NSN 5990-01-310-5421
Part Details | TRANSMITTER SYNCHRO
5990-01-310-5421 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: 51601131, 5160113-1, TGH11H7, TGH-11-H-7, TGH11H7, TGH-11-H-7, 5990-01-310-5421, 01-310-5421, 5990013105421, 013105421
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 07, 1989 | 01-310-5421 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-01-310-5421
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5160113-1 | 55973 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| TGH-11-H-7 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TGH-11-H-7 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-310-5421
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 54.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 900.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 392.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 2430.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 11.30 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 50.30 NOMINAL |
| ZRS RESISTANCE IN OHMS | 556.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 210.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 230.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 9.70 NOMINAL |
| TRANSFORMATION RATIO | 0.158 STATOR TO ROTOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 5.300 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 4400.0 MILLIMETER-MILLIGRAMS 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 | 2.1150 INCHES MAXIMUM |
| FLANGE DIAMETER | 1.0610 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0880 INCHES MINIMUM AND 0.0980 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 | 1.6000 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| TEST DATA DOCUMENT | 55973-5160113 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| SHAFT MAXIMUM RADIAL PLAY | 0.0005 INCHES |
| SHAFT RADIAL PLAY TEST POINT | 0.125 INCHES NOMINAL |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0008 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
