NSN 5990-00-538-7330
Part Details | TRANSMITTER SYNCHRO
5990-00-538-7330 A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials.
Alternate Parts: 8526, 85-26, G15P5010, 7856719, 785671-9, AY201A1B, 7856719, 785671-9, AY201A1B, AY2011B, AY201-1B, 45112683, 451-1268-3, CGH15DS1, CGH-15-DS-1, 144A21800212, 144A21800-212, 144A21800212, 144A21800-212, 5990-00-538-7330, 00-538-7330, 5990005387330, 005387330
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 59 | JAN 01, 1963 | 00-538-7330 | 02073 ( SYNCHRO, TRANSMITTER ) |
REFERENCE DRAWINGS & PICTURES
STANDARD ROUND C
Cross Reference | NSN 5990-00-538-7330
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 85-26 | 81413 | BAE SYSTEMS INFORMATION ANDELECTRONIC SYSTEMS INTEGRATION I |
| G15P5010 | 94033 | CARDWELL CONDENSER CORPLAPOINTE-ADMIRAL DIV |
| 785671-9 | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| AY201A1B | 96774 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 785671-9 | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201A1B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| AY201-1B | 55972 | HONEYWELL INTL INCDEFENSE AVIONICS SYSTEMS |
| 451-1268-3 | 11530 | LOCKHEED MARTIN CORPORATIONDIV LOCKHEED MARTIN INFORMATION |
| CGH-15-DS-1 | 99932 | MOOG INC.DBA MOOG COMPONENTS GROUP |
| 144A21800-212 | 15280 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV ES DEFENSIVE SYSTEMS DIVISION |
| 144A21800-212 | 26916 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MULTIPLE |
Technical Data | NSN 5990-00-538-7330
| Characteristic | Specifications |
|---|---|
| BODY SIZE | 15 |
| ROTOR INPUT VOLTAGE RATING IN VOLTS | 26.0 NOMINAL |
| ROTOR INPUT CURRENT RATING | 225.0 MILLIAMPERES NOMINAL |
| ROTOR INPUT ELECTRICAL POWER RATING | 1.3 WATTS NOMINAL |
| FREQUENCY IN HERTZ | 400.0 NOMINAL |
| ZRO RESISTANCE IN OHMS | 25.00 NOMINAL |
| PLUS J ZRO REACTANCE IN OHMS | 115.00 NOMINAL |
| ROTOR DC RESISTANCE IN OHMS | 9.50 NOMINAL |
| STATOR DC RESISTANCE IN OHMS | 3.50 NOMINAL |
| PHASE SHIFT ANGLE IN DEG | 4.500 INPUT TO OUTPUT NOMINAL |
| ELECTRICAL ERROR ANGULAR RANGE IN MINUTES | M15.0/P15.0 |
| ACTUATOR FRICTION TORQUE AT MINUS 55 DEG CELSIUS | 15.00 CENTIMETER-GRAMS NOMINAL |
| ACTUATOR FRICTION TORQUE AT PLUS 25 DEG CELSIUS | 5.00 CENTIMETER-GRAMS NOMINAL |
| BODY STYLE | STANDARD ROUND C |
| SHOULDER DIAMETER | 1.3115 INCHES MINIMUM AND 1.3120 INCHES MAXIMUM |
| PILOT DIAMETER | 0.4995 INCHES MINIMUM AND 0.5000 INCHES MAXIMUM |
| OVERALL LENGTH | 2.1310 INCHES NOMINAL |
| FLANGE DIAMETER | 1.4360 INCHES MINIMUM AND 1.4370 INCHES MAXIMUM |
| FLANGE THICKNESS | 0.0930 INCHES NOMINAL |
| UNDERCUT DIAMETER | 1.3120 INCHES NOMINAL |
| UNDERCUT WIDTH | 0.0780 INCHES NOMINAL |
| PILOT LENGTH | 0.0400 INCHES NOMINAL |
| SHOULDER LENGTH | 0.0920 INCHES NOMINAL |
| MOUNTING SURFACE TO TERMINAL END DISTANCE | 1.5910 INCHES NOMINAL |
| TERMINAL TYPE AND QUANTITY | 5 WIRE LEAD |
| TERMINAL LOCATION | REAR |
| BODY MATERIAL | STEEL, STAINLESS |
| FRAGILITY FACTOR | MODERATELY RUGGED |