NSN 5990-00-631-9480
Part Details | TRANSMITTER SYNCHRO
5990-00-631-9480 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: AY50326A2, AY503-26A2, AY50326A2, AY503-26A2, 5990-00-631-9480, 00-631-9480, 5990006319480, 006319480
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-631-9480 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-631-9480
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY503-26A2 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY503-26A2 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-631-9480
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 185.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.7 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 35.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 145.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.30 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 31.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 66.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 27.50 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 9.10 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 10.70 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 26.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.90 NOMINAL |
| MAXIMUM TEMP RISE | 40.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M2.0/P2.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2250.0 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 | 0.8350 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 | 1.2030 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0630 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 |
| FRAGILITY FACTOR | MODERATELY RUGGED |