NSN 5990-01-091-3567
Part Details | TRANSMITTER SYNCHRO
5990-01-091-3567 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: 13764104, 137641-04, 5990-01-091-3567, 01-091-3567, 5990010913567, 010913567
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | MAR 06, 1980 | 01-091-3567 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A

Cross Reference | NSN 5990-01-091-3567
Part Number | Cage Code | Manufacturer |
---|---|---|
137641-04 | 35351 | GE AVIATION SYSTEMS LLC |
Technical Data | NSN 5990-01-091-3567
Characteristic | Specifications |
---|---|
BODY SIZE | 8 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 200.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 1.12 WATTS MAXIMUM |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 27.20 MINIMUM AND 36.80 MAXIMUM |
PLUS J ZRO REACTANCE IN OHMS | 127.50 MINIMUM AND 172.50 MAXIMUM |
ZSO RESISTANCE IN OHMS | 6.21 MINIMUM AND 8.39 MAXIMUM |
PLUS J ZSO REACTANCE IN OHMS | 22.27 MINIMUM AND 30.13 MAXIMUM |
ZRS RESISTANCE IN OHMS | 43.74 MINIMUM AND 64.26 MAXIMUM |
PLUS J ZRS REACTANCE IN OHMS | 12.32 MINIMUM AND 19.68 MAXIMUM |
ROTOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
TRANSFORMATION RATIO | 0.448 ROTOR TO STATOR NOMINAL |
PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT NOMINAL |
MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 75.00 |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
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 | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.8970 INCHES MAXIMUM |
FLANGE DIAMETER | 0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0570 INCHES NOMINAL |
PILOT LENGTH | 0.0430 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES NOMINAL |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |
SHAFT MAXIMUM RADIAL PLAY | 0.0008 INCHES |
SHAFT RADIAL PLAY TEST POINT | 0.250 INCHES NOMINAL |
SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
SHAFT END PLAY | 0.0003 INCHES MINIMUM AND 0.0015 INCHES MAXIMUM |
SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
FRAGILITY FACTOR | MODERATELY RUGGED |