NSN 5990-00-965-7085
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-965-7085 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 3162019, 1047291, 3162019, 1047291, AY110BA43A1, AY110BA43A1, 5990-00-965-7085, 00-965-7085, 5990009657085, 009657085
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-965-7085 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-965-7085
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3162019 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 1047291 | 77068 | ALLIED-SIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 3162019 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1047291 | 59364 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110BA43A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110BA43A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-965-7085
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 73.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 420.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 16.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 76.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 79.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 57.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 35.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 12.10 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT MINIMUM AND 6.200 INPUT TO OUTPUT MAXIMUM |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS 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 | 2.2410 INCHES MINIMUM AND 2.2440 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9700 INCHES MINIMUM AND 0.9800 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0450 INCHES MINIMUM AND 0.0550 INCHES MAXIMUM |
| 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 | 1.6820 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0125 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8190 INCHES MAXIMUM |
| SECURING HOLE QUANTITY | 4 |
| MOUNTING FACILITY SCREW THREAD SERIES DESIGNATOR | UNC |
| MOUNTING FACILITY NOMINAL SCREW THREAD DIAMETER | 0.112 INCHES |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
| FRAGILITY FACTOR | MODERATELY RUGGED |
