NSN 5990-00-776-4115
Part Details | RECEIVER SYNCHRO
5990-00-776-4115 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: 101201, 10120-1, 08TR0156B, L9140008, 1782615004, 1782615-004, 425701, 4257-01, CRH8A1L410, CRH8A1/L410, CRH8AL410, CRH8A1, CRH-8-A-1, 353003, 35-3003, 5990-00-776-4115, 00-776-4115, 5990007764115, 007764115
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-776-4115 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND A
Cross Reference | NSN 5990-00-776-4115
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10120-1 | 10138 | ASTRONAUTICS CORPORATION OF AMERICA |
| 08TR0156B | 51761 | CDA INTERCORP LLC |
| L9140008 | D2439 | DIEHL AEROSPACE GMBH,STANDORTFRANKFURT |
| 1782615-004 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| 4257-01 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CRH8A1/L410 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CRH8AL410 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| CRH-8-A-1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 35-3003 | F0296 | THALES AVIONICS ELECTRICALSYSTEMSSAS |
Technical Data | NSN 5990-00-776-4115
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 8 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 540.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 54.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 260.00 NOMINAL |
| ZSO RESISTANCE IN OHMS | 12.00 NOMINAL |
| PLUS J ZSO REACTANCE IN OHMS | 45.00 NOMINAL |
| ZRS RESISTANCE IN OHMS | 88.00 NOMINAL |
| PLUS J ZRS REACTANCE IN OHMS | 22.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 37.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 12.00 NOMINAL |
| RECEIVER ERROR ANGULAR RANGE IN MINUTES | M30.0/P30.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 16.0 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 4.0 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND A |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6160 INCHES NOMINAL |
| FLANGE DIAMETER | 0.7490 INCHES MINIMUM AND 0.7620 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.6880 INCHES MINIMUM AND 0.6910 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0430 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| SHAFT MAXIMUM RADIAL PLAY | 0.0010 INCHES |
| SHAFT RADIAL PLAY DETERMINING WEIGHT | 4.0 OUNCES |
| SHAFT END PLAY | 0.0020 INCHES MINIMUM AND 0.0050 INCHES MAXIMUM |
| SHAFT END PLAY DETERMINING WEIGHT | 8.0 OUNCES |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
