NSN 5990-00-781-6762
Part Details | RECEIVER SYNCHRO
5990-00-781-6762 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: 10218002, 10218-002, AY110CA49C1, AY110CA49C1, AY110CA49B1, TRH11CS4A933, TRH-11-CS-4/A933, TRH11CS4A933, TRH-11-CS-4/A933, 5990-00-781-6762, 00-781-6762, 5990007816762, 007816762
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-781-6762 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-781-6762
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10218-002 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| AY110CA49C1 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY110CA49C1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY110CA49B1 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| TRH-11-CS-4/A933 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| TRH-11-CS-4/A933 | 4H618 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-00-781-6762
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 11 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 265.0 MILLIAMPERES MAXIMUM |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.2 WATTS MAXIMUM |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 19.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 102.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 4.50 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 18.70 NOMINAL |
| ZRS RESISTANCE IN OHMS | 21.70 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 11.20 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 | 1.9370 INCHES NOMINAL |
| FLANGE DIAMETER | 1.0590 INCHES MINIMUM AND 1.0620 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 | 1.6250 INCHES MAXIMUM |
| ALIGNMENT HOLE DEPTH | 0.0500 INCHES NOMINAL |
| ALIGNMENT HOLE BOLT CIRCLE DIAMETER | 0.8120 INCHES NOMINAL |
| ALIGNMENT HOLE QUANTITY | 3 |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| FRAGILITY FACTOR | MODERATELY RUGGED |
