NSN 5990-00-880-8225
Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-880-8225 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the rotor is dependent upon both the position of the rotor and the electrical input to the stator from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, or variable transformers.
Alternate Parts: 04052573017899, 13703003, 137030-03, CM41002022, CM41004022, CM41002022, CM41004022, HTC8DD4F974, HTC-8-DD-4/F974, CTH3DD4L158, CTH8DD4L158, CTH-8-DD-4/L158, 5990-00-880-8225, 00-880-8225, 5990008808225, 008808225
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-880-8225 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
1 Y-ROTOR, 1 STATOR
Cross Reference | NSN 5990-00-880-8225
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 04052573017899 | D1131 | AUTOFLUG GMBHDBA AUTOFLUG SICHERHEITSGERATE |
| 137030-03 | 35351 | GE AVIATION SYSTEMS LLC |
| CM41002022 | 09301 | KEARFOTT CORP SOMA FORWARDING DIV |
| CM41004022 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41002022 | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| CM41004022 | 05088 | KEARFOTT CORPORATIONDIV A SUBSIDIARY OF ASTRONAUTICS |
| HTC-8-DD-4/F974 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH3DD4L158 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-8-DD-4/L158 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-880-8225
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 40.0 MILLIAMPERES MAXIMUM |
| STATOR INPUT ELECTRICAL POWER RATING | 100.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 470.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 1770.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 81.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 330.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 590.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 190.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 365.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 64.00 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 8.500 INPUT TO OUTPUT NOMINAL |
| MAXIMUM TOTAL NULL VOLTAGE OUTPUT IN MILLIVOLTS PER VOLT | 40.00 |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.0210 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.7450 INCHES MINIMUM AND 0.7500 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| 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, CORROSION RESISTING |
| SCHEMATIC DIAGRAM DESIGNATOR | 1 Y-ROTOR, 1 STATOR |
| CUBIC MEASURE | 0.219 CUBIC INCHES |
