NSN 5990-00-990-1711
Part Details | TRANSMITTER SYNCHRO
5990-00-990-1711 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: 11244004, 112440-04, 129029915, 1290299-15, AY50225A1, AY-502-25-A1, 129029915, 1290299-15, AY50225A1, AY-502-25-A1, 5990-00-990-1711, 00-990-1711, 5990009901711, 009901711
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-990-1711 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-990-1711
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 112440-04 | 35351 | GE AVIATION SYSTEMS LLC |
| 1290299-15 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY-502-25-A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 1290299-15 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY-502-25-A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-990-1711
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 35.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 300.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 225.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 695.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 265.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 111.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 11.000 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M1.0/P1.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8113 INCHES MINIMUM AND 0.8118 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.7790 INCHES NOMINAL |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8350 INCHES MINIMUM AND 0.8400 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0380 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0630 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0360 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.0320 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SPECIAL FEATURES | REAR SHAFT DIM. 0.2500 IN. NOM LG,0.0895 IN. MIN 0.0900 IN. MAX DIA,0.0200 IN. NOM W BY 0.0300 IN. NOM DEEP SLOT |
