NSN 5990-00-136-7127
Part Details | RECEIVER SYNCHRO
5990-00-136-7127 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 1497781, AY110DL121B1, 1497781, AY110DL121B1, 5990-00-136-7127, 00-136-7127, 5990001367127, 001367127
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 24, 1969 | 00-136-7127 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-136-7127
Part Number | Cage Code | Manufacturer |
---|---|---|
1497781 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY110DL121B1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
1497781 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
AY110DL121B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-136-7127
Characteristic | Specifications |
---|---|
BODY SIZE | 11 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 95.0 MILLIAMPERES MINIMUM AND 100.0 MILLIAMPERES MAXIMUM |
ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 44.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 43.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 11.70 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 40.50 NOMINAL |
ZRS RESISTANCE IN OHMS | 57.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 28.00 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 18.00 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 9.30 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 4.000 INPUT TO OUTPUT NOMINAL |
RECEIVER ERROR ANGULAR RANGE IN MINUTES | M45.0/P45.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 5000.00 MILLIMETER-MILLIGRAMS MAXIMUM |
TORQUE GRADIENT PER ANGULAR DEG | 2000.000 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 | 1.9380 INCHES NOMINAL |
FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0900 INCHES MINIMUM AND 0.0960 INCHES MAXIMUM |
UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
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 | 1.6820 INCHES MAXIMUM |
ALIGNMENT HOLE DEPTH | 0.0900 INCHES MINIMUM |
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 |