NSN 5990-00-504-6032
Part Details | TRANSMITTER SYNCHRO
5990-00-504-6032 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: 1047293, 35631500304, 3563150-0304, D78567112, D785671-12, AY201S1B1, AY201S1B, AY201S1B, AY201S1, AY201S1B, AY201S-1B, 706560, 35631500304, 3563150-0304, D78567112, D785671-12, AY201S1B1, AY201S1B, AY201S1B, 7411380P2, AY201S1B, AY201S-1-B, 402202, 4022-02, 15TX5046032, 15TX504-6032, 9868041, 986804-1, 9868041, 986804-1, 5990-00-504-6032, 00-504-6032, 5990005046032, 005046032
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-504-6032 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-504-6032
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1047293 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 3563150-0304 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| D785671-12 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S1B1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S1B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S1B | 02987 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS |
| AY201S1 | 02987 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX FLIGHT SYSTEMS |
| AY201S-1B | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 706560 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 3563150-0304 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| D785671-12 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S1B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S1B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S1B | 7Y670 | INSTRUMENT SUPPORT INC |
| 7411380P2 | 94271 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| AY201S-1-B | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 4022-02 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 15TX504-6032 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| 986804-1 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 986804-1 | 4K539 | POLYTECHNIC INDUSTRIES, INC. |
Technical Data | NSN 5990-00-504-6032
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 250.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.1 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 9.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 134.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 5.10 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 22.10 NOMINAL |
| ZRS RESISTANCE IN OHMS | 2.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 13.00 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 30.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M1.0/P1.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 30.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 10.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 3000.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |
