NSN 5990-00-615-5413
Part Details | TRANSMITTER SYNCHRO
5990-00-615-5413 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: AY110JA55A1, 12682213, 1268221-3, AY60530A1, AY605-30A1, AY110JA55A1, 12682213, 1268221-3, AY60530A1, AY605-30A1, 5990-00-615-5413, 00-615-5413, 5990006155413, 006155413
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-615-5413 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-615-5413
Part Number | Cage Code | Manufacturer |
---|---|---|
AY110JA55A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
1268221-3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY605-30A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY110JA55A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
1268221-3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
AY605-30A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-615-5413
Characteristic | Specifications |
---|---|
BODY SIZE | 11 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 115.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 5.5 AMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 1.6 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
TRANSFORMATION RATIO | 0.158 ROTOR TO STATOR NOMINAL |
TORQUE GRADIENT PER ANGULAR DEG | 2.2 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 | 2.2440 INCHES NOMINAL |
FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
PILOT LENGTH | 0.0620 INCHES NOMINAL |
SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6820 INCHES MAXIMUM |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ALUMINUM |
FRAGILITY FACTOR | MODERATELY RUGGED |