NSN 5990-00-503-4120
Part Details | RECEIVER SYNCHRO
5990-00-503-4120 A synchro consisting of a stator and rotor inductively coupled. The rotor is free to turn in accordance with the electrical input from a transmitter synchro or a differential synchro. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: AY201S2E, AY201S2B, AY201S2E, AY201S2B, 58418, 45112682, 451-1268-2, 2G40097, 2G4009-7, 1819950, 739900001, 739-900-001, 50141, 58418, 15TR3B1594, 15TR3B-1594, 15SS1594, 5990-00-503-4120, 00-503-4120, 5990005034120, 005034120
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-503-4120 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-503-4120
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AY201S2E | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S2B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201S2E | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201S2B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 58418 | 1PQF4 | L3 TECHNOLOGIES, INC.DBA LINK SIMULATION & TRAINING |
| 451-1268-2 | 11530 | LOCKHEED MARTIN CORPORATIONDIV LOCKHEED MARTIN INFORMATION |
| 2G4009-7 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 1819950 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 739-900-001 | 15090 | RAYTHEON COMPANYDBA RAYTHEON |
| 50141 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
| 58418 | 36378 | RAYTHEON TECHNICAL SERVICES COMPANY |
| 15TR3B-1594 | 73693 | SCHULZE MFG. INC. |
| 15SS1594 | 73693 | SCHULZE MFG. INC. |
Technical Data | NSN 5990-00-503-4120
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 450.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 45.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 255.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 7.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 39.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 36.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 23.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 16.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 7.00 NOMINAL |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M45.0/P45.0 |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1310 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 | 1.5910 INCHES NOMINAL |
| ALIGNMENT HOLE DEPTH | 0.1250 INCHES NOMINAL |
| 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 ALLOY |
| FRAGILITY FACTOR | MODERATELY RUGGED |