NSN 5990-01-042-7317
Part Details | RECEIVER SYNCHRO
5990-01-042-7317 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: 10TR1378, BB1436A, BB-1436-A, 10TR354A8A, 10TR-354-A-8A, AB1162A, AB-1162-A, ZE9A, ZE9-A, URH10J1B600, URH10JS1B600, URH-10-JS-1/B600, 5990-01-042-7317, 01-042-7317, 5990010427317, 010427317
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JUN 14, 1977 | 01-042-7317 | 02072 ( SYNCHRO, RECEIVER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-01-042-7317
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10TR1378 | 14404 | AMETEK TECHNICAL & INDUSTRIALPRODUCTS, INC. |
| BB-1436-A | 61349 | AMETEK, INC.DIV AEROSPACE & DEFENSE |
| 10TR-354-A-8A | 06989 | API HAROWE INCDBA API MOTION DIV API |
| AB-1162-A | 65003 | BERRY, JOHNDBA BERRY MANUFACTURING |
| ZE9-A | 51761 | CDA INTERCORP LLC |
| URH10J1B600 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| URH-10-JS-1/B600 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
Technical Data | NSN 5990-01-042-7317
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 90.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 43.0 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 33.00 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 11.60 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 7.800 INPUT TO OUTPUT NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 0.3 MILLIMETER-MILLIGRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 0.8123 INCHES NOMINAL |
| PILOT DIAMETER | 0.5000 INCHES NOMINAL |
| OVERALL LENGTH | 1.8340 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9330 INCHES NOMINAL |
| FLANGE THICKNESS | 0.0620 INCHES NOMINAL |
| UNDERCUT DIAMETER | 0.8123 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0620 INCHES NOMINAL |
| PILOT LENGTH | 0.0620 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0380 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.2410 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | ALUMINUM ALLOY |
| FRAGILITY FACTOR | MODERATELY RUGGED |
