Part Details | RECEIVER SYNCHRO
5990-00-251-6719 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: AY110321B1, AY1103-21B1, 11TR1427, 148655727, 1486557-27, AY110321B1, AY1103-21B1, 148655727, 1486557-27, AY110321B1, AY1103-21B1, 11TR2516719, 11TR251-6719, AY110321B1, AY1103-21B1, 5990-00-251-6719, 00-251-6719, 5990002516719, 002516719
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUL 16, 1969 | 00-251-6719 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-251-6719
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY1103-21B1 | 0SML3 | AERO INTERNATIONAL INCORPORATED |
| 11TR1427 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 1486557-27 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY1103-21B1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1486557-27 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY1103-21B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 11TR251-6719 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
| AY1103-21B1 | 4K539 | POLYTECHNIC INDUSTRIES, INC. |
Technical Data | NSN 5990-00-251-6719
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 25.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 920.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 4800.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 14.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 43.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 1100.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 500.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 406.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 9.30 NOMINAL |
| TRANSFORMATION RATIO | 0.103 STATOR TO ROTOR NOMINAL |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M45.0/P45.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 6000.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| 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 | 1.8610 INCHES MINIMUM AND 1.8910 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6200 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0900 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
| FRAGILITY FACTOR | MODERATELY RUGGED |