NSN 5990-00-503-3264
Part Details | TRANSMITTER SYNCHRO
5990-00-503-3264 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: 9706302, 970630-2, AY5034A1, AY503-4A1, 7331903, 733190-3, 129029920, 1290299-20, AY5034A1, AY503-4A1, 7331903, 733190-3, 5990-00-503-3264, 00-503-3264, 5990005033264, 005033264
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-503-3264 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-503-3264
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 970630-2 | 03848 | ARMA DIVAMBAC INDUSTRIES INC |
| AY503-4A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 733190-3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1290299-20 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| AY503-4A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 733190-3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-503-3264
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 220.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 2.5 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 36.20 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 109.50 NOMINAL |
| ZSO RESISTANCE IN OHMS | 9.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 24.20 NOMINAL |
| ZRS RESISTANCE IN OHMS | 62.30 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 25.20 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 8.70 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 7.85 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 25.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.50 NOMINAL |
| MAXIMUM TEMP RISE | 40.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2300.0 MILLIMETER-MILLIGRAMS NOMINAL |
| 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 | 1.6540 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8340 INCHES MINIMUM AND 0.8370 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 NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |