NSN 5990-00-578-6254
Part Details | TRANSMITTER SYNCHRO
5990-00-578-6254 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: G15P5033, 11TX0894L, 11TX-0894-L, AY600B6A1, AY110FA40A1, AY6000, AY-600-0, AY600B6A1, AY110FA40A1, AY6000, AY-600-0, 1591025, 159-1025, G15P5033, 5990-00-578-6254, 00-578-6254, 5990005786254, 005786254
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-578-6254 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-578-6254
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| G15P5033 | 94033 | CARDWELL CONDENSER CORPLAPOINTE-ADMIRAL DIV |
| 11TX-0894-L | 51761 | CDA INTERCORP LLC |
| AY600B6A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110FA40A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY-600-0 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY600B6A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY110FA40A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY-600-0 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 159-1025 | 71313 | VIKING TECHNOLOGIES, LTD. |
| G15P5033 | 71313 | VIKING TECHNOLOGIES, LTD. |
Technical Data | NSN 5990-00-578-6254
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 250.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.4 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.60 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 26.00 |
| 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 | 4200.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 1.9950 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 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 | 1.6200 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0900 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 1.0250 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |