NSN 5990-00-269-2226
Part Details | TRANSMITTER SYNCHRO
5990-00-269-2226 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: 13764101, 137641-01, 1376401, 13764-01, 13764101, 137641-01, 13764101, 137641-01, 13764101, 137641-01, CGH8F1L302, 5990-00-269-2226, 00-269-2226, 5990002692226, 002692226
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-269-2226 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-269-2226
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 137641-01 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| 13764-01 | 06989 | API HAROWE INCDBA API MOTION DIV API |
| 137641-01 | 35351 | GE AVIATION SYSTEMS LLC |
| 137641-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 137641-01 | 1K426 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CGH8F1L302 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-269-2226
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 200.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.1 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 32.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 150.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.30 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 26.20 NOMINAL |
| ZRS RESISTANCE IN OHMS | 54.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 16.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 24.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.50 NOMINAL |
| TRANSFORMATION RATIO | 0.448 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 9.500 INPUT TO OUTPUT MAXIMUM |
| MAXIMUM TEMP RISE | 10.0 DEG CELSIUS |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 30.00 OUTPUT |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 60.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M7.0/P7.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.0 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.0 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.4640 INCHES MINIMUM AND 1.5040 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |