NSN 5990-00-583-3724
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-583-3724 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: 10491801, 104918-01, 78567121, 785671-21, AY201S5B, AY201S5B, 78567121, 785671-21, 78567121, 785671-21, AY201S5B, AU9002, AY201S5B, CT15D4, 2109900002, 5990-00-583-3724, 00-583-3724, 5990005833724, 005833724
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-583-3724 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-583-3724
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 104918-01 | 35351 | GE AVIATION SYSTEMS LLC |
| 785671-21 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S5B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S5B | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 785671-21 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
| 785671-21 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S5B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AU9002 | 0NKU0 | LCT ELECTRONICS |
| AY201S5B | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| CT15D4 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 2109900002 | 57057 | NAVCOM DEFENSE ELECTRONICS, INC. |
Technical Data | NSN 5990-00-583-3724
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 25.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 70.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 125.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 480.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 250.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 63.00 NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5310 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |