NSN 5990-00-681-2726
Part Details | TRANSMITTER SYNCHRO
5990-00-681-2726 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: AY201S26B, AY201S26B, 5990-00-681-2726, 00-681-2726, 5990006812726, 006812726
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
59 | JAN 01, 1963 | 00-681-2726 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-681-2726
Part Number | Cage Code | Manufacturer |
---|---|---|
AY201S26B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
AY201S26B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-681-2726
Characteristic | Specifications |
---|---|
BODY SIZE | 15 |
ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
ROTOR INPUT CURRENT RATING | 125.0 MILLIAMPERES NOMINAL |
ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS NOMINAL |
FREQUENCY IN HERTZ | 400.0 NOMINAL |
ZRO RESISTANCE IN OHMS | 33.00 NOMINAL |
PLUS J ZRO REACTANCE IN OHMS | 224.00 NOMINAL |
ZSO RESISTANCE IN OHMS | 9.40 NOMINAL |
PLUS J ZSO REACTANCE IN OHMS | 39.00 NOMINAL |
ZRS RESISTANCE IN OHMS | 36.00 NOMINAL |
PLUS J ZRS REACTANCE IN OHMS | 22.50 NOMINAL |
ROTOR DC RESISTANCE IN OHMS | 12.60 NOMINAL |
STATOR DC RESISTANCE IN OHMS | 5.80 NOMINAL |
PHASE SHIFT ANGLE IN DEG | 2.700 INPUT TO OUTPUT NOMINAL |
ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M12.0/P12.0 |
BODY STYLE | STANDARD ROUND C |
SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
OVERALL LENGTH | 1.1310 INCHES NOMINAL |
FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
PILOT LENGTH | 0.0400 INCHES NOMINAL |
SHOULDER LENGTH | 0.1320 INCHES NOMINAL |
MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
ALIGNMENT HOLE DEPTH | 0.1250 INCHES MAXIMUM |
ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
ALIGNMENT HOLE QUANTITY | 4 |
TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
TERMINAL LOCATION | REAR |
BODY MATERIAL | ALUMINUM |