NSN 5990-00-828-1771
Part Details | RECEIVER SYNCHRO
5990-00-828-1771 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: 35631003031, 3563100-3031, 14970230000, 1497023-0000, AY100TA50A1, 14970230000, 1497023-0000, 1497023, AY100TA50A1, 10TR8281771, 10TR828-1771, 5990-00-828-1771, 00-828-1771, 5990008281771, 008281771
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | AUG 30, 1967 | 00-828-1771 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-828-1771
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563100-3031 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1497023-0000 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY100TA50A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1497023-0000 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 1497023 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY100TA50A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 10TR828-1771 | 2X130 | MOTION DEVICES TECHNOLOGY, INC. |
Technical Data | NSN 5990-00-828-1771
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 45.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 950.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 591.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 3510.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 6.54 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 29.70 NOMINAL |
| ZRS RESISTANCE IN OHMS | 707.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 278.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 309.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 4.66 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.700 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 10000.0 MILLIMETER-MILLIGRAMS NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 3200.0 MILLIMETER-MILLIGRAMS MINIMUM |
| 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 | 1.6210 INCHES MAXIMUM |
| 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 | 1.2410 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0730 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 ALLOY |
