NSN 5990-01-104-6703
Part Details | TRANSMITTER SYNCHRO
5990-01-104-6703 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: 8100017001, 810-0017-001, 8100017001, 810-0017-001, TRH11G4, TRH-11-G-4, 5990-01-104-6703, 01-104-6703, 5990011046703, 011046703
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | DEC 09, 1980 | 01-104-6703 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B

Cross Reference | NSN 5990-01-104-6703
Part Number | Cage Code | Manufacturer |
---|---|---|
810-0017-001 | 13044 | BFGOODRICH AEROSPACE COMPONENTOVERHAUL AND REPAIR INC |
810-0017-001 | 25583 | L3 AVIATION PRODUCTS, INC. |
TRH-11-G-4 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-104-6703
Characteristic | Specifications |
---|---|
BODY SIZE | 11 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 260.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 15.80 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 100.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 3.48 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 17.50 NOMINAL |
ZSS RESISTANCE IN OHMS | 21.00 NOMINAL |
PLUS J ZSS REACTANCE IN OHMS | 8.50 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 9.20 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 3.00 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 5.000 INPUT TO OUTPUT NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.5/P7.5 |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 1.0 CENTIMETER-GRAMS MAXIMUM |
BODY STYLE | STANDARD ROUND B |
SHOULDER DIAMETER | 1.0000 INCHES NOMINAL |
PILOT DIAMETER | 0.6250 INCHES NOMINAL |
OVERALL LENGTH | 2.0840 INCHES NOMINAL |
FLANGE DIAMETER | 1.0670 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0590 INCHES MINIMUM AND 0.0650 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0500 INCHES MINIMUM |
PILOT LENGTH | 0.0620 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.7020 INCHES NOMINAL |
TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
FRAGILITY FACTOR | MODERATELY RUGGED |