737834-1, 23TX4, MILS20708, MILS16892, 113F2A, 23TX4, AS2070894, AS20708/94, 7674818, 5990-00-503-4126, 00-503-4126, 5990005034126, 005034126
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-503-4126 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND D
Cross Reference | NSN 5990-00-503-4126
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 591C27-3 | 94033 | CARDWELL CONDENSER CORPLAPOINTE-ADMIRAL DIV |
| VTX23/36-4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 3563240-0503 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY240AA 4 A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY240AA 4 A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 113F2A | C1834 | KONTRON AG |
| C737834-1 | 49671 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 23TX4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS16892 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 113F2A | 95542 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
| 23TX4 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS20708/94 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 7674818 | 19200 | US ARMY ARDEC RDECOM |
Technical Data | NSN 5990-00-503-4126
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 23 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.21 AMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 0.36 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 105.00 NOMINAL |
| ZRO IMPEDANCE ANGLE IN DEG | 86.00 NOMINAL |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M8.0/P8.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.130 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND D |
| SHOULDER DIAMETER | 1.9950 INCHES NOMINAL |
| PILOT DIAMETER | 0.6000 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 1.9995 INCHES NOMINAL |
| SECOND SHOULDER LENGTH | 0.1540 INCHES NOMINAL |
| OVERALL LENGTH | 4.2990 INCHES NOMINAL |
| FLANGE DIAMETER | 2.2500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 1.9840 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| SHOULDER LENGTH | 0.2660 INCHES NOMINAL |
| AFT OF FIRST FLANGE DIAMETER | 1.9950 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 3.5800 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| 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.). |
| FRAGILITY FACTOR | MODERATELY RUGGED |