Part Details | TRANSMITTER SYNCHRO
5990-00-115-2374 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 08CX55570, 7602241, 35630800249, 3563080-0249, 35630800249, 3563080-0249, CM91014038, EGH8LL06L849, EGH-8-LL-06/L849, 5990-00-115-2374, 00-115-2374, 5990001152374, 001152374
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | OCT 19, 1972 | 00-115-2374 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-115-2374
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 08CX55570 | 25565 | BOWMAR CANADA LTD |
| 7602241 | 93322 | GE AVIATION SYSTEMS LLCDBA GE AVIATION |
| 3563080-0249 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563080-0249 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| CM91014038 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| EGH-8-LL-06/L849 | 21530 | SPENCER INDUSTRIES INC |
Technical Data | NSN 5990-00-115-2374
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 85.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 70.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 305.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 16.50 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 50.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 127.20 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 23.00 NOMINAL |
| ZSS RESISTANCE IN OHMS | 127.20 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 23.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 50.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 30.00 |
| 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 A |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.8390 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7500 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.4210 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 SCREW |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ANY ACCEPTABLE |
| FRAGILITY FACTOR | MODERATELY RUGGED |