NSN 5990-00-539-7329
Part Details | TRANSMITTER SYNCHRO
5990-00-539-7329 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: AYA4011A, AYA401-1A, AY4011, AY401-1, AYA4011A, AYA401-1A, AY4011, AY401-1, AY4011A, AY401-1A, 5990-00-539-7329, 00-539-7329, 5990005397329, 005397329
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-539-7329 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-539-7329
Part Number | Cage Code | Manufacturer |
---|---|---|
AYA401-1A | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY401-1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AYA401-1A | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
AY401-1 | 19315 | HONEYWELL INTL INC DEFENSE AVIONICSSYSTEMS FORMER BENDIX NAVIGATION AND |
AY401-1A | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-539-7329
Characteristic | Specifications |
---|---|
BODY SIZE | 22 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 900.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 5.0 WATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 0.60 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 0.26 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 50.000 INPUT TO OUTPUT NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M10.0/P10.0 |
ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 45.0 CENTIMETER-GRAMS NOMINAL |
ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 15.0 CENTIMETER-GRAMS NOMINAL |
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 | 0.1230 INCHES MINIMUM AND 0.1270 INCHES MAXIMUM |
UNDERCUT DIAMETER | 1.9970 INCHES MINIMUM AND 2.0030 INCHES MAXIMUM |
UNDERCUT WIDTH | 0.1000 INCHES NOMINAL |
PILOT LENGTH | 0.0600 INCHES NOMINAL |
SHOULDER LENGTH | 0.1980 INCHES MINIMUM AND 0.2020 INCHES MAXIMUM |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 2.6120 INCHES NOMINAL |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ANY ACCEPTABLE |
FRAGILITY FACTOR | MODERATELY RUGGED |