NSN 5990-00-924-4164
Part Details | TRANSMITTER SYNCHRO
5990-00-924-4164 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: 8190W10P001, 11CX4C, 26V11CX4C, 26V11CX4B, 1599017210L, 615558000, 615558-000, MILS207088, MIL-S-20708/8, 26V11CX4A, 26V11CX4, 26V-11CX4, M20708801C, M20708/8-01C, M20708201E, M20708/2-01E, M2070811201C, M20708/112-01C, 26V11CX4B, 45090092433, 450900-9243-3, 4509009243003, 450900-9243-003, AS207088, AS20708/8, AS207088, AS20708/8, AS207088, AS20708/8, M20708801C, M20708/8-01C, 5990-00-924-4164, 00-924-4164, 5990009244164, 009244164
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 20, 1966 | 00-924-4164 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-924-4164
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8190W10P001 | 97424 | AMETEK INC.DBA AMETEK AEROSPACE & DEFENSE |
| 11CX4C | 25565 | BOWMAR CANADA LTD |
| 26V11CX4C | 09301 | KEARFOTT CORP SOMA FORWARDING DIV |
| 26V11CX4B | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| 1599017210L | A0810 | LEONARDO S.P.A. - AIRBORNE & SPACESYSTEM DIVISION |
| 615558-000 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| MIL-S-20708/8 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V11CX4A | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V-11CX4 | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/8-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/2-01E | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| M20708/112-01C | 81349 | MILITARY SPECIFICATIONSPROMULGATED BY MILITARY |
| 26V11CX4B | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 450900-9243-3 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| 450900-9243-003 | D4856 | NORTHROP GRUMMAN LITEF GMBHDBA LITEF |
| AS20708/8 | 0VH01 | SAE CUSTOMER SERVICEDEPT 2045 |
| AS20708/8 | 05AY8 | SAE INC |
| AS20708/8 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| M20708/8-01C | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 5990-00-924-4164
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 130.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 340.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO IMPEDANCE MAGNITUDE IN OHMS | 200.00 MINIMUM AND 300.00 MAXIMUM |
| ZRO IMPEDANCE ANGLE IN DEG | 80.50 MINIMUM AND 84.00 MAXIMUM |
| ZSS IMPEDANCE MAGNITUDE IN OHMS | 6.00 MINIMUM AND 12.00 MAXIMUM |
| ZSS IMPEDANCE ANGLE IN DEG | 18.00 MINIMUM AND 30.00 MAXIMUM |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 12.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 19.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| TORQUE GRADIENT PER ANGULAR DEG | 0.070 INCH-OUNCES MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.3560 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.3560 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| 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 8 GOVERNMENT SPECIFICATION |
| FRAGILITY FACTOR | MODERATELY RUGGED |
