NSN 5990-00-446-0518
Part Details | DIFFERENTIAL RECEIVER SYNCHRO
5990-00-446-0518 A synchro, the rotor of which is free to turn, which will assume a position in accordance with the sum or difference of the electrical angular information received from two transmitter synchros. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: CDH8A1, 314990071708, 314-990071-708, AY083AA43A1, AY083AA-43-A1, CM01044107, CL40912002, CDC8A1, 42690102, 4269-01-02, CDH8A1, 2290262000, 229-0262-000, 229026200, 229-0262-00, 5990-00-446-0518, 00-446-0518, 5990004460518, 004460518
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-446-0518 | 02070 ( SYNCHRO, DIFFERENTIAL RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-446-0518
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CDH8A1 | 26197 | CHEMCON INC |
| 314-990071-708 | 90073 | CMC ELECTRONICS INC |
| AY083AA-43-A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CM01044107 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CL40912002 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CDC8A1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 4269-01-02 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CDH8A1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 229-0262-000 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
| 229-0262-00 | 13499 | ROCKWELL COLLINS, INC.DBA GOVERNMENT SYSTEMS |
Technical Data | NSN 5990-00-446-0518
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 96.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 210.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 38.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 122.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 28.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 114.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 47.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 13.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 36.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 125.0 DEG CELSIUS |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.5730 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6890 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 | 1.1790 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 6 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 | 0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |