NSN 5990-00-326-2172
Part Details | TRANSMITTER SYNCHRO
5990-00-326-2172 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: 35631100175, 3563110-0175, 22771810001, 2277181-0001, 35631100175, 3563110-0175, 22771810001, 2277181-0001, 5990-00-326-2172, 00-326-2172, 5990003262172, 003262172
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | NOV 28, 1973 | 00-326-2172 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-326-2172
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3563110-0175 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 2277181-0001 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 3563110-0175 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 2277181-0001 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
Technical Data | NSN 5990-00-326-2172
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 280.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.0 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 16.20 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 105.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 3.60 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 17.60 NOMINAL |
| ZRS RESISTANCE IN OHMS | 22.50 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 7.28 NOMINAL |
| ZSS RESISTANCE IN OHMS | 3.90 NOMINAL |
| PLUS J ZSS REACTANCE IN OHMS | 1.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 9.10 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.00 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.400 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 0.5 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.3 CENTIMETER-GRAMS MAXIMUM |
| TORQUE GRADIENT PER ANGULAR DEG | 5760.0 MILLIMETER-MILLIGRAMS MINIMUM |
| 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 | 2.3080 INCHES MINIMUM AND 2.3320 INCHES MAXIMUM |
| 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 | 1.8810 INCHES MINIMUM AND 1.8850 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8150 INCHES MAXIMUM |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |