NSN 5990-00-503-2457
Part Details | TRANSMITTER SYNCHRO
5990-00-503-2457 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: A6201S19B, AY201S19B, AY201S19B, AY201S19B, 681280, CR15DS1A033, CRH15DS1A033, A6201S19B, 5990-00-503-2457, 00-503-2457, 5990005032457, 005032457
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-503-2457 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-503-2457
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| A6201S19B | 06840 | BENDIX CORP THE |
| AY201S19B | 06840 | BENDIX CORP THE |
| AY201S19B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S19B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 681280 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| CR15DS1A033 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CRH15DS1A033 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| A6201S19B | 06845 | RAYTHEON COMPANYDBA RAYTHEON |
Technical Data | NSN 5990-00-503-2457
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 125.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 500.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 6.70 NOMINAL |
| TRANSFORMATION RATIO | 0.450 ROTOR TO STATOR NOMINAL |
| TORQUE GRADIENT PER ANGULAR DEG | 2250.0 MILLIMETER-MILLIGRAMS MINIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1620 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 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 | 1.6220 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.0950 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8750 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 4 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM |
