NSN 5990-00-686-4499
Part Details | RECEIVER SYNCHRO
5990-00-686-4499 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: 08TR1364, 8TR300G1A, AY080AA50A1, AY080AA-50-A1, CRC8A9, CRH8A9, 55689, 173460902, 173460-902, 173460, 5990-00-686-4499, 00-686-4499, 5990006864499, 006864499
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-686-4499 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-686-4499
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 08TR1364 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 8TR300G1A | 06989 | API HAROWE INCDBA API MOTION DIV API |
| AY080AA-50-A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CRC8A9 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CRH8A9 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 55689 | 34830 | ROGERSON KRATOS |
| 173460-902 | 65092 | SOLARTRON ELECTRONICS INCWESTON INSTRUMENTS DIV |
| 173460 | 65092 | SOLARTRON ELECTRONICS INCWESTON INSTRUMENTS DIV |
Technical Data | NSN 5990-00-686-4499
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 29.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 950.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 3850.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 36.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 550.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 420.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 700.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.40 NOMINAL |
| TRANSFORMATION RATIO | 9.745 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5400.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 2700.0 MILLIMETER-MILLIGRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 2400.0 MILLIMETER-MILLIGRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0020 INCHES MINIMUM AND 0.0040 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |