NSN 5990-00-819-2272
Part Details | TRANSMITTER SYNCHRO
5990-00-819-2272 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: 8595314001, 8595314-001, 11CX1682, 8595314001, 8595314-001, 7901464001, 7901464-001, 8595314001, 8595314-001, AY110AC40A1, AY110AC40A1, 5990-00-819-2272, 00-819-2272, 5990008192272, 008192272
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-819-2272 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-819-2272
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8595314-001 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 11CX1682 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 8595314-001 | 99974 | DELCO ELECTRONICS CORPDELCO SYSTEMS OPNS |
| 7901464-001 | 99974 | DELCO ELECTRONICS CORPDELCO SYSTEMS OPNS |
| 8595314-001 | 24617 | GENERAL MOTORS CORP |
| AY110AC40A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110AC40A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-819-2272
| 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 |
| ZRO RESISTANCE IN OHMS | 14.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 122.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 4.40 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 21.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 22.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 12.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 8.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 4.00 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 NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.9950 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0820 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9620 INCHES MINIMUM AND 0.9670 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6200 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
