NSN 5990-00-904-7315
Part Details | DIFFERENTIAL TRANSMITTER SYNCHRO
5990-00-904-7315 A synchro, the rotor of which is mechanically positioned for modifying electrical angular information, received from a transmitter synchro and transmitting to receiver synchro or control transformer synchro electrical information corresponding to the sum or difference of the electrical input angle and its rotor position angle. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: CDN10AS1, CDH10AS1B443, CDH10AS1/B443, 2325877, 2325877REVC, 5990-00-904-7315, 00-904-7315, 5990009047315, 009047315
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1960 | 00-904-7315 | 02071 ( SYNCHRO, DIFFERENTIAL TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND B
Cross Reference | NSN 5990-00-904-7315
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CDN10AS1 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| CDH10AS1/B443 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 2325877 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| 2325877REVC | 53711 | NAVAL SEA SYSTEMS COMMAND |
Technical Data | NSN 5990-00-904-7315
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 10 |
| STATOR INPUT VOLTAGE RATING IN VOLTS | 11.8 NOMINAL |
| STATOR INPUT CURRENT RATING | 100.0 MILLIAMPERES NOMINAL |
| STATOR INPUT ELECTRICAL POWER RATING | 250.0 MILLIWATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 28.90 MINIMUM AND 39.10 MAXIMUM |
| PLUS J ZRO REACTANCE IN OHMS | 107.10 MINIMUM AND 130.90 MAXIMUM |
| ROTOR DC RESISTANCE IN OHMS | 28.80 MINIMUM AND 35.20 MAXIMUM |
| STATOR DC RESISTANCE IN OHMS | 22.50 MINIMUM AND 27.50 MAXIMUM |
| TRANSFORMATION RATIO | 1.028 ROTOR TO STATOR MINIMUM AND 1.090 ROTOR TO STATOR MAXIMUM |
| PHASE SHIFT ANGLE IN DEG | 10.200 OUTPUT TO INPUT MAXIMUM |
| MAXIMUM FUNDAMENTAL NULL VOLTAGE IN MILLIVOLTS PER VOLT | 60.00 OUTPUT |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 9.00 CENTIMETER-GRAMS MAXIMUM |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 3.00 CENTIMETER-GRAMS MAXIMUM |
| BODY STYLE | STANDARD ROUND B |
| SHOULDER DIAMETER | 0.8118 INCHES MINIMUM AND 0.8123 INCHES MAXIMUM |
| PILOT DIAMETER | 0.5000 INCHES MINIMUM AND 0.5005 INCHES MAXIMUM |
| OVERALL LENGTH | 1.6650 INCHES MAXIMUM |
| FLANGE DIAMETER | 0.9360 INCHES MINIMUM AND 0.9370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0580 INCHES MINIMUM AND 0.0680 INCHES MAXIMUM |
| UNDERCUT WIDTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| PILOT LENGTH | 0.0350 INCHES MINIMUM AND 0.0450 INCHES MAXIMUM |
| SHOULDER LENGTH | 0.0570 INCHES MINIMUM AND 0.0670 INCHES MAXIMUM |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.1900 INCHES MAXIMUM |
| TERMINAL TYPE AND QUANTITY | 6 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, CORROSION RESISTING |
| TEST DATA DOCUMENT | 10001-2325877 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| SHAFT MAXIMUM RUNOUT | 0.0010 INCHES |
| FRAGILITY FACTOR | MODERATELY RUGGED |
