NSN 5990-00-818-3480
Part Details | RECEIVER SYNCHRO
5990-00-818-3480 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: 7910952, 7910952, AY60040A1, AY600-40A1, AY60040A1, AY600-40A1, R9257AM0D, R925-7AM0D, TRC11E2A024, 5990-00-818-3480, 00-818-3480, 5990008183480, 008183480
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1962 | 00-818-3480 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-818-3480
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7910952 | 99974 | DELCO ELECTRONICS CORPDELCO SYSTEMS OPNS |
| 7910952 | 24617 | GENERAL MOTORS CORP |
| AY600-40A1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY600-40A1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| R925-7AM0D | 88818 | KEARFOTT CORPORATIONDBA KEARFOTT |
| TRC11E2A024 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-818-3480
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 125.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 600.0 MILLIWATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 38.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 250.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 10.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 43.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 57.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 24.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 17.20 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 8.50 NOMINAL |
| TRANSFORMATION RATIO | 0.454 ROTOR TO STATOR NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.600 INPUT TO OUTPUT NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.9995 INCHES MINIMUM AND 1.0000 INCHES MAXIMUM |
| PILOT DIAMETER | 0.6245 INCHES MINIMUM AND 0.6250 INCHES MAXIMUM |
| OVERALL LENGTH | 2.0610 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0570 INCHES MINIMUM AND 1.0650 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.9750 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0500 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0620 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.6870 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0940 INCHES MAXIMUM |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
