Part Details | TRANSMITTER SYNCHRO
5990-00-810-3969 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: AY100AA47A1, AY503F42A1, AY100AA47A1, AY503F42A1, 5990-00-810-3969, 00-810-3969, 5990008103969, 008103969
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-810-3969 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-810-3969
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY100AA47A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY503F42A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY100AA47A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY503F42A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-810-3969
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 115.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 530.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 40.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 224.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 8.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 37.80 NOMINAL |
| ZRS RESISTANCE IN OHMS | 46.40 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 22.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 20.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 5.75 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.200 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 50.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2500.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6470 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0730 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6780 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |