NSN 5990-00-583-9920
Part Details | TRANSMITTER SYNCHRO
5990-00-583-9920 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: AY4022A1, AY402-2A1, AY4022A1, AY402-2A1, 5990-00-583-9920, 00-583-9920, 5990005839920, 005839920
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-583-9920 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-583-9920
Part Number | Cage Code | Manufacturer |
---|---|---|
AY402-2A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY402-2A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-583-9920
Characteristic | Specifications |
---|---|
BODY SIZE | 22 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 1.0 AMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 4.0 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M1.0/P1.0 |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 1.9990 INCHES MINIMUM AND 1.9995 INCHES MAXIMUM |
PILOT DIAMETER | 0.7495 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
OVERALL LENGTH | 3.1720 INCHES NOMINAL |
FLANGE DIAMETER | 2.1600 INCHES MINIMUM AND 2.1610 INCHES MAXIMUM |
FLANGE THICKNESS | 0.1250 INCHES NOMINAL |
UNDERCUT DIAMETER | 2.0000 INCHES NOMINAL |
UNDERCUT WIDTH | 0.1000 INCHES NOMINAL |
PILOT LENGTH | 0.0600 INCHES NOMINAL |
SHOULDER LENGTH | 0.2000 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.6120 INCHES NOMINAL |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | STEEL, STAINLESS |