NSN 5990-01-160-5967
Part Details | TRANSMITTER SYNCHRO
5990-01-160-5967 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: ST12AY1, ST-12AY-1, L478C2007, TT100086, 5990-01-160-5967, 01-160-5967, 5990011605967, 011605967
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | FEB 26, 2007 | 01-160-5967 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-01-160-5967
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| ST-12AY-1 | 1U5F4 | ARCHER TECHNOLOGIES INTERNATIONAL,INCORPORATED |
| L478C2007 | 43999 | BOEING COMPANY, THEDBA BOEING |
| TT100086 | 1FSK7 | TECHTROL, INC. |
Technical Data | NSN 5990-01-160-5967
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 300.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.1 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 16.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 107.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 3.70 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 18.10 NOMINAL |
| ZRS RESISTANCE IN OHMS | 22.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 8.90 NOMINAL |
| ZSS RESISTANCE IN OHMS | 4.10 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 1.40 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TEMP RISE | 20.0 DEG CELSIUS |
| TORQUE GRADIENT PER ANGULAR DEG | 0.008 INCH-OUNCES MINIMUM |
| 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 | 2.8250 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0500 INCHES MINIMUM AND 1.0510 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
| UNDERCUT DIAMETER | 0.9290 INCHES MINIMUM AND 0.9410 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0970 INCHES MINIMUM AND 0.1030 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 | 2.2500 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES MINIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 1 CONNECTOR, PLUG |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT END PLAY | 0.0010 INCHES NOMINAL |
