NSN 5990-00-676-9520
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-676-9520 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: AY60011A1, AY600-11-A1, 12124393, 1212439-3, AY60011A1, AY600-11-A1, 12124393, 1212439-3, 5345101, 534510-1, 5990-00-676-9520, 00-676-9520, 5990006769520, 006769520
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-676-9520 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-676-9520
Part Number | Cage Code | Manufacturer |
---|---|---|
AY600-11-A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
1212439-3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY600-11-A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
1212439-3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
534510-1 | 22525 | INSTRUMENTS AND FLIGHT RESEARCH INC. |
Technical Data | NSN 5990-00-676-9520
Characteristic | Specifications |
---|---|
BODY SIZE | 11 |
STATOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES MAXIMUM |
STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS MAXIMUM |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 126.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 707.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 27.00 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 130.00 NOMINAL |
ZSS RESISTANCE IN OHMS | 147.00 NOMINAL |
PLUS J ZSS REACTANCE IN OHMS | 103.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 71.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 21.00 NOMINAL |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 3.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 9.0 CENTIMETER-GRAMS 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 | 1.9590 INCHES MINIMUM AND 2.0240 INCHES MAXIMUM |
FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
UNDERCUT DIAMETER | 0.9450 INCHES MINIMUM AND 1.0050 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.0470 INCHES MINIMUM AND 0.0530 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 | 1.6520 INCHES MINIMUM AND 1.7120 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.0637 INCHES MINIMUM AND 0.1237 INCHES MAXIMUM |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8090 INCHES MINIMUM AND 0.8150 INCHES MAXIMUM |
ALIGNMENT HOLE QUANTITY | 4 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, CORROSION RESISTING |
SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
SHAFT RADIAL PLAY DETERMINING WEIGHT | 75.0 GRAMS |
SHAFT END PLAY | 0.0002 INCHES MINIMUM AND 0.0013 INCHES MAXIMUM |
SHAFT END PLAY DETERMINING WEIGHT | 3.0 OUNCES |