Part Details | CONTROL TRANSFORMER SYNCHRO
5990-00-436-2224 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: 15CT0114E, 15CT-0114E, 15CTQ114E, 15CT-Q114E, 6624263, 662426-3, 6624263, 662426-3, AY169B3, AY169B3, 40032903, 4003-29-03, CTH15DS2F871, CTH-15-DS-2/F871, 5990-00-436-2224, 00-436-2224, 5990004362224, 004362224
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | MAY 20, 1974 | 00-436-2224 | 15289 ( SYNCHRO, CONTROL TRANSFORMER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-436-2224
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 15CT-0114E | 51761 | CDA INTERCORP LLC |
| 15CT-Q114E | 51761 | CDA INTERCORP LLC |
| 662426-3 | 70040 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| 662426-3 | 7X677 | GENERAL MOTORS LLCDBA GENERAL MOTORS |
| AY169B3 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY169B3 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 4003-29-03 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CTH-15-DS-2/F871 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-436-2224
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 130.0 MILLIAMPERES NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 42.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 10.80 NOMINAL |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 1.3120 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 2.1300 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4370 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0930 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 | 1.6310 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.6750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |