NSN 5990-00-085-0829
Part Details | RECEIVER-TRANSMITTER SYNCHRO
5990-00-085-0829 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: AY37014C2, AY3701-4C2, 37TRX4A, 808112, 37TX4B, 37TRX4A, M207087001A, M20708-70-01A, M2070870001, M20708-70-001, MILS207087037T, MILS20708-70-37T, MILS2070870, MIL-S-20708/70, AY37014C2, AY3701-4C2, AS2070870, AS20708/70, AJ100291, AJ10029-1, 5990-00-085-0829, 00-085-0829, 5990000850829, 000850829
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | DEC 24, 1967 | 00-085-0829 | 27218 ( SYNCHRO, RECEIVER-TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND DOUBLE FLANGE A
Cross Reference | NSN 5990-00-085-0829
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY3701-4C2 | 06840 | BENDIX CORP THE |
| 37TRX4A | 10112 | GENERAL DYNAMICS GLOBAL IMAGINGTECHNOLOGIES, INC. |
| 808112 | 06141 | L3 AVIATION PRODUCTS, INC. |
| 37TX4B | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 37TRX4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-70-01A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708-70-001 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MILS20708-70-37T | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| MIL-S-20708/70 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| AY3701-4C2 | 06845 | RAYTHEON COMPANYDBA RAYTHEON |
| AS20708/70 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| AJ10029-1 | 08480 | WILSON TROPHY CO |
Technical Data | NSN 5990-00-085-0829
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 37 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 1.9 AMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 20.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 3.00 MINIMUM AND 4.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 66.00 MINIMUM AND 70.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.783 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 1.000 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 | 0.900 INCH-OUNCES NOMINAL |
| BODY STYLE | STANDARD ROUND DOUBLE FLANGE A |
| SHOULDER DIAMETER | 3.3290 INCHES MINIMUM AND 3.3340 INCHES MAXIMUM |
| PILOT DIAMETER | 1.6250 INCHES NOMINAL |
| SECOND SHOULDER DIAMETER | 3.3740 INCHES MINIMUM AND 3.3750 INCHES MAXIMUM |
| SECOND SHOULDER LENGTH | 0.3750 INCHES NOMINAL |
| OVERALL LENGTH | 5.9200 INCHES NOMINAL |
| FLANGE DIAMETER | 3.6240 INCHES MINIMUM AND 3.6250 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.2500 INCHES NOMINAL |
| BODY DIAMETER | 3.3850 INCHES MINIMUM AND 3.3900 INCHES MAXIMUM |
| DISTANCE BETWEEN FLANGES | 1.3120 INCHES NOMINAL |
| PILOT LENGTH | 0.1600 INCHES NOMINAL |
| SHOULDER LENGTH | 0.6550 INCHES NOMINAL |
| AFT OF SECOND FLANGE DIAMETER | 3.3740 INCHES MINIMUM AND 3.3750 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 4.0300 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| 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 70 GOVERNMENT SPECIFICATION |