NSN 5990-00-436-2224
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 |