Part Details | TRANSMITTER SYNCHRO
5990-00-946-4544 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: AY110EH104A1, 35631100016, 3563110-0016, AY110EH104A1, 35631100016, 3563110-0016, 5990-00-946-4544, 00-946-4544, 5990009464544, 009464544
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAR 09, 1966 | 00-946-4544 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-946-4544
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY110EH104A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563110-0016 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110EH104A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 3563110-0016 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-946-4544
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 210.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 23.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 124.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.80 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 22.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 39.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 18.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 10.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 50.00 INPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
| PILOT DIAMETER | 0.6250 INCHES NOMINAL |
| OVERALL LENGTH | 2.1250 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0620 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6100 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |