Part Details | TRANSMITTER SYNCHRO
5990-00-226-5496 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: AY150CZ19A1, AY150CZ19A1, AY150CZ19A1, HGH15ZS4F183, HGH-15-ZS-4/F183, HGH15RCDS4F978, HGH-15-RCDS-4/F978, 5990-00-226-5496, 00-226-5496, 5990002265496, 002265496
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1961 | 00-226-5496 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-226-5496
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY150CZ19A1 | 99251 | CARLETON LIFE SUPPORT SYSTEMS INC.DBA COBHAM MISSION SYSTEM |
| AY150CZ19A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY150CZ19A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| HGH-15-ZS-4/F183 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| HGH-15-RCDS-4/F978 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-226-5496
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 120.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 0.65 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 49.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 248.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 12.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 42.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 55.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 30.00 NOMINAL |
| ZSO-90 RESISTANCE IN OHMS | 7.60 NOMINAL |
| PLUS J ZSO-90 REACTANCE IN OHMS | 13.50 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 21.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| TRANSFORMATION RATIO | 0.454 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.200 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 190.0 DEG CELSIUS |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M20.0/P20.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 4.5 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 1.5 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.9430 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0010 INCHES MINIMUM AND 0.0020 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |