NSN 5990-00-504-8809
Part Details | TRANSMITTER SYNCHRO
5990-00-504-8809 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: AY201S4, 99373102, 993731-02, 78567119, 785671-19, AY201S4B, AY2014B, AY201-4B, 78567119, 785671-19, 35631500314, 3563150-0314, AY201S4B, AY201S4, 15TX5048809, 15TX504-8809, 5990-00-504-8809, 00-504-8809, 5990005048809, 005048809
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-504-8809 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-504-8809
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY201S4 | 06840 | BENDIX CORP THE |
| 993731-02 | 35351 | GE AVIATION SYSTEMS LLC |
| 785671-19 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY201S4B | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY201-4B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 785671-19 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563150-0314 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S4B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S4 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 15TX504-8809 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
Technical Data | NSN 5990-00-504-8809
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 125.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 260.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.30 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 43.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 44.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 28.00 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 6.10 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 12.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 3.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 25.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 2.0 MILLIMETER-MILLIGRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2250.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| 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 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 | STEEL, CORROSION RESISTING |
| SPECIAL FEATURES | 18 INCH WIRE LEAD TERMINAL REQUIRED |
| FRAGILITY FACTOR | MODERATELY RUGGED |